MULTI-AXIS AIRFLOW RECTIFICATION SYSTEM WITH SYNCHRONOUS FLOW GUIDE ADJUSTMENT

Abstract

Disclosed is a multi-axis airflow rectification system comprising a series of rotational flow guides disposed within a housing structure. Each said rotational flow guide is aligned along an axis intersecting an airflow channel. A gear assembly is longitudinally coupled to said rotational flow guides to enable synchronous rotational adjustment. A control unit is engaged with said gear assembly to regulate the orientation of said rotational flow guides to optimize airflow laminarity through such a housing structure.

Specification

Description:Field of the Invention


The present disclosure generally relates to airflow control systems. Further, the present disclosure particularly relates to a multi-axis airflow rectification system to optimize airflow laminarity.
Background
The background description includes information that may be useful in understanding the present invention. It is not an admission that any of the information provided herein is prior art or relevant to the presently claimed invention, or that any publication specifically or implicitly referenced is prior art.
Various airflow rectification systems are well-known for enhancing airflow laminarity in different environments. Such systems typically find use in industrial, automotive, and aerospace applications where controlling airflow is critical to optimize efficiency, reduce turbulence, and improve aerodynamic performance. One common method involves the utilization of fixed guide vanes, which are arranged along an airflow path to direct air through specific angles. These fixed guide vanes attempt to smoothen the airflow and reduce turbulence. However, the fixed nature of such guide vanes limits adaptability, especially in situations where airflow conditions are variable or subject to change. Consequently, the performance of such systems remains suboptimal in dynamic environments, resulting in reduced efficiency and increased energy consumption.
Further, certain state-of-the-art systems employ active flow control devices, which include adjustable guide vanes or fins. Such systems attempt to address the limitation of fixed vanes by allowing for some degree of control over airflow direction. Active systems frequently involve the use of electronic actuators to alter the orientation of guide vanes based on real-time airflow conditions. Nevertheless, such systems often suffer from complexities related to the actuation mechanisms, requiring intricate designs that are prone to mechanical failures. Additionally, the response time of electronic actuators can be slow, leading to inadequate adjustments during rapid fluctuations in airflow, which causes further inefficiencies in maintaining optimal laminarity.
Moreover, another class of known systems incorporates rotating guide structures to direct airflow. Such systems use rotationally adjustable vanes or blades to influence airflow in a controlled manner. Although rotational guide structures offer enhanced flexibility over fixed vanes, the control mechanisms for such systems often rely on multiple independent motors or actuators. This decentralization of control introduces significant complexities in synchronization between the multiple moving parts. Synchronization problems can result in irregularities in airflow, leading to turbulence rather than reducing it. Furthermore, decentralization increases maintenance needs due to the high number of individual components, increasing the likelihood of system malfunctions.
Additionally, gear-based systems are also used in certain airflow rectification techniques, where gears control the movement of guide structures along a specific axis. Such gear-based systems, while robust in design, are limited by their inability to handle complex multi-axis adjustments. Most conventional systems operate along a single axis, thereby restricting the system's capability to adapt to varying directions of airflow. As a result, the system's effectiveness diminishes when airflow enters from multiple directions or when the system operates in environments with unpredictable airflow patterns. The lack of multi-axis adjustability also imposes constraints on the system's ability to optimize airflow laminarity, particularly in high-performance applications.
In light of the above discussion, there exists an urgent need for solutions that overcome the problems associated with conventional systems and/or techniques for airflow rectification, particularly in maintaining optimal laminarity and synchronization across dynamic environments.
Summary
The following presents a simplified summary of various aspects of this disclosure in order to provide a basic understanding of such aspects. This summary is not an extensive overview of all contemplated aspects, and is intended to neither identify key or critical elements nor delineate the scope of such aspects. Its purpose is to present some concepts of this disclosure in a simplified form as a prelude to the more detailed description that is presented later.
The following paragraphs provide additional support for the claims of the subject application.
An objective of the present disclosure is to provide a multi-axis airflow rectification system that enables optimal control over airflow laminarity and precise directional adjustments in an airflow channel. The system of the present disclosure aims to optimize airflow characteristics by regulating the orientation of multiple rotational flow guides disposed within a housing structure.
In an aspect, the present disclosure provides a multi-axis airflow rectification system comprising a series of rotational flow guides disposed within a housing structure, each rotational flow guide being aligned along an axis intersecting an airflow channel. A gear assembly is longitudinally coupled to said rotational flow guides to enable synchronous rotational adjustment, and a control unit is engaged with said gear assembly to regulate the orientation of said rotational flow guides to optimize airflow laminarity through the housing structure.
Further, the system enhances airflow precision through tangential interfacing of each rotational flow guide with an airflow channel wall via a pivot joint, which minimizes friction and enhances angular adjustment. Moreover, a torque distribution shaft transversely integrated with the gear assembly uniformly distributes rotational force across the rotational flow guides. The control unit is operatively linked to a variable resistance element positioned adjacent to the gear assembly to regulate the rotational speed of the flow guides in response to varying airflow conditions.
Additionally, each rotational flow guide incorporates a series of micro-fins along its surface, which disrupts boundary layer formation and enhances laminar airflow. The housing structure includes a mounting framework arranged perpendicularly to the airflow channel to provide secure attachment for the rotational flow guides, while allowing for selective disengagement when required.
Furthermore, an aerodynamic casing encompasses the rotational flow guides, which streamlines the airflow and reduces turbulence. A dampening unit engaged with the gear assembly absorbs rotational shocks, improving the operational stability of the system. The control unit also comprises a feedback sensor positioned along the torque distribution shaft to monitor and adjust the angular displacement of the rotational flow guides in real-time. The rotational flow guides are provided with an interlocking feature, engaging adjacent guides in a sequential pattern, enhancing the system's synchronized movement.

Brief Description of the Drawings


The features and advantages of the present disclosure would be more clearly understood from the following description taken in conjunction with the accompanying drawings in which:
FIG. 1 illustrates a multi-axis airflow rectification system (100), in accordance with the embodiments of the present disclosure.
FIG. 2 illustrates the operational sequence of a multi-axis airflow rectification system 100, in accordance with the embodiments of the present disclosure.
Detailed Description
In the following detailed description of the invention, reference is made to the accompanying drawings that form a part hereof, and in which is shown, by way of illustration, specific embodiments in which the invention may be practiced. In the drawings, like numerals describe substantially similar components throughout the several views. These embodiments are described in sufficient detail to claim those skilled in the art to practice the invention. Other embodiments may be utilized and structural, logical, and electrical changes may be made without departing from the scope of the present invention. The following detailed description is, therefore, not to be taken in a limiting sense, and the scope of the present invention is defined only by the appended claims and equivalents thereof.
The use of the terms "a" and "an" and "the" and "at least one" and similar referents in the context of describing the invention (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or clearly contradicted by context. The use of the term "at least one" followed by a list of one or more items (for example, "at least one of A and B") is to be construed to mean one item selected from the listed items (A or B) or any combination of two or more of the listed items (A and B), unless otherwise indicated herein or clearly contradicted by context. The terms "comprising," "having," "including," and "containing" are to be construed as open-ended terms (i.e., meaning "including, but not limited to,") unless otherwise noted. Recitation of ranges of values herein are merely intended to serve as a shorthand method of referring individually to each separate value falling within the range, unless otherwise indicated herein, and each separate value is incorporated into the specification as if it were individually recited herein. All methods described herein can be performed in any suitable order unless otherwise indicated herein or otherwise clearly contradicted by context. The use of any and all examples, or exemplary language (e.g., "such as") provided herein, is intended merely to better illuminate the invention and does not pose a limitation on the scope of the invention unless otherwise claimed. No language in the specification should be construed as indicating any non-claimed element as essential to the practice of the invention.
Pursuant to the "Detailed Description" section herein, whenever an element is explicitly associated with a specific numeral for the first time, such association shall be deemed consistent and applicable throughout the entirety of the "Detailed Description" section, unless otherwise expressly stated or contradicted by the context.
As used herein, the term "multi-axis airflow rectification system" refers to an arrangement of components designed to direct and regulate airflow along multiple axes. Such a system includes a series of flow-guiding elements and mechanisms that alter the trajectory of the airflow in order to achieve a laminar flow pattern. The system can be utilized in a variety of applications, including, but not limited to, industrial ventilation, automotive air management, and HVAC systems. The "multi-axis airflow rectification system" typically includes multiple axes of rotation to manipulate the direction of the airflow, ensuring that such airflow passes through specific channels in an organized manner. Said system is contained within a housing structure, which protects the internal components and ensures smooth airflow passage. The housing structure may be cylindrical, rectangular, or any other shape, depending on the specific application requirements. In certain applications, additional components, such as filters or dampers, may also be incorporated within the system.
As used herein, the term "rotational flow guide" refers to a flow-directing component that rotates around an axis to adjust the direction and alignment of the airflow. Such a component may be composed of blades or vanes, which can alter their orientation to regulate airflow within a system. Each said "rotational flow guide" is positioned along a specific axis that intersects the airflow channel within the housing structure. The purpose of the rotational flow guide is to direct airflow in a precise manner to achieve the desired flow characteristics, such as laminar flow or reduction of turbulence. The design and material of such rotational flow guides may vary depending on the system's operational requirements, such as the flow rate or pressure conditions. In certain embodiments, multiple rotational flow guides may be used in tandem to manipulate airflow along multiple axes, providing a more controlled airflow environment.
As used herein, the term "housing structure" refers to a protective enclosure that contains and supports the components of the system. Such a structure typically surrounds the internal elements, such as rotational flow guides and gear assemblies, to ensure smooth operation and efficient airflow management. The "housing structure" may have various shapes and sizes, depending on the specific design and intended application of the system. Materials used for the housing structure may include metals, polymers, or composites, depending on factors such as weight, durability, and environmental exposure. The housing structure is typically designed to provide both structural integrity and aerodynamic efficiency, ensuring that airflow through the system is optimized while protecting internal components from external influences, such as dust or debris. In some cases, the housing structure may also include access panels or ports for maintenance and inspection purposes.
As used herein, the term "airflow channel" refers to the passage through which air travels within the system. Such a channel is defined by the arrangement of internal components and the boundaries of the housing structure. The airflow channel allows for the smooth and controlled passage of air from the inlet to the outlet of the system. The dimensions and configuration of the airflow channel can vary depending on the application, with certain channels being designed to promote laminar flow, while others may focus on maximizing airflow volume or velocity. The airflow channel works in conjunction with the rotational flow guides to manage and direct the airflow along the intended path, reducing turbulence and improving system performance. Additional elements, such as baffles or perforated plates, may also be incorporated within the airflow channel to further influence airflow characteristics.
As used herein, the term "gear assembly" refers to a mechanical system consisting of gears that are coupled to one another to transmit rotational motion. Said "gear assembly" is connected to the rotational flow guides in order to facilitate synchronous movement and adjustment. Each gear within the assembly interacts with adjacent gears, ensuring that the rotational flow guides align in a coordinated manner along their respective axes. The design of such a gear assembly can vary depending on the number of rotational flow guides in the system and the degree of precision required for their adjustment. The gear assembly may be operated manually or controlled via an automated system, depending on the application. Materials for the gears may include metals, plastics, or composites, selected based on factors such as load-bearing capacity and environmental resistance. The gear assembly's placement within the housing structure ensures that the rotational flow guides adjust simultaneously to regulate airflow effectively.
As used herein, the term "control unit" refers to an electronic or mechanical device that governs the operation of other system components. Said "control unit" is engaged with the gear assembly to regulate the movement and orientation of the rotational flow guides. In most cases, the control unit receives input signals, which correspond to system parameters such as airflow rate, pressure, or direction. Based on such inputs, the control unit adjusts the gear assembly to alter the orientation of the rotational flow guides in real-time. The control unit may be programmable or pre-configured to operate within specific parameters, depending on the requirements of the system. The design of the control unit typically includes both input and output interfaces, enabling communication with external sensors or control systems. In some embodiments, the control unit may also incorporate feedback loops to monitor system performance and make necessary adjustments to maintain optimal airflow conditions.
FIG. 1 illustrates a multi-axis airflow rectification system (100), in accordance with the embodiments of the present disclosure. In an embodiment, a series of rotational flow guides 102 are disposed within a housing structure 104 of the regulation system 100 arranged in a wind turbine apparatus 110. Each said rotational flow guide 102 is positioned along an axis that intersects an airflow channel 106, thereby allowing the flow of air to be directed in a controlled manner. The rotational flow guides 102 may consist of a series of blades or vanes that are oriented along their respective axes to modify the direction of airflow as it passes through the housing structure 104. Each rotational flow guide 102 can be individually or collectively adjusted to align with the airflow, thereby minimizing turbulence and promoting a more uniform airflow. The positioning of the rotational flow guides 102 is such that the axes of rotation intersect the airflow channel 106 at predetermined intervals, allowing for precise management of the airflow through the housing structure 104. The rotational flow guides 102 may be constructed from materials that can withstand high airflow velocities and environmental factors associated with wind turbine operations.
In an embodiment, a gear assembly 108 is longitudinally coupled to the rotational flow guides 102 to facilitate synchronous rotational adjustment of said flow guides 102. The gear assembly 108 comprises a series of interlocking gears or other mechanical components that are aligned along the length of the housing structure 104. Said gear assembly 108 transmits rotational movement along the axis of the rotational flow guides 102, ensuring that each flow guide 102 rotates simultaneously in response to external inputs. The longitudinal coupling of the gear assembly 108 ensures that rotational adjustments can be made across the entire series of flow guides 102, allowing for coordinated changes in airflow direction through the airflow channel 106. The gear assembly 108 may include components such as shafts, bearings, and couplings that facilitate the smooth transmission of mechanical forces. The material composition and design of the gear assembly 108 may vary depending on the operational demands of the wind turbine apparatus 110, with considerations for durability, maintenance, and operational efficiency.
In an embodiment, a control unit 110 is engaged with the gear assembly 108 to regulate the orientation of the rotational flow guides 102 for optimizing airflow laminarity through the housing structure 104. The control unit 110 may include an electronic interface, mechanical switches, or other devices that manage the input signals governing the rotational adjustment of the flow guides 102. Said control unit 110 receives input regarding the current airflow conditions, which could be based on factors such as wind speed, pressure, or direction. The control unit 110 then processes such input and adjusts the gear assembly 108 accordingly, enabling real-time manipulation of the rotational flow guides 102 to maintain or improve airflow conditions. The control unit 110 may also include feedback loops or sensors that monitor the system's performance, ensuring that the airflow remains consistent and laminar through the housing structure 104. The control unit 110 may be programmed or manually operated, depending on the specific requirements of the wind turbine apparatus 110, with provisions for both automatic and manual adjustments based on the operating conditions.
In an embodiment, each rotational flow guide 102 within the multi-axis airflow rectification system 100 is tangentially interfaced with an airflow channel 106 wall through a pivot joint. Said pivot joint allows for smooth angular movement of the rotational flow guide 102 while minimizing friction during such movement. The pivot joint serves as a connection point between the rotational flow guide 102 and the interior surface of the airflow channel 106, allowing the flow guide to swivel in response to external control signals. This swivel action facilitates the angular adjustment of the rotational flow guide 102, enabling fine-tuned control over the direction of airflow passing through the airflow channel 106. By tangentially interfacing the flow guide with the channel wall, the rotational flow guide 102 is capable of maximizing its range of motion while maintaining a close alignment with the airflow, which reduces resistance and prevents airflow disruption. The minimization of friction at the pivot joint further enhances the system's efficiency, ensuring that the rotational flow guide 102 can respond rapidly to changes in operational conditions.
In an embodiment, the gear assembly 108 of the multi-axis airflow rectification system 100 is transversely integrated with a torque distribution shaft. Said torque distribution shaft is responsible for transmitting rotational force uniformly across the series of rotational flow guides 102. The transverse integration of the gear assembly 108 with the torque distribution shaft ensures that each rotational flow guide 102 receives equal rotational force, regardless of its position within the system. This uniform distribution of torque enables synchronous movement of all flow guides 102, allowing them to adjust in tandem to optimize airflow characteristics within the airflow channel 106. The torque distribution shaft may be composed of materials capable of withstanding the mechanical forces generated during system operation, such as high-strength alloys or composites. By evenly distributing the torque, the torque distribution shaft ensures that no single rotational flow guide 102 is subjected to excessive strain, thereby extending the operational lifespan of the system.
In an embodiment, the control unit 110 of the multi-axis airflow rectification system 100 is operatively linked with a variable resistance element. Said variable resistance element is positioned adjacent to the gear assembly 108 and plays a key role in regulating the rotational speed of the rotational flow guides 102. By adjusting the resistance applied to the gear assembly 108, the variable resistance element enables the control unit 110 to fine-tune the rotational speed of the flow guides 102, allowing the system to adapt to varying airflow conditions. For example, in high wind conditions, the variable resistance element may increase the resistance applied to the gear assembly 108, thereby slowing the rotation of the flow guides 102 to maintain optimal airflow laminarity. Conversely, in lower wind conditions, the resistance can be reduced to allow for faster rotation and greater airflow manipulation. The variable resistance element may be electronically controlled, allowing for real-time adjustments based on input from external sensors monitoring wind speed and direction.
In an embodiment, each rotational flow guide 102 of the multi-axis airflow rectification system 100 incorporates a series of micro-fins along its surface. Said micro-fins extend radially from the surface of the rotational flow guide 102 and are strategically designed to disrupt boundary layer formation along the airflow channel 106. The boundary layer is a thin layer of air that adheres to the surface of the channel walls and the flow guide surfaces, which can cause drag and reduce the efficiency of the airflow system. By introducing micro-fins, the system creates localized turbulence along the surface of the flow guide 102, thereby disrupting the boundary layer and preventing its formation. This disruption minimizes drag and enhances the overall airflow characteristics within the channel 106. The micro-fins may vary in size and shape depending on the specific airflow conditions, and can be made from materials designed to withstand the forces associated with high-velocity airflow.
In an embodiment, the housing structure 104 of the multi-axis airflow rectification system 100 comprises a mounting framework with a locking latch. Said mounting framework is arranged perpendicularly relative to the airflow channel 106 and provides a secure attachment point for each of the rotational flow guides 102. The perpendicular arrangement of the framework ensures that the flow guides 102 are positioned in a manner that maximizes their ability to influence the direction of airflow. The locking latch allows for selective engagement and disengagement of the rotational flow guides 102 from the mounting framework, facilitating maintenance, replacement, or adjustment of individual components. The mounting framework may be composed of durable materials capable of withstanding mechanical stress, environmental exposure, and the high-velocity forces generated by the airflow. The locking latch is designed for easy operation, enabling quick adjustments without requiring disassembly of the entire system.
In an embodiment, the rotational flow guides 102 of the multi-axis airflow rectification system 100 are further encompassed by an aerodynamic casing. Said aerodynamic casing is affixed to the housing structure 104 and serves to streamline the flow path through the airflow channel 106. The casing is designed to reduce turbulence by smoothing the flow of air around the rotational flow guides 102, which helps maintain laminar flow throughout the system. The aerodynamic casing may be made of lightweight materials such as polymers or composites, which offer high strength and low resistance to airflow. The shape of the casing is contoured to match the natural flow path of the air within the channel 106, minimizing the creation of vortices or eddies that could disrupt the system's efficiency. In addition to reducing turbulence, the aerodynamic casing also provides a protective barrier for the flow guides 102, shielding them from external debris or damage.
In an embodiment, the gear assembly 108 of the multi-axis airflow rectification system 100 is further equipped with a dampening unit. Said dampening unit is engaged with each gear within the gear assembly 108 and is designed to absorb rotational shocks that may occur during the operation of the system. The dampening unit helps reduce the mechanical stress on the gears by cushioning the impact of sudden changes in rotational force. This is particularly important in applications where the airflow conditions are subject to rapid fluctuations, as the dampening unit prevents the gear assembly 108 from experiencing excessive wear or damage. The dampening unit may consist of springs, hydraulic components, or other energy-absorbing materials that are capable of withstanding repeated use. By absorbing shocks, the dampening unit enhances the longevity and reliability of the gear assembly 108, ensuring consistent performance over time.
In an embodiment, the control unit 110 of the multi-axis airflow rectification system 100 comprises a feedback sensor. Said feedback sensor is longitudinally positioned along the torque distribution shaft of the gear assembly 108 and is responsible for monitoring the angular displacement of the rotational flow guides 102 in real-time. The feedback sensor continuously measures the position of each flow guide 102 and transmits such data to the control unit 110. Based on this information, the control unit 110 can make precise adjustments to the gear assembly 108, ensuring that the flow guides 102 remain in the optimal position for controlling airflow. The feedback sensor may utilize various sensing technologies, such as optical encoders, magnetic sensors, or potentiometers, depending on the requirements of the system. By providing real-time feedback, the sensor enables the control unit 110 to respond quickly to changes in operational conditions, ensuring that the system maintains optimal airflow characteristics.
In an embodiment, the rotational flow guides 102 of the multi-axis airflow rectification system 100 are provided with an interlocking feature. Said interlocking feature is arranged to engage with adjacent flow guides 102 in a sequential pattern, ensuring that each guide moves in coordination with its neighboring guides. The interlocking feature may consist of mechanical components such as tabs, slots, or gears that physically connect adjacent flow guides 102, allowing them to rotate in unison. This sequential engagement ensures that all rotational flow guides 102 adjust simultaneously, providing consistent and coordinated airflow control throughout the system. The interlocking feature is designed to be durable and resistant to wear, ensuring that the flow guides 102 maintain proper alignment and coordination over extended periods of operation. The interlocking design also simplifies the system's mechanical layout by reducing the number of independent moving parts, which contributes to the overall stability and reliability of the airflow system.
FIG. 2 illustrates the operational sequence of a multi-axis airflow rectification system 100, in accordance with the embodiments of the present disclosure. Airflow enters through the airflow channel 106, where it encounters the rotational flow guides 102. Said flow guides 102 are disposed within the housing structure 104 and are aligned along axes that intersect the airflow channel 106. The rotational flow guides 102 adjust the airflow direction in response to input from the gear assembly 108, which is longitudinally coupled to said flow guides 102. The control unit 110 is engaged with the gear assembly 108 and sends adjustment signals to regulate the orientation of the rotational flow guides 102. Upon receiving the signal, the gear assembly 108 rotates the flow guides 102 in a synchronized manner to optimize airflow laminarity through the housing structure 104. After the airflow has been adjusted, it exits the housing structure 104, ensuring a more controlled and laminar flow.
In an embodiment, the multi-axis airflow rectification system 100 includes a series of rotational flow guides 102 disposed within a housing structure 104. Each rotational flow guide 102 is aligned along an axis that intersects an airflow channel 106. The alignment of said flow guides 102 along the intersecting axis allows for precise control over the direction of airflow through the airflow channel 106. This configuration enables the flow guides 102 to adjust the trajectory of airflow, promoting laminar flow and reducing turbulence. The ability of each flow guide 102 to rotate and align with the airflow path allows the system to respond dynamically to changing airflow conditions, improving overall control. Furthermore, the strategic placement of the flow guides 102 within the housing structure 104 enhances the system's ability to regulate airflow at various velocities and pressure levels, contributing to optimal aerodynamic performance and airflow stabilization across multiple axes.
In an embodiment, each rotational flow guide 102 is tangentially interfaced with an airflow channel 106 wall through a pivot joint. The pivot joint provides a smooth, low-friction connection, allowing the rotational flow guide 102 to swivel with minimized resistance. This tangential interface enables precise angular adjustment of the flow guide 102, enhancing its ability to direct airflow within the channel 106. The minimized friction at the pivot joint reduces mechanical wear and tear, ensuring long-term durability of the system while maintaining accurate adjustment capabilities. Additionally, the tangential interface facilitates smoother adjustments by allowing the flow guide 102 to pivot more freely, which is particularly beneficial in applications requiring continuous airflow regulation. The pivot joint's ability to handle angular changes ensures that the system can maintain consistent airflow direction under varying conditions, optimizing the overall aerodynamic behavior of the airflow channel 106.
In an embodiment, the gear assembly 108 is transversely integrated with a torque distribution shaft, providing a means for distributing rotational force evenly across all rotational flow guides 102. The integration of the torque distribution shaft allows for uniform rotational force transfer, ensuring that each flow guide 102 rotates synchronously with the others. This uniform distribution of torque prevents imbalances that could arise from uneven force application, which could potentially disrupt airflow control. By coordinating the rotational movement of each flow guide 102 through the torque distribution shaft, the system maintains a stable and consistent airflow direction throughout the airflow channel 106. The transverse integration also allows for efficient force transmission without excessive mechanical strain on individual components, contributing to the system's reliability during extended use. The smooth transfer of rotational force ensures that the system can maintain precise control over airflow direction even in high-demand scenarios.
In an embodiment, the control unit 110 is operatively linked with a variable resistance element, which is positioned adjacent to the gear assembly 108. The variable resistance element regulates the rotational speed of the flow guides 102 by modulating the resistance applied to the gear assembly 108. This configuration allows the system to adapt the rotational speed of the flow guides 102 to varying airflow conditions, such as changes in wind velocity or pressure fluctuations. By controlling the resistance, the system can slow down or speed up the rotation of the flow guides 102 as needed, ensuring that airflow laminarity is maintained through the airflow channel 106. The variable resistance element provides a means for dynamic adjustment, allowing for real-time optimization of airflow based on external conditions. The regulation of rotational speed via this element enhances the flexibility of the system, enabling it to respond effectively to both gradual and sudden changes in airflow dynamics.
In an embodiment, each rotational flow guide 102 incorporates a series of micro-fins along its surface, with said micro-fins extending radially from the central axis of the flow guide. These micro-fins are designed to disrupt the formation of boundary layers along the interior surface of the airflow channel 106. Boundary layers, which typically form as air adheres to the surface of the channel, can increase drag and reduce overall airflow efficiency. The inclusion of micro-fins breaks up these boundary layers by inducing localized turbulence, preventing the buildup of drag-inducing air along the surface. This disruption promotes smoother airflow through the channel 106, enhancing the system's ability to maintain laminar flow. The radial configuration of the micro-fins also improves the interaction between the airflow and the rotational flow guide 102, allowing for more effective airflow redirection and better overall performance of the airflow rectification system.
In an embodiment, the housing structure 104 comprises a mounting framework equipped with a locking latch, with the mounting framework being arranged perpendicularly to the airflow channel 106. The perpendicular arrangement allows the framework to securely hold the rotational flow guides 102 in place, ensuring stable operation within the airflow rectification system 100. The locking latch provides an additional layer of functionality by allowing selective engagement or disengagement of the flow guides 102 when required, such as during maintenance or system calibration. This secure yet flexible attachment mechanism prevents unwanted movement or displacement of the flow guides 102 while still allowing for quick adjustments or replacements. The mounting framework's perpendicular positioning also facilitates easy alignment of the flow guides 102 with the airflow channel 106, ensuring that the system can maintain optimal airflow control throughout its operation. The locking latch mechanism enhances the system's adaptability, particularly in applications requiring frequent adjustments or maintenance access.
In an embodiment, the rotational flow guides 102 are further encompassed by an aerodynamic casing, which is affixed to the housing structure 104. The aerodynamic casing serves to streamline the airflow passing through the airflow channel 106, reducing turbulence and promoting smoother air movement. By enclosing the rotational flow guides 102 within the casing, the system minimizes the creation of vortices or eddies that could otherwise disrupt the airflow's path. The aerodynamic design of the casing allows air to flow more smoothly around the flow guides 102, contributing to enhanced laminar flow and more efficient airflow rectification. The casing also provides a protective barrier for the flow guides 102, shielding them from external environmental factors such as dust or debris. The smooth, contoured surface of the aerodynamic casing helps reduce drag, improving the overall performance of the airflow channel 106 by maintaining a more consistent airflow trajectory.
In an embodiment, the gear assembly 108 is equipped with a dampening unit, which is engaged with each gear within the assembly. The dampening unit absorbs rotational shocks that may occur during the operation of the system, particularly when the rotational flow guides 102 undergo sudden changes in speed or direction. By cushioning the impact of such shocks, the dampening unit prevents excessive mechanical strain on the gear assembly 108, reducing the risk of wear or damage over time. The integration of the dampening unit ensures smoother operation of the gear assembly 108, allowing the rotational flow guides 102 to adjust more gradually and with less mechanical stress. This feature is especially beneficial in environments where airflow conditions can change rapidly, as the dampening unit helps maintain the integrity and longevity of the gear assembly 108 while ensuring consistent airflow control through the system.
In an embodiment, the control unit 110 is equipped with a feedback sensor, which is longitudinally positioned along the torque distribution shaft of the gear assembly 108. The feedback sensor continuously monitors the angular displacement of the rotational flow guides 102, providing real-time data to the control unit 110. Based on this feedback, the control unit 110 can make precise adjustments to the gear assembly 108, ensuring that the rotational flow guides 102 are positioned optimally for airflow control. The sensor detects even minor deviations in the angle of the flow guides 102, allowing for fine-tuned control over the direction of airflow within the airflow channel 106. The feedback sensor enables the system to adapt quickly to changing conditions, maintaining consistent performance by continuously adjusting the flow guides 102 based on real-time data. This monitoring capability enhances the overall precision of the airflow rectification system, ensuring optimal performance at all times.
In an embodiment, the rotational flow guides 102 are provided with an interlocking feature, allowing them to engage with adjacent flow guides 102 in a sequential pattern. The interlocking feature mechanically connects neighboring flow guides 102, ensuring that their movements are coordinated during operation. This sequential engagement allows the rotational flow guides 102 to adjust in unison, providing more consistent and reliable airflow control across the entire system. The interlocking mechanism prevents individual flow guides 102 from becoming misaligned, which could












I/We Claims


A multi-axis airflow rectification system (100) comprising:
a series of rotational flow guides (102) disposed within a housing structure (104), each said rotational flow guide (102) being aligned along an axis intersecting an airflow channel (106);
a gear assembly (108) longitudinally coupled to said rotational flow guides (102) to facilitate synchronous rotational adjustment; and
a control unit (110) engaged with said gear assembly (108) to regulate the orientation of said rotational flow guides (102) for optimizing airflow laminarity through such housing structure (104).
The multi-axis airflow rectification system (100) of claim 1, wherein each rotational flow guide (102) is tangentially interfaced with an airflow channel (106) wall through a pivot joint, allowing said rotational flow guide (102) to swivel with minimized friction, enhancing the angular adjustment for precise airflow direction.
The multi-axis airflow rectification system (100) of claim 1, wherein said gear assembly (108) is transversely integrated with a torque distribution shaft, said torque distribution shaft being configured to distribute rotational force uniformly across such rotational flow guides (102).
The multi-axis airflow rectification system (100) of claim 1, wherein said control unit (110) is operatively linked with a variable resistance element, such variable resistance element being positioned adjacent to said gear assembly (108) to regulate the rotational speed of said rotational flow guides (102) for adapting to varying airflow conditions.
The multi-axis airflow rectification system (100) of claim 1, wherein each said rotational flow guide (102) incorporates a series of micro-fins along the surface, said micro-fins extending radially and configured to disrupt boundary layer formation along said airflow channel (106).
The multi-axis airflow rectification system (100) of claim 1, wherein said housing structure (104) comprises a mounting framework with a locking latch, said mounting framework being perpendicularly arranged relative to said airflow channel (106), providing a secure attachment for said rotational flow guides (102) while allowing for selective disengagement when required.
The multi-axis airflow rectification system (100) of claim 1, wherein said rotational flow guides (102) are further encompassed by an aerodynamic casing, said aerodynamic casing being affixed to said housing structure (104) to streamline the flow path and reduce turbulence.
The multi-axis airflow rectification system (100) of claim 1, wherein said gear assembly (108) is further equipped with a dampening unit, said dampening unit being engaged with each gear within such assembly to absorb rotational shocks.
The multi-axis airflow rectification system (100) of claim 1, wherein said control unit (110) comprises a feedback sensor, said feedback sensor being longitudinally positioned along said torque distribution shaft of said gear assembly (108) to monitor and adjust the angular displacement of said rotational flow guides (102) in real-time.
The multi-axis airflow rectification system (100) of claim 1, wherein said rotational flow guides (102) are provided with an interlocking feature, said interlocking feature being arranged to engage with adjacent flow guides in a sequential pattern.




Disclosed is a multi-axis airflow rectification system comprising a series of rotational flow guides disposed within a housing structure. Each said rotational flow guide is aligned along an axis intersecting an airflow channel. A gear assembly is longitudinally coupled to said rotational flow guides to enable synchronous rotational adjustment. A control unit is engaged with said gear assembly to regulate the orientation of said rotational flow guides to optimize airflow laminarity through such a housing structure.

, Claims:I/We Claims


A multi-axis airflow rectification system (100) comprising:
a series of rotational flow guides (102) disposed within a housing structure (104), each said rotational flow guide (102) being aligned along an axis intersecting an airflow channel (106);
a gear assembly (108) longitudinally coupled to said rotational flow guides (102) to facilitate synchronous rotational adjustment; and
a control unit (110) engaged with said gear assembly (108) to regulate the orientation of said rotational flow guides (102) for optimizing airflow laminarity through such housing structure (104).
The multi-axis airflow rectification system (100) of claim 1, wherein each rotational flow guide (102) is tangentially interfaced with an airflow channel (106) wall through a pivot joint, allowing said rotational flow guide (102) to swivel with minimized friction, enhancing the angular adjustment for precise airflow direction.
The multi-axis airflow rectification system (100) of claim 1, wherein said gear assembly (108) is transversely integrated with a torque distribution shaft, said torque distribution shaft being configured to distribute rotational force uniformly across such rotational flow guides (102).
The multi-axis airflow rectification system (100) of claim 1, wherein said control unit (110) is operatively linked with a variable resistance element, such variable resistance element being positioned adjacent to said gear assembly (108) to regulate the rotational speed of said rotational flow guides (102) for adapting to varying airflow conditions.
The multi-axis airflow rectification system (100) of claim 1, wherein each said rotational flow guide (102) incorporates a series of micro-fins along the surface, said micro-fins extending radially and configured to disrupt boundary layer formation along said airflow channel (106).
The multi-axis airflow rectification system (100) of claim 1, wherein said housing structure (104) comprises a mounting framework with a locking latch, said mounting framework being perpendicularly arranged relative to said airflow channel (106), providing a secure attachment for said rotational flow guides (102) while allowing for selective disengagement when required.
The multi-axis airflow rectification system (100) of claim 1, wherein said rotational flow guides (102) are further encompassed by an aerodynamic casing, said aerodynamic casing being affixed to said housing structure (104) to streamline the flow path and reduce turbulence.
The multi-axis airflow rectification system (100) of claim 1, wherein said gear assembly (108) is further equipped with a dampening unit, said dampening unit being engaged with each gear within such assembly to absorb rotational shocks.
The multi-axis airflow rectification system (100) of claim 1, wherein said control unit (110) comprises a feedback sensor, said feedback sensor being longitudinally positioned along said torque distribution shaft of said gear assembly (108) to monitor and adjust the angular displacement of said rotational flow guides (102) in real-time.
The multi-axis airflow rectification system (100) of claim 1, wherein said rotational flow guides (102) are provided with an interlocking feature, said interlocking feature being arranged to engage with adjacent flow guides in a sequential pattern.

Documents