Glue joint tool for helicopter tail rotor supporting piece

Abstract

The invention discloses a glue joint tool for helicopter tail rotor supporting pieces, which comprises a base plate, a first positioning part is arranged on the base plate and used for positioning a flexible beam on the base plate, and a second positioning part and a third positioning part are further arranged on the base plate and used for positioning a first supporting piece and a second supporting piece on preset mounting positions on the flexible beam respectively. During use, the flexible beam is positioned on the base plate through the first positioning part, the position of the flexible beam on the base plate is fixed, and then the first supporting piece and the second supporting piece are positioned and glued to the pre-installation position of the flexible beam through the second positioning part and the third positioning part respectively. Therefore, the tool not only can ensure the mounting precision requirement of the supporting piece and the flexible beam, but also can improve the assembly efficiency.

Description

Technical Field

[0001] The present invention relates to the technical field of helicopter tail rotor assembly tooling, and more specifically, to an adhesive tool for a helicopter tail rotor support member. Background Art

[0002] The helicopter tail rotor is a component used to balance the counter torque and control the helicopter's heading. Generally, the structure of the tail rotor is as Figures 1-2 shown. The tail rotor includes a flexible beam 100 connected to the helicopter drive component, a support member 200 mounted on the flexible beam 100, and blades (not shown) mounted on both ends of the flexible beam. The support member 200 includes a first support member 2001 and a second support member 2002. The first support member 2001 and the second support member 2002 are respectively sleeved with a sealing rubber sleeve 400 on the sleeves 300 of the two side blades. Among them, the support member 200 is an important part of the tail rotor blade, which plays a role in supporting the sealing rubber sleeve 400 and the sealing sleeve 300. Both the first support member 2001 and the second support member 2002 are made of non-metallic materials, and each includes an upper support plate 2003 and a lower support plate 2004 that are fitted together up and down and fixed by connecting screws 500. After applying glue to the bottom end of the upper support plate 2003 and the top end of the lower support plate 2004, they need to be adhesively bonded to the upper surface and the lower surface of the flexible beam 100 respectively. The installation position tolerance of the bonding position of the upper support plate 2003 and the lower support plate 2004 on the flexible beam 100 is required to be 0.01, and the installation accuracy requirement is relatively high.

[0003] Currently, for the installation of the existing support member adhesively bonded to the flexible beam, usually, a worker uses a measuring ruler to measure and mark the installation positions of the upper support plate and the lower support plate on the upper and lower surfaces of the flexible beam, and then manually adhesively bonds the upper support plate and the lower support plate according to the marked positions. However, this manual measurement and marking method has a large human subjective factor, often resulting in the installation accuracy of the support member not meeting the predetermined requirements, a high rejection rate, and a low assembly efficiency.

[0004] Therefore, how to provide an adhesive tool for a helicopter tail rotor support member that can not only ensure the installation accuracy requirements of the support member and the flexible beam but also improve the assembly efficiency is an urgent problem to be solved by those skilled in the art. Summary of the Invention

[0005] In view of this, the present invention provides an adhesive tool for a helicopter tail rotor support member that can not only ensure the installation accuracy requirements of the support member and the flexible beam but also improve the assembly efficiency.

[0006] To achieve the above object, the present invention adopts the following technical solutions:

[0007] An adhesive bonding tool for a helicopter tail rotor support member, comprising: a substrate, on which a first positioning portion is provided for positioning a flexible beam on the substrate, and a second positioning portion and a third positioning portion are also provided on the substrate for respectively positioning a first support member and a second support member at predetermined installation positions on the flexible beam.

[0008] As can be seen from the above technical solution, compared with the prior art, the present invention discloses an adhesive bonding tool for a helicopter tail rotor support member. When in use, the flexible beam is positioned on the substrate through the first positioning portion to fix the position of the flexible beam on the substrate, and then the first support member and the second support member are respectively positioned and adhesively bonded at the pre-installation positions on the flexible beam through the second positioning portion and the third positioning portion. Therefore, this tool can not only ensure the installation accuracy requirements of the support member and the flexible beam, but also improve the assembly efficiency.

[0009] Further, the first positioning portion includes:

[0010] A middle supporting boss, the bottom end of the middle supporting boss is fixedly connected to the middle of the top surface of the substrate, and a positioning mandrel is detachably installed on the top surface of the middle supporting boss, and the central hole on the flexible beam is sleeved on the positioning mandrel;

[0011] A left supporting boss, the bottom end of the left supporting boss is fixedly connected to the left edge of the top surface of the substrate, and an upper left positioning protrusion and a lower left positioning protrusion are fixedly arranged at intervals up and down on the top surface of the left supporting boss, and the side surface of the lower left positioning protrusion facing the upper left positioning protrusion is a first lateral positioning surface;

[0012] A right supporting boss, the bottom end of the right supporting boss is fixedly connected to the right edge of the top surface of the substrate, and an upper right positioning protrusion and a lower right positioning protrusion are fixedly arranged at intervals up and down on the top surface of the right supporting boss, and the side surface of the upper right positioning protrusion facing the lower right positioning protrusion is a second lateral positioning surface;

[0013] A lateral tightening screw, which is screwed on the outer end of the lower right positioning protrusion and is used to abut against the lower right side surface of the flexible beam placed on the middle supporting boss, the left supporting boss and the right supporting boss, so that the upper right side surface and the lower left side surface of the flexible beam respectively abut against the second lateral positioning surface and the first lateral positioning surface.

[0014] The beneficial effects of adopting the above technical solution are as follows: The flexible beam is sleeved on the positioning mandrel on the substrate through the central hole thereon to achieve the preliminary positioning of the flexible beam. Then, the lateral tightening screw is rotated so that the lateral tightening screw abuts against the lower right side surface of the beam of the flexible beam, and then the flexible beam is pushed, so that the upper right side surface and the lower left side surface of the beam of the flexible beam respectively abut against the second lateral positioning surface and the first lateral positioning surface, and finally the position of the flexible beam on the substrate is fixed. Then, the first support member and the second support member are respectively positioned and adhesively bonded at the pre-installed positions of the flexible beam through the second positioning portion and the third positioning portion. Therefore, the positioning structure of the flexible beam is simple and easy to operate.

[0015] Further, the second positioning portion includes: an upper left L-shaped plate, an upper left tightening screw, a lower left L-shaped plate, and a lower left tightening screw;

[0016] One side of the upper long plate of the upper left L-shaped plate is fixedly connected to one side of the upper left positioning convex block. The left side surface of the upper left positioning convex block is flush with the upper left side surface of the substrate, and the two together form an upper left positioning surface. The upper left tightening screw is screwed on the upper short plate of the upper left L-shaped plate, and an upper left smooth surface pressing block is fixed at the tail end of the upper left tightening screw;

[0017] One side of the lower long plate of the lower left L-shaped plate is fixedly connected to one side of the lower left positioning convex block. The left side surface of the lower left positioning convex block is flush with the lower left side surface of the substrate, and the two together form a lower left positioning surface. The lower left tightening screw is screwed on the lower short plate of the lower left L-shaped plate, and a lower left smooth surface pressing block is fixed at the tail end of the lower left tightening screw;

[0018] By adjusting the upper left tightening screw and the lower left tightening screw, the upper left smooth surface pressing block and the lower left smooth surface pressing block thereon respectively abut against the left side surface of the first support member, so that the right side surface of the first support member is positioned and pressed against the upper left positioning surface and the lower left positioning surface;

[0019] The third positioning portion includes: an upper right L-shaped plate, an upper right tightening screw, a lower right L-shaped plate, and a lower right tightening screw;

[0020] One side of the upper long plate of the upper right L-shaped plate is fixedly connected to one side of the upper right positioning convex block. The right side surface of the upper right positioning convex block is flush with the upper right side surface of the substrate, and the two together form an upper right positioning surface. The upper right tightening screw is screwed on the upper short plate of the upper right L-shaped plate, and an upper right smooth surface pressing block is fixed at the tail end of the upper right tightening screw;

[0021] One side of the lower right long plate of the lower right L-shaped plate is fixedly connected to one side of the lower right positioning convex block. The right side surface of the lower right positioning convex block is flush with the lower right side surface of the substrate, and the two together form a lower right positioning surface. A lower right tightening screw is screwed on the lower right short plate of the lower right L-shaped plate, and a lower right smooth surface pressing block is fixed at the tail end of the lower right tightening screw.

[0022] By adjusting the upper right tightening screw and the lower right tightening screw, the upper right smooth surface pressing block and the lower right smooth surface pressing block thereon are respectively abutted against the right side surface of the second support member, so that the left side surface of the second support member is positioned and pressed on the upper right positioning surface and the lower right positioning surface.

[0023] The beneficial effects of adopting the above technical solutions are as follows: After the flexible beam is positioned, the bottom end surface of the upper support plate and the top end surface of the lower support plate of the first support member are coated with glue, and then they are respectively placed on the top end surface and the bottom end surface on one side of the flexible beam. Then, the upper support plate and the lower support plate are pre-connected by connecting screws. Then, the upper left tightening screw and the lower left tightening screw are respectively rotated to drive the upper left smooth surface pressing block and the lower left smooth surface pressing block to push the combined position of the upper support plate and the lower support plate, so that the right side surfaces of the upper support plate and the lower support plate are both positioned and pressed on the upper left positioning surface and the lower left positioning surface. Then, the connecting screws are tightened to firmly fix the upper support plate and the lower support plate on the flexible beam. Then, the second support member is installed by the same method, and then cured, and the gluing is completed. Therefore, this tool realizes the precise and rapid positioning and installation of the support member on the flexible beam through the corresponding tightening screws and the corresponding positioning surfaces, without manual measurement of the installation position, and improves the efficiency of gluing and assembling the support member and the flexible beam.

[0024] Further, a positioning hole is provided on the top end surface of the middle supporting convex platform. The positioning core shaft includes: a positioning disk and a plug-in shaft. The bottom end surface of the positioning disk is fixedly connected to one end of the plug-in shaft, the plug-in shaft is plugged into the positioning hole, and the central hole is sleeved on the positioning disk.

[0025] The beneficial effects of adopting the above technical solutions are as follows: The positioning core shaft and the substrate are connected by a plug-in structure, which is conducive to the rapid positioning and assembly of the positioning core shaft and the substrate.

[0026] Further, the positioning disk is fixed on the substrate by a first fixing screw.

[0027] The beneficial effects of adopting the above technical solutions are as follows: It improves the installation firmness of the positioning core shaft on the substrate, avoids the rotation of the positioning core shaft on the substrate, and affects the positioning and installation of the flexible beam.

[0028] Further, it further includes a pressing plate. The pressing plate is fixed on the positioning disk by a second fixing screw, and the bottom end surface of the pressing plate is pressed against the top end surface of the flexible beam.

[0029] The beneficial effects of adopting the above technical solution are as follows: The pressing plate can further improve the installation stability of the flexible beam on the substrate.

[0030] Furthermore, it also includes a plurality of supporting feet fixed on the bottom end surface of the substrate.

[0031] The beneficial effects of adopting the above technical solution are as follows: The supporting feet can raise the substrate to a certain height, which is convenient for the installation of the lower supporting plate.

[0032] Furthermore, a plurality of threaded holes are evenly formed on the top end surface of the substrate, and threaded columns are fixed at the top ends of the plurality of supporting feet, and the plurality of threaded columns are respectively threadedly fixed with the plurality of threaded holes.

[0033] The beneficial effects of adopting the above technical solution are as follows: It is easy to disassemble and assemble the supporting feet.

[0034] Furthermore, a weight-reducing hole is formed on the substrate.

[0035] The beneficial effects of adopting the above technical solution are as follows: The weight of the substrate can be reduced, which is convenient for the movement and carrying of the tool. BRIEF DESCRIPTION OF THE DRAWINGS

[0036] In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required for the description of the embodiments or the prior art. Obviously, the drawings in the following description are only the embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained according to the provided drawings without creative efforts.

[0037] Figure 1 It is a schematic structural diagram of the tail rotor provided by the present invention.

[0038] Figure 2 For Figure 1 The sectional structural schematic diagram of the middle section A - A.

[0039] Figure 3 It is a front view structural schematic diagram of an adhesive tool for a helicopter tail rotor support provided by the present invention.

[0040] Figure 4 It is a top view structural schematic diagram of an adhesive tool for a helicopter tail rotor support provided by the present invention.

[0041] Figure 5 It is a schematic structural diagram of the substrate provided by the present invention.

[0042] Figure 6 It is a schematic structural diagram of the supporting foot provided by the present invention. DETAILED DESCRIPTION OF THE INVENTION

[0043] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0044] As Figures 1-6 shown, an adhesive bonding tool for a helicopter tail rotor support member according to an embodiment of the present invention includes: a substrate 1, on which a first positioning portion 2 is provided for positioning a flexible beam 100 on the substrate 1. A second positioning portion 3 and a third positioning portion 4 are further provided on the substrate 1 for respectively positioning a first support member 2001 and a second support member 2002 at predetermined installation positions on the flexible beam 100.

[0045] Specifically, the first positioning portion 2 includes:

[0046] A middle supporting boss 21, the bottom end of the middle supporting boss 21 is fixedly connected to the middle of the top surface of the substrate 1, and a positioning mandrel 22 is detachably installed on the top surface of the middle supporting boss 21. The central hole 1001 on the flexible beam 100 is sleeved on the positioning mandrel 22;

[0047] A left supporting boss 23, the bottom end of the left supporting boss 23 is fixedly connected to the left edge of the top surface of the substrate 1. An upper left positioning convex block 24 and a lower left positioning convex block 25 are fixedly arranged at intervals up and down on the top surface of the left supporting boss 23. The side surface of the lower left positioning convex block 25 facing the upper left positioning convex block 24 is a first lateral positioning surface 251;

[0048] A right supporting boss 26, the bottom end of the right supporting boss 26 is fixedly connected to the right edge of the top surface of the substrate 1. An upper right positioning convex block 27 and a lower right positioning convex block 28 are fixedly arranged at intervals up and down on the top surface of the right supporting boss 26. The side surface of the upper right positioning convex block 27 facing the lower right positioning convex block 28 is a second lateral positioning surface 271;

[0049] A lateral tightening screw 29, which is screwed on the outer end of the lower right positioning convex block 28 and is used to abut against the lower right side surface 1002 of the flexible beam 100 placed on the middle supporting boss 21, the left supporting boss 23, and the right supporting boss 26, so that the upper right side surface 1003 and the lower left side surface 1004 of the flexible beam 100 respectively abut against the second lateral positioning surface 271 and the first lateral positioning surface 251.

[0050] The second positioning portion 3 includes: an upper left L-shaped plate 31, an upper left tightening screw 32, a lower left L-shaped plate 33, and a lower left tightening screw 34;

[0051] One side of the upper left long plate 311 of the upper left L-shaped plate 31 is fixedly connected to one side of the upper left positioning projection 24. The left side surface of the upper left positioning projection 24 is flush with the upper left side surface of the substrate 1, and the two together form an upper left positioning surface 241. An upper left tightening screw 32 is screwed on the upper left short plate 312 of the upper left L-shaped plate 31, and an upper left smooth surface pressing block 35 is fixed to the tail end of the upper left tightening screw 32;

[0052] One side of the lower left long plate 331 of the lower left L-shaped plate 33 is fixedly connected to one side of the lower left positioning projection 25. The left side surface of the lower left positioning projection 25 is flush with the lower left side surface of the substrate 1, and the two together form a lower left positioning surface 252. A lower left tightening screw 34 is screwed on the lower left short plate 332 of the lower left L-shaped plate 33, and a lower left smooth surface pressing block 36 is fixed to the tail end of the lower left tightening screw 34;

[0053] By adjusting the upper left tightening screw 32 and the lower left tightening screw 34, the upper left smooth surface pressing block 35 and the lower left smooth surface pressing block 36 on them are respectively abutted against the left side surface of the first support member 2001, so that the right side surface of the first support member 2001 is positioned and pressed on the upper left positioning surface 241 and the lower left positioning surface 252;

[0054] The third positioning portion 4 includes: an upper right L-shaped plate 41, an upper right tightening screw 42, a lower right L-shaped plate 43, and a lower right tightening screw 44;

[0055] One side of the upper right long plate 411 of the upper right L-shaped plate 41 is fixedly connected to one side of the upper right positioning projection 27. The right side surface of the upper right positioning projection 27 is flush with the upper right side surface of the substrate 1, and the two together form an upper right positioning surface 272. An upper right tightening screw 42 is screwed on the upper right short plate 412 of the upper right L-shaped plate 41, and an upper right smooth surface pressing block 45 is fixed to the tail end of the upper right tightening screw 42;

[0056] One side of the lower right long plate 431 of the lower right L-shaped plate 43 is fixedly connected to one side of the lower right positioning projection 28. The right side surface of the lower right positioning projection 28 is flush with the lower right side surface of the substrate 1, and the two together form a lower right positioning surface 281. A lower right tightening screw 44 is screwed on the lower right short plate 432 of the lower right L-shaped plate 43, and a lower right smooth surface pressing block 46 is fixed to the tail end of the lower right tightening screw 44;

[0057] By adjusting the upper right tightening screw 42 and the lower right tightening screw 44, the upper right smooth surface pressing block 45 and the lower right smooth surface pressing block 46 on them are respectively abutted against the right side surface of the second support member 2002, so that the left side surface of the second support member 2002 is positioned and pressed on the upper right positioning surface 272 and the lower right positioning surface 281.

[0058] In the above embodiments, a positioning hole 211 is formed on the top surface of the middle supporting boss 21. The positioning mandrel 22 includes a positioning disk 221 and an insertion shaft 222. The bottom end surface of the positioning disk 221 is fixedly connected to one end of the insertion shaft 222. The insertion shaft 222 is inserted into the positioning hole 211, and the central hole 1001 is sleeved on the positioning disk 221.

[0059] The positioning disk 221 is fixed on the substrate 1 by the first fixing screw 5.

[0060] In some embodiments, the bonding tool for the helicopter tail rotor support further includes a pressing plate 6. The pressing plate 6 is fixed on the positioning disk 221 by the second fixing screw 7, and the bottom end surface of the pressing plate 6 is press-connected to the top surface of the flexible beam 100.

[0061] In other embodiments, the bonding tool for the helicopter tail rotor support further includes a plurality of feet 8 fixed on the bottom end surface of the substrate 1.

[0062] Specifically, a plurality of threaded holes 101 are uniformly formed on the top surface of the substrate 1. Threaded posts 81 are fixed to the tops of the plurality of feet 8, and the plurality of threaded posts 81 are respectively threadedly fixed to the plurality of threaded holes 101.

[0063] Of course, in the above embodiments, a weight-reducing hole 102 is formed on the substrate 1.

[0064] The steps of bonding the upper support plate and the lower support plate to the flexible beam using this tool are as follows:

[0065] First, the flexible beam is sleeved on the positioning mandrel on the substrate through the central hole thereon to achieve preliminary positioning of the flexible beam. Then, the lateral tightening screw is rotated so that the lateral tightening screw abuts against the lower right side surface of the flexible beam, and then the flexible beam is pushed, so that the upper right side surface and the lower left side surface of the flexible beam respectively abut against the second lateral positioning surface and the first lateral positioning surface, and finally the position of the flexible beam on the substrate is fixed. Then, the bottom end surface of the upper support plate of the first support member and the top end surface of the lower support plate are coated with glue, and then they are respectively placed on the top surface and the bottom surface on one side of the flexible beam. Then, the upper support plate and the lower support plate are pre-connected by the connecting screw. Then, the upper left tightening screw and the lower left tightening screw are respectively rotated to drive the upper left smooth pressing block and the lower left smooth pressing block to push the joint position of the upper support plate and the lower support plate, so that the right side surfaces of the upper support plate and the lower support plate are respectively positioned and press-connected to the upper left positioning surface and the lower left positioning surface. Then, the connecting screw is tightened to firmly fix the upper support plate and the lower support plate on the flexible beam. Then, the second support member is installed using the same method, and then cured, and the bonding is completed.

[0066] Therefore, this tool can meet the installation accuracy requirements of the support member and the flexible beam through the positioning part, without manual measurement of the installation position, which can greatly improve the assembly efficiency and reduce the assembly rejection rate.

[0067] The various embodiments in this specification are described in a progressive manner. Each embodiment focuses on the differences from other embodiments. For the same or similar parts among the embodiments, reference can be made to each other. For the devices disclosed in the embodiments, since they correspond to the methods disclosed in the embodiments, the description is relatively simple. For the relevant parts, reference can be made to the description in the method section.

[0068] The above description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be obvious to those skilled in the art. The general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to these embodiments shown herein, but rather to the broadest scope consistent with the principles and novel features disclosed herein.

Claims

1. An adhesive tool for a helicopter tail rotor support member, characterized in that, Comprising: A substrate (1) is provided with a first positioning portion (2) thereon for positioning a flexible beam (100) on the substrate (1). The substrate (1) is further provided with a second positioning portion (3) and a third positioning portion (4) for positioning a first support member (2001) and a second support member (2002) respectively at predetermined installation positions on the flexible beam (100).

2. The bonding tool for a helicopter tail rotor support member according to claim 1, wherein The first positioning portion (2) comprises: A middle supporting boss (21), the bottom end of the middle supporting boss (21) is fixedly connected to the middle of the top surface of the substrate (1). A positioning mandrel (22) is detachably installed on the top surface of the middle supporting boss (21), and a central hole (1001) on the flexible beam (100) is sleeved on the positioning mandrel (22); A left supporting boss (23), the bottom end of the left supporting boss (23) is fixedly connected to the left edge of the top surface of the substrate (1). An upper left positioning protrusion (24) and a lower left positioning protrusion (25) are fixedly arranged at intervals up and down on the top surface of the left supporting boss (23). The side surface of the lower left positioning protrusion (25) facing the upper left positioning protrusion (24) is a first lateral positioning surface (251); A right supporting boss (26), the bottom end of the right supporting boss (26) is fixedly connected to the right edge of the top surface of the substrate (1). An upper right positioning protrusion (27) and a lower right positioning protrusion (28) are fixedly arranged at intervals up and down on the top surface of the right supporting boss (26). The side surface of the upper right positioning protrusion (27) facing the lower right positioning protrusion (28) is a second lateral positioning surface (271); A lateral tightening screw (29) is screwed on the outer end of the lower right positioning protrusion (28) and is used to abut against the lower right side surface (1002) of the flexible beam (100) placed on the middle supporting boss (21), the left supporting boss (23), and the right supporting boss (26), so that the upper right side surface (1003) and the lower left side surface (1004) of the flexible beam (100) are respectively abutted against the second lateral positioning surface (271) and the first lateral positioning surface (251).

3. The bonding tool for a helicopter tail rotor support member according to claim 2, characterized in that, The second positioning portion (3) comprises: an upper left L-shaped plate (31), an upper left tightening screw (32), a lower left L-shaped plate (33), and a lower left tightening screw (34); One side of the upper long plate (311) of the upper left L-shaped plate (31) is fixedly connected to one side of the upper left positioning protrusion (24). The left side surface of the upper left positioning protrusion (24) is flush with the upper left side surface of the substrate (1), and the two together form an upper left positioning surface (241). The upper left tightening screw (32) is screwed on the upper short plate (312) of the upper left L-shaped plate (31), and the tail end of the upper left tightening screw (32) is fixed with an upper left smooth pressing block (35); One side of the lower left long plate (331) of the lower left L-shaped plate (33) is fixedly connected to one side of the lower left positioning projection (25). The left side surface of the lower left positioning projection (25) is flush with the lower left side surface of the substrate (1), and the two together form a lower left positioning surface (252). A lower left tightening screw (34) is screwed on the lower left short plate (332) of the lower left L-shaped plate (33), and a lower left smooth surface pressing block (36) is fixed to the tail end of the lower left tightening screw (34); By adjusting the upper left tightening screw (32) and the lower left tightening screw (34), the upper left smooth surface pressing block (35) and the lower left smooth surface pressing block (36) thereon are respectively abutted against the left side surface of the first support member (2001), so that the right side surface of the first support member (2001) is positioned and pressed against the upper left positioning surface (241) and the lower left positioning surface (252); The third positioning portion (4) includes: an upper right L-shaped plate (41), an upper right tightening screw (42), a lower right L-shaped plate (43), and a lower right tightening screw (44); One side of the upper right long plate (411) of the upper right L-shaped plate (41) is fixedly connected to one side of the upper right positioning projection (27). The right side surface of the upper right positioning projection (27) is flush with the upper right side surface of the substrate (1), and the two together form an upper right positioning surface (272). An upper right tightening screw (42) is screwed on the upper right short plate (412) of the upper right L-shaped plate (41), and an upper right smooth surface pressing block (45) is fixed to the tail end of the upper right tightening screw (42); One side of the lower right long plate (431) of the lower right L-shaped plate (43) is fixedly connected to one side of the lower right positioning projection (28). The right side surface of the lower right positioning projection (28) is flush with the lower right side surface of the substrate (1), and the two together form a lower right positioning surface (281). A lower right tightening screw (44) is screwed on the lower right short plate (432) of the lower right L-shaped plate (43), and a lower right smooth surface pressing block (46) is fixed to the tail end of the lower right tightening screw (44); By adjusting the upper right tightening screw (42) and the lower right tightening screw (44), the upper right smooth surface pressing block (45) and the lower right smooth surface pressing block (46) thereon are respectively abutted against the right side surface of the second support member (2002), so that the left side surface of the second support member (2002) is positioned and pressed against the upper right positioning surface (272) and the lower right positioning surface (281).

4. The bonding tool for a helicopter tail rotor support according to claim 2 or 3, characterized in that, A positioning hole (211) is formed on the top end surface of the middle supporting convex platform (21). The positioning core shaft (22) includes: a positioning disk (221) and a plugging shaft (222). The bottom end surface of the positioning disk (221) is fixedly connected to one end of the plugging shaft (222). The plugging shaft (222) is plugged and connected with the positioning hole (211), and the central hole (1001) is sleeved on the positioning disk (221).

5. The bonding tool for a helicopter tail rotor support according to claim 4, characterized in that The positioning disk (221) is fixed to the substrate (1) by a first fixing screw (5).

6. The bonding tool for a helicopter tail rotor support according to claim 4, characterized in that, It further includes a pressing plate (6), and the pressing plate (6) is fixed on the positioning disk (221) by a second fixing screw (7), and the bottom end surface of the pressing plate (6) is in press contact with the top end surface of the flexible beam (100).

7. A bonding tool for a helicopter tail rotor support member according to any one of claims 1-3, 5-6, characterized in that It further includes a plurality of feet (8) fixed on the bottom end surface of the substrate (1).

8. The bonding tool for a helicopter tail rotor support member according to claim 7, characterized in that, A plurality of threaded holes (101) are uniformly formed on the top end surface of the substrate (1), the top ends of the plurality of feet (8) are respectively fixed with threaded posts (81), and the plurality of threaded posts (81) are respectively threadedly fixed with the plurality of threaded holes (101).

9. A bonding tool for a helicopter tail rotor support member according to any one of claims 1-3, 5-6, characterized in that, A weight-reducing hole (102) is formed on the substrate (1).

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