Mounting bracket assembly for engine throttle valve steering engine of aviation unmanned aerial vehicle

Abstract

The utility model provides an aviation unmanned aerial vehicle engine throttle valve steering engine installation support assembly which comprises an installation base frame, a steering engine frame arranged on the installation base frame and an inhaul cable frame arranged on the steering engine frame, the installation base frame comprises a plurality of installation blocks and an installation cross beam, each installation block is arranged on an engine, and the installation cross beam is arranged on the installation base frame. The mounting cross beam is detachably arranged on the mounting block, two through holes are formed in the top wall of the mounting cross beam, a limiting bolt is arranged in each through hole, each limiting bolt is fixed to the mounting cross beam through a nut, the steering engine frame is provided with a vertical section and a transverse section, and U-shaped through grooves are formed in the outer walls of the two sides of the vertical section and face the interior of the vertical section; the two through grooves are located above the two through holes respectively, and the inhaul cable frame is detachably arranged on the steering engine frame. By optimizing the structure of the support, the support is simple and compact in structure, convenient to assemble and high in strength, and therefore the support can be prevented from deforming in the using process.

Description

Technical Field

[0001] This utility model relates to the field of aviation unmanned aerial vehicle (UAV) engine technology, specifically to an aviation UAV engine throttle valve servo mounting bracket assembly. Background Technology

[0002] In the existing technology, the throttle position adjustment structure of unmanned aerial vehicles (UAVs) adopts the cable structure design of manned aircraft. This means that an additional throttle servo is needed to drive and adjust the position by adjusting the throttle cable. However, the structure of the servo installation will affect the accuracy of the servo, which will directly affect the control accuracy of the UAV engine and the control consistency of mass-produced engines.

[0003] Although the existing patent (publication number: CN201610978576) servo bracket mechanism has optimized and strengthened the support structure of the servo and increased the support at the back, it still has not solved the systemic problem of the throttle control accuracy of the UAV. Therefore, the existing technology has certain limitations. Utility Model Content

[0004] This utility model was developed to solve the above-mentioned problems, and its purpose is to provide an aviation unmanned aerial vehicle (UAV) engine throttle valve servo mounting bracket assembly.

[0005] This utility model provides a mounting bracket assembly for the throttle valve servo of an aircraft unmanned aerial vehicle (UAV) engine, characterized by comprising: a mounting base, a servo bracket mounted on the mounting base, and a cable bracket mounted on the servo bracket.

[0006] The mounting frame includes multiple mounting blocks and a mounting beam. Each mounting block is mounted on an engine and positioned near the engine's output end. The mounting beam is detachably mounted on the mounting block, located above the engine, and its orientation is perpendicular to the engine's axial direction. The top wall of the mounting beam has two through holes, each containing a limiting bolt. Each limiting bolt is secured to the mounting beam by a nut.

[0007] The servo mount is T-shaped and horizontally mounted on the mounting base. The servo mount has a vertical section and a horizontal section. The bottom wall of the vertical section fits against the top wall of the mounting beam. U-shaped through slots are formed on the outer walls of both sides of the vertical section, extending inwards. Two through slots are located above two through holes. The side walls of the horizontal section fit against the side walls of the mounting beam. A mounting hole for placing the servo is formed on the top wall of the horizontal section, specifically above the mounting beam.

[0008] The cable support is detachably mounted on the servo frame, and has slots for the cable to pass through. These slots are located below the servo's adjustment lever.

[0009] The distance between the two limit bolts is greater than the distance between the bottoms of the two through slots, but less than the distance between the openings of the two through slots.

[0010] The aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly provided by this utility model also has the following features: the distance between the end of the limiting bolt and the top wall of the mounting beam is not less than the depth of the through groove, and the end diameter of the limiting bolt is greater than the width of the through groove.

[0011] The aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly provided by this utility model also has the following features: each mounting block has multiple threaded grooves on its top wall, and the mounting beam has positioning holes corresponding to each threaded groove. Each positioning hole has a first fixing bolt for fixing the mounting beam to the mounting block.

[0012] The aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly provided by this utility model also has the following features: multiple mounting holes for fixing the servo are provided on the top wall of the horizontal section, above and below the mounting hole, each mounting hole has an internal thread on its wall, and each mounting hole has a second fixing bolt.

[0013] The aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly provided by this utility model also has the following features: a fixing hole is provided on the top wall of the horizontal section and on one side of the mounting hole; the cable frame is L-shaped; a threaded hole is provided on the vertical part of the cable frame corresponding to the position of each fixing hole; and a third fixing bolt is provided in each threaded hole.

[0014] The aviation unmanned aerial vehicle engine throttle valve servo mounting bracket assembly provided by this utility model also has the following feature: the slot is funnel-shaped.

[0015] The aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly provided by this utility model also has the following feature: the bottom wall of the mounting hole and the top wall of the vertical section are located on the same horizontal plane.

[0016] Functions and effects of utility models

[0017] According to the aviation unmanned aerial vehicle (UAV) engine throttle valve servo mounting bracket assembly involved in this utility model, by optimizing the bracket structure, the bracket structure is simple and compact, easy to assemble, and has high strength, thereby preventing the bracket from deforming during use. At the same time, because the bracket is arranged close to the engine throttle valve, it can reduce the cumulative control error of the throttle valve drive, and ensure the accuracy and consistency of the UAV engine throttle valve position control. Attached Figure Description

[0018] Figure 1 This is a front view of the present invention;

[0019] Figure 2 This is a top view of the present invention;

[0020] Figure 3 This is a structural schematic diagram of the present invention from a first-person perspective;

[0021] Figure 4 This is a structural schematic diagram of the present invention from a second perspective;

[0022] Figure 5 This is a schematic diagram of the structure of the present invention, an aviation unmanned aerial vehicle engine, and a throttle adjustment mechanism.

[0023] Explanation of reference numerals in the attached figures:

[0024] 10. Mounting base; 11. Mounting block; 12. Mounting beam; 13. Threaded groove; 14. Through hole; 15. Limit bolt; 16. Nut; 17. Positioning hole; 18. First fixing bolt; 20. Servo frame; 21. Vertical section; 22. Horizontal section; 23. Through groove; 24. Mounting hole; 25. Mounting hole; 26. Second fixing bolt; 27. Fixing hole; 30. Cable bracket; 31. Slot; 32. Threaded hole; 33. Third fixing bolt; A. Servo; B. Adjusting lever; C. Engine; D. Throttle valve; E. Throttle valve adjustment mechanism. Detailed Implementation

[0025] To make the technical means, creative features, objectives and effects of this utility model easy to understand, the following embodiments are described in detail with reference to the accompanying drawings.

[0026] Example

[0027] Figure 1 This is a front view of the present invention. Figure 2 This is a top view of the present invention. Figure 3 This is a structural schematic diagram of the present invention from a first-person perspective. Figure 4 This is a structural schematic diagram of the present invention from a second perspective. Figure 5 This is a schematic diagram of the structure of the present invention, an aviation unmanned aerial vehicle engine, and a throttle adjustment mechanism.

[0028] like Figures 1 to 5 As shown, this embodiment provides an aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly, including: a mounting base 10, a servo bracket 20 disposed on the mounting base 10, and a cable bracket 30 disposed on the servo bracket 20.

[0029] like Figures 1 to 4 As shown, the mounting base 10 includes multiple mounting blocks 11 and mounting beams 12.

[0030] In this embodiment, each mounting block 11 is mounted on an engine and positioned near the engine's output end. Each mounting block 11 has multiple threaded grooves 13 on its top wall.

[0031] like Figure 5 As shown, the specific number of mounting blocks 11 depends on the number of engines. One mounting block 11 can be installed above and below each engine, and near the throttle valve.

[0032] In this embodiment, the mounting beam 12 is detachably mounted on the mounting block 11. The mounting beam 12 is located above the engine and its arrangement direction is perpendicular to the axial direction of the engine. The top wall of the mounting beam 12 is provided with two through holes 14, and each of the two through holes 14 is provided with a limiting bolt 15. Each limiting bolt 15 is fixed to the mounting beam 12 by a nut 16.

[0033] like Figure 5 As shown, the mounting beam 12 is preferably L-shaped and inverted on multiple mounting blocks 11.

[0034] In this embodiment, a positioning hole 17 is provided on the mounting beam 12 at the position corresponding to each threaded groove 13, and a first fixing bolt 18 is provided in each positioning hole 17 for fixing the mounting beam 12 to the mounting block 11. The inner wall of the positioning hole 17 is provided with internal thread.

[0035] like Figures 1 to 4 As shown, the servo mount 20 is T-shaped and horizontally mounted on the mounting base 10. The servo mount 20 has a vertical section 21 and a horizontal section 22. The bottom wall of the vertical section 21 is flush with the top wall of the mounting beam 12. U-shaped through slots 23 are formed on both outer sides of the vertical section 21, extending inwards. The two through slots 23 are located above the two through holes 14. The side wall of the horizontal section 22 is flush with the side wall of the mounting beam 12. A mounting hole 24 for placing the servo is formed on the top wall of the horizontal section 22, above the mounting beam 12. The vertical section 21 and horizontal section 22 of the servo mount 20 can be found in the attached instruction manual. Figure 2 Included with instruction manual Figure 3 It is clearly distinguishable and can be seen in the text.

[0036] In this embodiment, the top wall of the horizontal segment 22 is provided with a plurality of mounting holes 25 for fixing the servo motor, located above and below the mounting hole 24. Each mounting hole 25 has an internal thread on its hole wall and a second fixing bolt 26 is provided in each mounting hole 25.

[0037] In this embodiment, a fixing hole 27 is provided on the top wall of the horizontal segment 22 and on one side of the mounting hole 24, and the inner wall of the fixing hole 27 is provided with an internal thread.

[0038] In this embodiment, the bottom wall of the mounting hole 24 and the top wall of the vertical section 21 are located on the same horizontal plane.

[0039] In this embodiment, the distance between the two limiting bolts 15 is greater than the distance between the bottoms of the two through slots 23, but less than the distance between the openings of the two through slots 23. Furthermore, the distance between the end of the limiting bolt 15 and the top wall of the mounting beam 12 is not less than the depth of the through slot 23, and the end diameter of the limiting bolt 15 is greater than the width of the through slot 23.

[0040] like Figures 1 to 4 As shown, the cable support 30 is detachably mounted on the servo frame 20. The cable support 30 has a slot 31 for the cable to pass through, and the slot 31 is located below the servo's adjustment lever.

[0041] In this embodiment, the slot 31 is funnel-shaped. Because the existing adjusting cable has a metal sheath on the outside, the funnel-shaped slot 31 makes it easy to place the adjusting cable into the slot 31, and at the same time, it can better limit and fix the adjusting cable at the wider part of the funnel opening.

[0042] In this embodiment, the cable frame 30 is L-shaped, and threaded holes 32 are provided on the vertical part of the cable frame 30 corresponding to the position of each fixing hole 27. Each threaded hole 32 is provided with a third fixing bolt 33.

[0043] The role and effect of the embodiments

[0044] According to the aviation unmanned aerial vehicle (UAV) engine throttle valve servo mounting bracket assembly involved in this utility model, by optimizing the bracket structure, the bracket structure is simple and compact, easy to assemble, and has high strength, thereby preventing the bracket from deforming during use. At the same time, because the bracket is arranged close to the engine throttle valve, it can reduce the cumulative control error of the throttle valve drive, and ensure the accuracy and consistency of the UAV engine throttle valve position control.

[0045] According to the aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly involved in this utility model, because the inner walls of the positioning hole, mounting hole and fixing hole are all provided with threads, they can be directly threadedly connected to the first fixing bolt, the second fixing bolt and the third fixing bolt, thereby eliminating the need for fixing nut workpieces, and thus making the structure of this utility model simple.

[0046] According to the aviation unmanned aerial vehicle engine throttle servo mounting bracket assembly involved in this utility model, because the servo bracket is slidably mounted on the mounting base through two U-shaped through slots, the position of the servo bracket can be freely adjusted within the through slots.

[0047] The above embodiments are preferred embodiments of this utility model and are not intended to limit the scope of protection of this utility model.

Claims

1. A mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle (UAV) engine, characterized in that, include: Mounting base frame, servo gear frame mounted on the mounting base frame, and cable bracket mounted on the servo gear frame. The mounting base includes multiple mounting blocks and a mounting beam. Each mounting block is mounted on one of the engines and positioned near the engine's output end. The mounting beam is detachably mounted on the mounting block, located above the engine, and its orientation is perpendicular to the engine's axial direction. The top wall of the mounting beam has two through holes, each containing a limiting bolt. Each limiting bolt is secured to the mounting beam by a nut. The servo mount is T-shaped and horizontally mounted on the mounting base. The servo mount has a vertical section and a horizontal section. The bottom wall of the vertical section fits against the top wall of the mounting beam. U-shaped through slots are formed on the outer walls of both sides of the vertical section, extending inwards. Two through slots are located above two through holes. The side walls of the horizontal section fit against the side walls of the mounting beam. A mounting hole for placing the servo is formed on the top wall of the horizontal section, specifically above the mounting beam. The cable support frame is detachably mounted on the servo frame, and the cable support frame has a slot for the cable to pass through. The slot is located below the servo's adjustment lever. The distance between the two limiting bolts is greater than the distance between the bottoms of the two through slots, but less than the distance between the openings of the two through slots.

2. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, The distance between the end of the limiting bolt and the top wall of the mounting beam is not less than the depth of the through groove, and the end diameter of the limiting bolt is greater than the width of the through groove.

3. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, Each mounting block has multiple threaded grooves on its top wall, and each mounting beam has a positioning hole corresponding to the position of each threaded groove. Each positioning hole has a first fixing bolt for fixing the mounting beam to the mounting block.

4. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, On the top wall of the horizontal section, above and below the mounting hole, there are multiple mounting holes for fixing the servo motor. Each mounting hole has an internal thread on its wall and a second fixing bolt in each mounting hole.

5. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, A fixing hole is provided on the top wall of the horizontal section and on one side of the mounting hole. The cable frame is L-shaped. A threaded hole is provided on the vertical part of the cable frame corresponding to the position of each fixing hole. A third fixing bolt is provided in each threaded hole.

6. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, The bottom wall of the mounting hole and the top wall of the vertical section are on the same horizontal plane.

7. The mounting bracket assembly for the throttle valve servo of an unmanned aerial vehicle engine according to claim 1, characterized in that: in, The slot is funnel-shaped.

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