Handle control mechanism

By designing a handle control mechanism that uses a spiral disc and cable assembly to drive the shaft to rotate, the deflection of the trim tabs is achieved. This solves the problem of increased control force when the trim tab control system malfunctions, and improves the aircraft's handling feel and safety.

CN121573155APending Publication Date: 2026-02-27SHAANXI AIRCRAFT CORPORATION
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Patent Information

Application Number
CN202511744179.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-11-25
Publication Date
2026-02-27

AI Technical Summary

Technical Problem

In the prior art, when the control plate control system malfunctions, the pilot is unable to control the control surface control plates to deflect, resulting in increased control surface force and affecting the aircraft's handling feel.

Method used

A handle control mechanism is designed, including a shaft, a steel cable assembly, a pointer assembly, a control handwheel, a first bracket, and a second bracket. The shaft and steel cable assembly are rotated by a spiral disc to achieve the deflection of the adjustment plate, providing a manual operation mode.

Benefits of technology

It effectively reduces the burden on the pilot to operate the control surfaces, improves the safety and reliability of the aircraft, and ensures the normal handling performance of the aircraft.

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Abstract

The invention provides a handle control mechanism, and belongs to the technical field of flight control, the handle control mechanism specifically comprises a shaft, a steel cable assembly, a pointer assembly, a control hand wheel, a first support and a second support, the shaft is supported in a bearing hole of the first support, the shaft is sleeved with the control hand wheel and is far away from the first support, and the pointer assembly comprises a spiral disc, a pointer, a label and a support; the spiral disc is fixedly connected with the shaft and connected with the back face of the control hand wheel, one end of the pointer is movably connected with the spiral disc, the other end of the pointer is fixed in a lining on a side arm of an engine control console, the label is fixed to the support, the support is fixed to the second support, the shaft is sleeved with the second support, and the steel cable assembly is fixedly connected with the shaft. The steel cable assembly is located between the first support and the second support, and the control hand wheel is rotated to drive the shaft and the steel cable assembly to rotate together through the spiral disc. By means of the processing scheme, deflection of the adjusting piece can be achieved, and the burden of a driver for controlling the control surface is relieved.
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Description

TECHNICAL FIELD

[0001] The present application relates to the field of flight control technology, and particularly relates to a handle control mechanism. BACKGROUND

[0002] The adjusting piece control system is used for balancing the airplane, reducing the fatigue of the pilot, and reducing the control force on the control stick when the airplane takes off and lands. When the control surface deflects, the adjusting piece automatically deflects in the opposite direction of the control surface to reduce the control force of the control surface. When the adjusting piece control system fails, the pilot cannot control the adjusting piece of the control surface to deflect, the control force of the control surface becomes large, and the control feeling of the airplane is affected. SUMMARY

[0003] Therefore, the embodiments of the present application provide a handle control mechanism, which at least partly solves the problem that the pilot cannot control the adjusting piece of the control surface to deflect, the control force of the control surface becomes large, and the control feeling of the airplane is affected when the adjusting piece control system fails.

[0004] The embodiments of the present application provide a handle control mechanism, which comprises a shaft, a steel cable assembly, a pointer assembly, a control handle, a first support and a second support. The shaft is supported in a bearing hole of the first support. The control handle is sleeved on the shaft and away from the first support. The pointer assembly comprises a spiral disc, a pointer, a label and a support. The spiral disc is fixedly connected with the shaft. The spiral disc is connected with the back of the control handle. One end of the pointer is movably connected with the spiral disc. The other end of the pointer is fixed in a bushing on a side arm of an engine control table. The label is fixed on the support. The support is fixed on the second support. The second support is sleeved on the shaft. The steel cable assembly is fixedly connected with the shaft. The steel cable assembly is located between the first support and the second support. The control handle is rotated to drive the shaft and the steel cable assembly to rotate together through the spiral disc.

[0005] According to a specific implementation manner of the embodiments of the present application, the back of the spiral disc is provided with a spiral groove. One end of the pointer is provided with a first shaft. The first shaft is in sliding fit with the spiral groove.

[0006] According to a specific implementation manner of the embodiments of the present application, the front of the spiral disc is provided with a plurality of bosses. The back of the control handle is provided with a plurality of grooves. The bosses are connected with the grooves in fit.

[0007] According to a specific implementation manner of the embodiments of the present application, the pointer assembly further comprises organic glass and a third support. The third support is fixed on the support. The organic glass is installed on the third support. The organic glass covers the label.

[0008] According to a specific implementation manner of the embodiments of the present application, the steel cable assembly comprises a steel cable drum, a second bushing and a third bushing. The steel cable drum is connected with the shaft through bolts. The front and rear ends of the steel cable drum are respectively provided with the second bushing and the third bushing. The steel cable drum is wound with a steel cable.

[0009] According to a specific implementation manner of the embodiment of the present application, the spiral disc is fixedly connected with the shaft through the spline.

[0010] According to a specific implementation manner of the embodiment of the present application, the handle control mechanism further comprises a top cover, one end of the top cover is fixed on the first support, the other end of the top cover is fixed on the second support, and the cable assembly is located on the inner side of the top cover.

[0011] According to a specific implementation manner of the embodiment of the present application, the front end of the center of the control hand wheel is provided with a front cover and a nut, and the control hand wheel is limited on the shaft through the front cover and the nut.

[0012] According to a specific implementation manner of the embodiment of the present application, the other end of the pointer is provided with a second shaft, and the pointer is supported in the bushing on the engine control platform side arm through the second shaft.

[0013] According to a specific implementation manner of the embodiment of the present application, the four protrusions and the four grooves are evenly distributed on the circumferential surface respectively.

[0014] Beneficial effects: The handle control mechanism in the embodiment of the present application, by setting the shaft, the cable assembly, the pointer assembly, the control hand wheel, the first support and the second support and forming a specific connection relationship between the components, when the control hand wheel is rotated, the shaft and the cable assembly can be driven to rotate together through the spiral disc, and then the deflection of the adjusting sheet can be realized. This structure provides a manual control of the deflection of the adjusting sheet for the pilot when the adjusting sheet control system fails, effectively reduces the burden of the pilot on the control surface, avoids the influence of the control surface on the control feeling of the aircraft due to the increase of the control force of the control surface, and improves the safety and reliability of the flight of the aircraft. At the same time, the handle control mechanism has reasonable structure design, stable connection of components and convenient operation, and has high practicability and popularization value. BRIEF DESCRIPTION OF DRAWINGS

[0015] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings needed in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creating laborious work.

[0016] Figure 1 It is a perspective view of the handle control mechanism according to an embodiment of the present application; Figure 2 It is an exploded view of the handle control mechanism according to an embodiment of the present application; Figure 3 It is a front structure view of the spiral disc according to an embodiment of the present application; Figure 4 This is a structural diagram of the back of a spiral disk according to an embodiment of the present invention; Figure 5 This is a schematic diagram of a pointer according to an embodiment of the present invention; Figure 6 This is a schematic diagram of the control lines of the elevator adjustment plate of the handle control mechanism according to an embodiment of the present invention.

[0017] In the diagram: 1. Handwheel, 2. Spiral disc, 3. First bushing, 4. Second bracket, 5. Second bushing, 6. First steel cable, 7. Steel cable drum, 8. Second steel cable, 9. Third bushing, 10. First bracket, 11. Small shaft, 12. Shaft, 13. First bolt, 14. Second bolt, 15. First screw, 16. Second screw, 17. Top cover, 18. Acrylic glass, 19. Third screw, 20. Third bracket, 21. Sign, 22. Support, 23. Third bolt, 24. Pointer, 25. Nut, 26. Front cover, 28. Handle control mechanism, 29. Steel cable guide wheel, 30. Steel cable guide plate, 31. Upper deflecting steel cable, 32. Lower deflecting steel cable, 33. Drum, 34. Elevator adjustment plate. Detailed Implementation

[0018] The embodiments of this application will now be described in detail with reference to the accompanying drawings.

[0019] The following specific examples illustrate the implementation of this application. Those skilled in the art can easily understand other advantages and effects of this application from the content disclosed in this specification. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of them. This application can also be implemented or applied through other different specific embodiments, and the details in this specification can also be modified or changed based on different viewpoints and applications without departing from the spirit of this application. It should be noted that, in the absence of conflict, the following embodiments and features in the embodiments can be combined with each other. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0020] It should be noted that various aspects of embodiments within the scope of the appended claims are described below. It will be apparent that the aspects described herein can be embodied in a wide variety of forms, and any particular structure and / or function described herein is merely illustrative. Based on this application, those skilled in the art will understand that one aspect described herein can be implemented independently of any other aspect, and two or more of these aspects can be combined in various ways. For example, any number of aspects set forth herein can be used to implement the device and / or practice the method. Additionally, this device and / or method can be implemented using structures and / or functionalities other than one or more of the aspects set forth herein.

[0021] It should also be noted that the illustrations provided in the following embodiments are only schematic representations of the basic concept of this application. The illustrations only show the components related to this application and are not drawn according to the number, shape and size of the components in actual implementation. In actual implementation, the form, quantity and proportion of each component can be arbitrarily changed, and the layout of the components may also be more complex.

[0022] Furthermore, specific details are provided in the following description to facilitate a thorough understanding of the examples. However, those skilled in the art will understand that the described aspects can be practiced without these specific details.

[0023] This application provides a handle control mechanism, which is described below with reference to... Figures 1 to 6 Provide a detailed description.

[0024] In one embodiment, refer to Figure 1 and Figure 2 The handle control mechanism includes a shaft 12, a steel cable assembly, a pointer 24 assembly, a control handwheel 1, a first bracket 10, and a second bracket 4. The shaft 12 is supported in the shaft 12 bearing hole of the first bracket 10. The control handwheel 11 is sleeved on the shaft 12 and away from the first bracket 10. The pointer 24 assembly includes a spiral disc 2, a pointer 24, a nameplate 21, and a support 22. The spiral disc 2 is fixedly connected to the shaft 12 and connected to the back of the control handwheel 1. One end of the pointer 24 is movably connected to the spiral disc 2, and the other end of the pointer 24 is fixed in a bushing on the side arm of the engine control panel. The nameplate 21 is fixed on the support 22, and the support 22 is fixed on the second bracket 4. The second bracket 4 is sleeved on the shaft 12. The steel cable assembly is fixedly connected to the shaft 12 and is located between the first bracket 10 and the second bracket 4. Rotating the control handwheel 1 drives the shaft 12 and the steel cable assembly to rotate together via the spiral disc 2.

[0025] In this embodiment, the control handwheel 1 is mounted on the shaft 12. By selecting the control handwheel 1, the steel cable assembly is rotated. One end of the pointer 24 moves radially on the spiral disk 2 as the disk rotates, causing it to shift relative to the label 21, thereby indicating the scale and determining the direction and angle of the adjustment plate deflection. This allows for the deflection of the adjustment plate, reducing the driver's workload on the control surfaces.

[0026] Furthermore, refer to Figure 4 and Figure 5 The back of the spiral disk 2 has a spiral groove, and one end of the pointer 24 has a first shaft that slides within the spiral groove. As the spiral disk 2 rotates, the first shaft of the pointer 24 moves radially within the spiral groove, causing displacement relative to the mark 21, thus indicating the scale. This design makes the movement of the pointer 24 smoother and more precise, accurately reflecting the deflection of the adjustment plate.

[0027] Furthermore, refer to Figure 3 The front of the spiral disk 2 has multiple bosses, and the back of the operating handwheel 1 has multiple grooves. The bosses and grooves are connected by a mating fit. Through the mating fit of the bosses and grooves, the rotation of the operating handwheel 1 drives the rotation of the spiral disk 2, which in turn drives the shaft 12 to rotate.

[0028] Furthermore, in order to protect the sign 21 from contamination or damage, the pointer 24 assembly also includes an acrylic glass 18 and a third bracket 20. The third bracket 20 is fixed on the support 22, and the acrylic glass 18 is mounted on the third bracket 20. The acrylic glass 18 covers the sign 21, and the scale on the sign 21 can be seen through the acrylic glass 18.

[0029] Furthermore, the cable assembly includes a cable drum 7, a second bushing 5, and a third bushing 9. The cable drum 7 is connected to the shaft 12 by bolts. The second bushing 5 and the third bushing 9 are respectively installed at the front and rear ends of the cable drum 7. A steel cable is wound around the cable drum 7. The steel cable includes a first steel cable and a second steel cable, which are connected to the elevator adjustment plate control line. Specifically, refer to... Figure 6 The first and second steel cables correspond to the lower and upper deflection cables, respectively, and are guided by cable guide wheels. Cable guide plates are fitted onto the lower and upper deflection cables. The lower deflection cable bypasses the drum 33 to become the upper deflection cable, and the drum drives the elevator trim plate to deflect. When the control lever 28 rotates clockwise, the lower deflection cable is under tension, causing the drum 33 to rotate. This, in turn, causes the drum 33 to drive the elevator trim plate 34 to deflect upwards, achieving the aircraft trim function.

[0030] In one embodiment, the spiral disk 2 is fixedly connected to the shaft 12 via a spline.

[0031] In one embodiment, the handle control mechanism further includes a top cover 17, one end of which is fixed to a first bracket 10 and the other end of which is fixed to a second bracket 4, with the cable assembly located inside the top cover 17.

[0032] In one embodiment, the front end of the center of the operating handwheel 1 is provided with a front cover 26 and a nut 25, which limit the operating handwheel 1 on the shaft 12.

[0033] In one embodiment, refer to Figure 5 The other end of the pointer 24 is provided with a second shaft, through which the pointer 24 is supported in a bushing on the side arm of the engine control panel.

[0034] In one embodiment, refer to Figure 3 There are four bosses and four grooves, which are evenly distributed on the circumferential surface.

[0035] In practical implementation, the steel cable assembly is connected to the shaft 12 via bolts or other connectors, and the various components are connected to each other via bolts, screws, or other connectors, including the first bushing 3, small shaft 11, first bolt 13, second bolt 14, first screw 15, second screw 16, third screw 19, and third bolt 23. This embodiment is merely an example and is not limited to the types and quantities of connectors listed in this embodiment.

[0036] The working principle of the handle control mechanism in this application is as follows: When the pilot turns the control handwheel 1, the control handwheel 1 drives the spiral disk 2 to rotate. Since the spiral disk 2 is fixedly connected to the shaft 12, the shaft 12 also rotates accordingly. The rotation of the shaft 12 further drives the cable assembly to rotate. The cables in the cable assembly are guided by guide wheels and guide plates, and finally connected to the elevator trim control lines. When the cable assembly rotates, it pulls or releases the corresponding cables, thereby driving the drum 33 to rotate. The drum 33 then drives the elevator trim to deflect. At the same time, the rotation of the spiral disk 2 causes the first axis of the pointer 24 to move radially within the spiral groove. The pointer 24 is displaced relative to the label 21, thereby indicating the direction and angle of the trim deflection. The pilot can precisely control the deflection of the trim according to the indication of the pointer 24 to achieve the aircraft trim function, reduce the control burden, and improve flight safety.

[0037] The embodiments provided by this invention achieve efficient and precise control of aircraft control levers through the ingenious design and combination of the various components of the control lever mechanism. This control lever mechanism is compact in structure and easy to operate, effectively reducing the pilot's workload when manipulating control surfaces and improving aircraft handling performance and flight safety. In practical applications, the size and material of the control lever mechanism can be appropriately adjusted and optimized according to the specific needs of different aircraft to better meet actual usage requirements. Furthermore, the design concept and method of this control lever mechanism can also provide reference and guidance for designs in other related fields.

[0038] The above description is merely a specific embodiment of this application, but the scope of protection of this application is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this application should be included within the scope of protection of this application. Therefore, the scope of protection of this application should be determined by the scope of the claims.

Claims

1. A handle operating mechanism, characterized in that, The device includes a shaft (12), a cable assembly, a pointer (24) assembly, a handwheel (1), a first bracket (10), and a second bracket (4). The shaft (12) is supported in the shaft (12) bearing hole of the first bracket (10). The handwheel is sleeved on the shaft (12) and is located away from the first bracket (10). The pointer (24) assembly includes a spiral disc (2), a pointer (24), a nameplate (21), and a support (22). The spiral disc (2) is fixedly connected to the shaft (12) and is connected to the back of the handwheel (1). One end of the pointer (24) is movably connected to the spiral disk (2), and the other end of the pointer (24) is fixed in the bushing on the side arm of the engine control panel. The nameplate (21) is fixed on the support (22), the support (22) is fixed on the second bracket (4), the second bracket (4) is sleeved on the shaft (12), the steel cable assembly is fixedly connected to the shaft (12), and the steel cable assembly is located between the first bracket (10) and the second bracket (4). Rotating the control handwheel (1) drives the shaft (12) and the steel cable assembly to rotate together through the spiral disk (2).

2. The handle operating mechanism according to claim 1, characterized in that, The back of the spiral disk (2) is provided with a spiral groove, and one end of the pointer (24) is provided with a first shaft, which slides in conjunction with the spiral groove.

3. The handle operating mechanism according to claim 1, characterized in that, The front of the spiral disc (2) is provided with multiple protrusions, and the back of the operating handwheel (1) is provided with multiple grooves, with the protrusions and grooves cooperating and connecting.

4. The handle operating mechanism according to claim 1, characterized in that, The pointer (24) assembly also includes an acrylic glass (18) and a third bracket (20), the third bracket (20) being fixed to the support (22), the acrylic glass (18) being mounted on the third bracket (20), and the acrylic glass (18) covering the sign (21).

5. The handle operating mechanism according to claim 1, characterized in that, The cable assembly includes a cable drum (7), a second bushing (5) and a third bushing (9). The cable drum (7) is connected to the shaft (12) by bolts. The second bushing (5) and the third bushing (9) are respectively provided at the front and rear ends of the cable drum (7). The cable drum (7) is wound with a steel cable.

6. The handle operating mechanism according to claim 1, characterized in that, The spiral disk (2) is fixedly connected to the shaft (12) via a spline.

7. The handle operating mechanism according to claim 1, characterized in that, The handle control mechanism also includes a top cover (17), one end of which is fixed to the first bracket (10), and the other end of which is fixed to the second bracket (4). The cable assembly is located inside the top cover (17).

8. The handle operating mechanism according to claim 1, characterized in that, The front end of the center of the operating handwheel (1) is provided with a front cover (26) and a nut (25), which limit the operating handwheel (1) on the shaft (12) by the front cover (26) and the nut (25).

9. The handle operating mechanism according to claim 2, characterized in that, The other end of the pointer (24) is provided with a second shaft, through which the pointer (24) is supported in a bushing on the side arm of the engine control panel.

10. The handle operating mechanism according to claim 3, characterized in that, There are four bosses and four grooves, which are evenly distributed on the circumferential surface.

Citation Information

Patent Citations

  • Deflection indicating method for elevator trim tab of aircraft

    CN110065621A