Helicopter blade auxiliary installation clamp
By introducing components such as U-shaped support plates, linear motors and electric push rods into the helicopter blade auxiliary installation fixture, automatic loading and position adjustment are achieved, solving the problem of labor and low efficiency of traditional fixtures under single operation. Improves installation efficiency and safety.
Patent Information
- Application Number
- CN202420731437.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-10
- Publication Date
- 2024-12-13
- Estimated Expiration
- 2034-04-10
AI Technical Summary
Traditional helicopter blade assisted installation fixtures still require manual push and adjustment under single operation, and the weight of the blades is laborious and the installation efficiency is not high.
The design includes U-shaped support plates, linear motors, vertical electric push rods, auxiliary electric push rods and servo motors. Through these components, automatic loading and position adjustment can be achieved, reducing manual operation and improving installation efficiency.
The installation of helicopter blades has been achieved by a single person, reducing manpower investment, improving installation efficiency and safety, and reducing efforts.
Smart Images

Figure CN222157808U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of helicopter installation, in particular to an auxiliary installation fixture for helicopter blades. Background Art
[0002] The main rotor blade is an important part of the helicopter lift system and is also the most valuable part of the helicopter. Currently, the installation process is usually done manually, which requires two to three people to work together, which is time-consuming and laborious. Therefore, a helicopter blade auxiliary installation fixture is needed, which can be completed by one person. However, even if the traditional helicopter blade auxiliary installation fixture is operated by one person, it still needs to be manually pushed and loaded, and then the position is adjusted. In addition, the blade itself is very heavy, which is still quite laborious.
[0003] A Chinese patent document (authorization announcement number CN206476128U) discloses a helicopter blade auxiliary installation device, including a blade rack and a blade hanger. The blade rack is composed of two vertical poles and connecting rods fixedly connected to the two vertical poles at both ends. The tops of the two vertical poles are fixedly connected with blade support blocks with U-shaped grooves. The blade hanger includes a suspension rod and a cross bar fixedly connected to the bottom of the suspension rod. The two ends of the cross bar are fixedly connected with blade clamping devices. The beneficial effects of the utility model are as follows: the utility model saves manpower, changes the original three-person cooperation to one person's independent completion, meets the requirements of the production line, eliminates the tedious blade installation angle adjustment work, and greatly improves the helicopter blade installation efficiency. Although it can be operated by one person and improves efficiency, it also requires manual pushing and loading, and then adjusting the position. In addition, the blade itself is very heavy, which is still relatively laborious. Utility Model Content
[0004] The utility model aims to provide a helicopter blade auxiliary installation fixture to solve the problems raised in the background technology.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a helicopter blade auxiliary installation fixture, comprising a U-shaped support plate for supporting the helicopter blade and a pressure plate arranged above the support plate for fixing the helicopter blade, a T-shaped assembly plate is arranged below the support plate, a linear motor for providing transmission power for the installation of the helicopter blade is connected to the top of the assembly plate, and the moving part of the linear motor is connected and fixed to the support plate;
[0006] Three vertical electric push rods are connected to the bottom end of the assembly plate, and the bottom end of the vertical electric push rods is connected to a brake caster. The side of the fixed part of one of the vertical electric push rods is connected to an L-shaped limiting plate for limiting the helicopter blades. A plurality of auxiliary electric push rods are embedded in the side of the support plate, and the moving part of the auxiliary electric push rods is connected to an adjustment plate for adjusting the position of the helicopter blades.
[0007] As a preferred embodiment, a connecting rod is connected to the side of one of the vertical electric push rods, and an oblique connecting rod is connected between the connecting rod and the other two vertical electric push rods.
[0008] As a preferred embodiment, an inverted L-shaped auxiliary plate is connected to the top of the support plate, and an adjustable electric push rod is connected between the auxiliary plate and the pressure plate.
[0009] As a preferred embodiment, the inner top wall of the auxiliary plate is connected to a tilted camera and an infrared rangefinder via an oblique connecting block.
[0010] As a preferred embodiment, the inner wall of the support plate is rotatably connected to a plurality of equally spaced sliding rods, a vertical plate is welded to the side of the support plate, and a lifting electric push rod is connected to the side of the vertical plate.
[0011] As a preferred embodiment, the top end of the moving part of the lifting electric push rod is connected to a lifting lug, and the lifting lug is rotatably connected to a conveying wheel via a rotating shaft.
[0012] As a preferred embodiment, a servo motor is connected to the side of the lifting ear, and the output shaft of the servo motor passes through the lifting ear and is connected and fixed to one of the rotating shafts.
[0013] Compared with the prior art, the technical effects and advantages of the utility model are as follows:
[0014] The helicopter blade auxiliary installation fixture benefits from the design of the vertical electric push rod, the auxiliary electric push rod and the linear motor. The extension of the vertical electric push rod can adjust the height of the helicopter blade after loading. The extension of the auxiliary electric push rod enables the adjustment plate to adjust the position of the helicopter blade. The linear motor drives the support plate to move, and indirectly drives the helicopter blade to move toward the main helicopter device. Multiple drives save time and effort compared with manual processing.
[0015] Thanks to the design of the slide bar and the conveyor wheel, the slide bar can support the helicopter blades and ensure that the helicopter blades are moved during subsequent pushing. The servo motor drives the conveyor wheel to rotate and assists the helicopter blades to move toward the limit plate, which is more labor-saving than pushing.
[0016] Thanks to the design of the pressure plate and the adjustment electric push rod, the extension of the electric push rod is adjusted so that the pressure plate cooperates with the support plate to fix the helicopter blades;
[0017] The helicopter blade auxiliary installation fixture can assist the helicopter blade in adjustment and displacement, saving time and effort. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] In order to more clearly illustrate the specific implementation methods of the utility model or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.
[0019] Figure 1 It is a structural schematic diagram of the utility model;
[0020] Figure 2 This is a front view of the support plate of the utility model;
[0021] Figure 3 It is a rear view of the oblique connecting block of the utility model;
[0022] Figure 4 It is a structural schematic diagram of the jacking electric push rod of the utility model.
[0023] Description of reference numerals:
[0024] In the figure: 1. Support plate; 2. Press plate; 3. Assembly plate; 4. Linear motor; 5. Vertical electric push rod; 6. Brake caster; 7. Limit plate; 8. Auxiliary electric push rod; 9. Adjustment plate; 10. Connecting rod; 11. Oblique connecting rod; 12. Auxiliary plate; 13. Adjustment electric push rod; 14. Oblique connecting block; 15. Camera; 16. Infrared rangefinder; 17. Sliding rod; 18. Lifting electric push rod; 19. Lifting ear; 20. Conveyor wheel; 21. Servo motor. DETAILED DESCRIPTION
[0025] In the following description, a large number of specific details are given to provide a more thorough understanding of the utility model. However, it is obvious to those skilled in the art that the utility model can be implemented without one or more of these details. In other examples, in order to avoid confusion with the utility model, some technical features known in the art are not described.
[0026] Unless otherwise defined, the directions of up, down, left, right, front, back, inside and outside involved in this document are based on the directions of up, down, left, right, front, back, inside and outside in the figures shown in the present utility model, and are explained here together.
[0027] The connection method can be bonding, welding, bolt connection, etc., depending on actual needs.
[0028] In order to adjust and move the energy level blades later, such as Figures 1 to 4The helicopter blade auxiliary installation fixture shown in the figure includes a U-shaped support plate 1 for supporting the helicopter blade and a pressure plate 2 arranged above the support plate 1 for fixing the helicopter blade. The size and shape of the pressure plate 2 are not subject to the figure and are fine-tuned according to actual needs. A T-shaped assembly plate 3 is arranged below the support plate 1. The top of the assembly plate 3 is connected to a linear motor 4 for providing transmission power for the installation of the helicopter blade. The moving part of the linear motor 4 is connected and fixed to the support plate 1, and the auxiliary electric push rod 8 is controlled to extend so that the pressure plate 2 fixes the helicopter blade, and the linear motor 4 is controlled to drive the support plate 1. Move toward the power equipment of the helicopter, and then the staff installs the helicopter blades; three vertical electric push rods 5 are connected to the bottom end of the assembly plate 3, and the side of the fixed part of one of the vertical electric push rods 5 is connected to an L-shaped limiting plate 7 for limiting the helicopter blades, and a plurality of auxiliary electric push rods 8 are embedded in the side of the support plate 1, and the moving part of the auxiliary electric push rods 8 is connected to an adjustment plate 9 for adjusting the position of the helicopter blades. The auxiliary electric push rods 8 are controlled to extend so that the adjustment plate 9 adjusts the position of the helicopter blades, and the auxiliary electric push rods 8 at the specified position are selected for adjustment according to actual needs.
[0029] In order to ensure the overall stability, the bottom end of the vertical electric push rod 5 is connected to a brake caster 6, a connecting rod 10 is connected to the side of one of the vertical electric push rods 5, and an oblique connecting rod 11 is connected between the connecting rod 10 and the other two vertical electric push rods 5.
[0030] In order to meet the needs of use, an inverted L-shaped auxiliary plate 12 is connected to the top of the support plate 1, an adjustable electric push rod 13 is connected between the auxiliary plate 12 and the pressure plate 2, and the inner top wall of the auxiliary plate 12 is connected to an inclined camera 15 and an infrared rangefinder 16 through a diagonal connecting block 14. The camera 15 records the operation and the infrared rangefinder 16 measures the distance, so that the staff can understand the situation in real time.
[0031] In order to assist the transportation and displacement of the helicopter blades, the inner wall of the support plate 1 is rotatably connected to a plurality of equally spaced slide bars 17, a vertical plate is welded to the side of the support plate 1, a lifting electric push rod 18 is connected to the side of the vertical plate, a lifting ear 19 is connected to the top of the moving part of the lifting electric push rod 18, the lifting ear 19 is rotatably connected to the conveying wheel 20 through a rotating shaft, a servo motor 21 is connected to the side of the lifting ear 19, the output shaft of the servo motor 21 passes through the lifting ear 19 and is fixedly connected to one of the rotating shafts, the helicopter blade to be installed is placed on the slide bar 17, and then the lifting electric push rod 18 is controlled to extend so that the conveying wheel 20 lifts the helicopter blade and moves up, the servo motor 21 is turned on, the servo motor 21 assists the conveying wheel 20 to rotate, drives the helicopter blade to move toward the limit plate 7, and after it hits the limit plate 7, the servo motor 21 is turned off, and the lifting electric push rod 18 is controlled to reset.
[0032] The linear motor 4, the vertical electric push rod 5, the auxiliary electric push rod 8, the camera 15, the infrared rangefinder 16, the lifting electric push rod 18 and the servo motor 21 are all set as the prior art. The working principle, size and model are irrelevant to the function of the present application, so they are not described in detail. The control method of the present invention is controlled by a controller. The control circuit of the controller can be realized by simple programming by technicians in this field. The provision of power is also common knowledge in this field. The present invention is mainly used to protect mechanical devices, so the present invention no longer explains the control method and circuit connection in detail.
[0033] How it works
[0034] The helicopter blade auxiliary installation fixture places the helicopter blade to be installed on the slide bar 17, then controls the lifting electric push rod 18 to extend, so that the conveying wheel 20 lifts the helicopter blade and moves it upward, turns on the servo motor 21, and the servo motor 21 assists the conveying wheel 20 to rotate, driving the helicopter blade to move toward the limit plate 7. After it abuts against the limit plate 7, turns off the servo motor 21, controls the lifting electric push rod 18 to reset, and controls the auxiliary electric push rod 8 to extend, so that the adjustment plate 9 adjusts the position of the helicopter blade, and then controls the auxiliary electric push rod 8 to extend, so that the pressure plate 2 fixes the helicopter blade, and controls the linear motor 4 to drive the support plate 1 to move toward the power equipment of the helicopter, and then the staff installs the helicopter blade.
[0035] It should be noted that, in this article, relational terms such as one and two are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions. The sentence "comprises an element defined by ... does not exclude the existence of other identical elements in the process, method, article or device including the element".
[0036] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A helicopter blade auxiliary installation fixture, comprising a U-shaped support plate (1) for supporting the helicopter blade and a pressing plate (2) arranged above the support plate (1) for fixing the helicopter blade, characterized in that: A T-shaped assembly plate (3) is arranged below the support plate (1), and a linear motor (4) for providing transmission power for helicopter blade installation is connected to the top of the assembly plate (3), and a moving part of the linear motor (4) is connected and fixed to the support plate (1); The bottom end of the assembly plate (3) is connected to three vertical electric push rods (5), and the bottom end of the vertical electric push rods (5) is connected to a brake caster (6). The side of the fixed part of one of the vertical electric push rods (5) is connected to an L-shaped limiting plate (7) for limiting the position of the helicopter blades. The side of the support plate (1) is embedded with a plurality of auxiliary electric push rods (8), and the movable part of the auxiliary electric push rods (8) is connected to an adjustment plate (9) for adjusting the position of the helicopter blades.
2. The helicopter blade auxiliary installation fixture according to claim 1, characterized in that: A connecting rod (10) is connected to the side of one of the vertical electric push rods (5), and an oblique connecting rod (11) is connected between the connecting rod (10) and the other two vertical electric push rods (5).
3. The helicopter blade auxiliary installation fixture according to claim 1, characterized in that: An inverted L-shaped auxiliary plate (12) is connected to the top end of the support plate (1), and an adjustable electric push rod (13) is connected between the auxiliary plate (12) and the pressure plate (2).
4. The helicopter blade auxiliary installation fixture according to claim 3 is characterized in that: The inner top wall of the auxiliary plate (12) is connected to an inclined camera (15) and an infrared rangefinder (16) via an oblique connecting block (14).
5. The helicopter blade auxiliary installation fixture according to claim 3, characterized in that: The inner wall of the support plate (1) is rotatably connected to a plurality of equally spaced sliding rods (17), a vertical plate is welded to the side of the support plate (1), and a lifting electric push rod (18) is connected to the side of the vertical plate.
6. The helicopter blade auxiliary installation fixture according to claim 5, characterized in that: The top end of the moving part of the lifting electric push rod (18) is connected with a lifting ear (19), and the lifting ear (19) is rotatably connected with a conveying wheel (20) via a rotating shaft.
7. The helicopter blade auxiliary installation fixture according to claim 6, characterized in that: A servo motor (21) is connected to the side of the lifting ear (19), and an output shaft of the servo motor (21) passes through the lifting ear (19) and is connected and fixed to one of the rotating shafts.
