Airplane rudder steering engine test bed convenient to move and position

Abstract

The utility model discloses an airplane rudder steering engine test bed convenient to move and position, which comprises a supporting mechanism and an adjusting mechanism, the supporting mechanism comprises a U-shaped base, a plurality of springs embedded in the two side walls of the interior of the U-shaped base, sliding blocks connected with the bottom ends of the springs, lifting plates connected between every two adjacent sliding blocks and a transverse table connected between the two lifting plates, and the two side walls of the interior of the U-shaped base are each provided with two sliding grooves suitable for sliding block lifting. According to the lifting device, when the transverse table is controlled to be lifted to the required height, field technicians start the motor, then the gear rotates, under mechanical transmission, the toothed plate pushes the clamping sleeve and the gentle slope to move outwards, then the gentle slope extrudes the rolling wheels, then the rolling wheels and the two lifting plates are matched to achieve lifting of the transverse table, after the transverse table reaches the required height, the motor is closed, and the transverse table is lifted to the required height. And the transverse table can be lifted to any height and is stably fixed.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft rudder and steering gear testing, in particular to an aircraft rudder and steering gear testing platform which is convenient for movement and positioning. Background Art

[0002] The hydraulic servo uses hydraulic oil as its working medium and is a device that can turn the aircraft's rudder and maintain the rudder position. The electric hydraulic servo is reliable, easy to operate, lightweight and durable, highly economical, and easy to maintain and manage. As the actuator of the flight control system, the hydraulic servo is a complex system with a high degree of integration of mechanical, electrical and hydraulic functions. It is also a link with a high failure rate. Its performance and reliability directly affect the performance and reliability of the flight control system and even the entire aircraft.

[0003] Application number CN202320785289.7 discloses an adjustable hydraulic steering gear test bench, including a support base plate and other components. This adjustable hydraulic steering gear test bench positions the test platform plate by providing locating pins that cooperate with locating slots. This provides greater stability during testing and reduces the risk of shaking during testing, facilitating practical applications. However, there are certain issues with actual use. For example, once the locating pin is between the two locating slots, it cannot be plugged into the support side plate, thus preventing the test platform from being more stable. Utility Model Content

[0004] The utility model aims to solve one of the technical problems existing in the prior art or related technologies.

[0005] To this end, the technical solution adopted in this utility model is:

[0006] An aircraft rudder and steering gear test bench that is easy to move and position includes a supporting mechanism and an adjusting mechanism. The supporting mechanism includes a U-shaped base, multiple springs embedded in the inner side walls of the U-shaped base, a slider connected to the bottom end of the spring, a lifting plate connected between two adjacent sliders, and a cross platform connected between the two lifting plates. Two sliding grooves suitable for lifting and lowering the sliders are provided on the inner side walls of the U-shaped base, and an adjusting mechanism. The adjusting mechanism includes a motor embedded in the bottom of the U-shaped base, a gear sleeved on the outside of the motor output shaft, two tooth plates meshing with the gears, a clamping sleeve clamped with one end of the tooth plate, and a gentle slope installed on one side of the clamping sleeve, and the lifting plate is located at the top of the gentle slope.

[0007] By adopting the above technical solution, when controlling the horizontal platform to be lifted to the required height, the on-site technician starts the motor, and then the gears rotate. Under the mechanical transmission, the tooth plate pushes the sleeve and the gentle slope to move outward, and then the gentle slope squeezes the roller, and then multiple rollers and two lifting plates cooperate to realize the lifting of the horizontal platform. After the horizontal platform reaches the required height, the motor is turned off, and it can be lifted to any height, and the horizontal platform is fixed and stable.

[0008] In a preferred example, the present invention can be further configured as follows: the thickness of the gear is equal to the thickness of the tooth plate, and both are in contact with the bottom of the inner cavity of the U-shaped base.

[0009] In a preferred example, the present invention can be further configured as follows: the two tooth plates are vertically symmetrical with respect to the gear, and the sliding directions of the two tooth plates are opposite.

[0010] In a preferred example, the present invention can be further configured as follows: the top of the gentle slope is set as an inclined surface, and a convex plate is integrally formed at the outer end.

[0011] In a preferred example, the present invention can be further configured as follows: a socket suitable for inserting a toothed plate is provided on the inner side of the gentle slope.

[0012] In a preferred example, the present invention can be further configured as follows: two pads are installed at the bottom of the U-shaped base, the two pads are vertically symmetrical about the motor, and the thickness of the pads is greater than the height of the motor body.

[0013] In a preferred example, the present invention can be further configured as follows: two rollers are installed at the bottom of the lifting plate, and both rollers are attached to the top of the inclined surface.

[0014] By adopting the above technical solution, the beneficial effects achieved by the utility model are as follows:

[0015] In the utility model, when controlling the horizontal platform to be lifted to the required height, the on-site technician starts the motor, and then the gears rotate. Under the mechanical transmission, the tooth plate pushes the sleeve and the gentle slope to move outward, and then the gentle slope squeezes the roller, and then multiple rollers and two lifting plates cooperate to realize the lifting of the horizontal platform. After the horizontal platform reaches the required height, the motor is turned off, and it can be lifted to any height, and the horizontal platform is fixed and stable. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a three-dimensional diagram of the overall structure of the utility model;

[0017] Figure 2 This is a schematic diagram of the assembly of the overall structure of the support mechanism of the utility model;

[0018] Figure 3 This is a schematic diagram of the disassembled overall structure of the support mechanism of the utility model;

[0019] Figure 4 This is a schematic diagram of the adjustment mechanism of the utility model;

[0020] Figure 5 This is a bottom view of the adjustment mechanism of the utility model;

[0021] Figure 6This is a schematic diagram of the disassembly relationship between the tooth plate and the ferrule of the utility model.

[0022] Reference numerals:

[0023] 100, support mechanism; 110, U-shaped base; 120, spring; 130, slider; 140, lifting plate; 150, horizontal platform;

[0024] 200, adjustment mechanism; 210, motor; 220, gear; 230, tooth plate; 240, ferrule; 250, gentle slope;

[0025] 300, pad;

[0026] 400. Roller. DETAILED DESCRIPTION

[0027] In order to make the purpose, technical solution and advantages of the present invention more clear, the present invention is further described in detail below in conjunction with specific embodiments and with reference to the accompanying drawings. It should be noted that the embodiments of the present invention and the features therein can be combined with each other unless there is any conflict.

[0028] It should be understood that these descriptions are only exemplary and are not intended to limit the scope of the present invention.

[0029] The following describes an aircraft rudder and steering gear test bench that is easy to move and position, provided by some embodiments of the present invention, in conjunction with the accompanying drawings.

[0030] Example 1:

[0031] Combine Figure 1-6 As shown, the aircraft rudder and steering gear test bench provided by the present invention, which is easy to move and position, includes a support mechanism 100 and an adjustment mechanism 200. The support mechanism 100 includes a U-shaped base 110, a plurality of springs 120 embedded in the inner side walls of the U-shaped base 110, a slider 130 connected to the bottom end of the spring 120, a lifting plate 140 connected between two adjacent sliders 130, and a horizontal platform 150 connected between the two lifting plates 140. The inner side walls of the U-shaped base 110 are each provided with two sliding grooves suitable for lifting and lowering the sliders 130.

[0032] The adjusting mechanism 200 includes a motor 210 embedded in the bottom of the U-shaped base 110, a gear 220 sleeved on the outside of the output shaft of the motor 210, two tooth plates 230 meshing with the gear 220, a clamping sleeve 240 clamped to one end of the tooth plate 230, and a gentle slope 250 installed on one side of the clamping sleeve 240, and the lifting plate 140 is located at the top of the gentle slope 250.

[0033] Furthermore, the thickness of the gear 220 is equal to that of the tooth plate 230 , and both fit in with the bottom of the inner cavity of the U-shaped base 110 . With this size and layout design, the gear 220 and the tooth plate 230 fit more stably.

[0034] Furthermore, the two tooth plates 230 are vertically symmetrical about the gear 220, and the two tooth plates 230 slide in opposite directions. With this structural design, the two gentle slopes 250 can move in opposite directions, and then the two lifting plates 140 can be lifted and lowered at the same time.

[0035] Furthermore, two pads 300 are installed at the bottom of the U-shaped base 110. The two pads 300 are vertically symmetrical about the motor 210. The thickness of the pads 300 is greater than the height of the motor 210. The pads 300 can be set to raise the U-shaped base 110 so that the motor 210 can be installed smoothly.

[0036] Furthermore, two rollers 400 are installed at the bottom of the lifting plate 140. The two rollers 400 are both attached to the top of the inclined surface. The rollers 400 are provided to facilitate the lifting of the lifting plate 140.

[0037] Example 2:

[0038] Combine Figure 1 and Figure 4-6 As shown, based on the first embodiment, the top of the gentle slope 250 is set as an inclined surface, and a convex plate is integrally formed at the outer end. The convex plate can prevent the roller 400 from sliding off the inclined surface.

[0039] Example 3:

[0040] Combine Figure 1 、 4 and Figure 6 As shown, in the above embodiment, a socket suitable for the tooth plate 230 to be plugged in is provided on the inner side of the gentle slope 250. The provision of the socket can expand the moving distance of the tooth plate 230 and enable the gentle slope 250 to move outward to the maximum extent.

[0041] The working principle and usage process of the present invention are as follows: when controlling the horizontal platform 150 to be lifted to the required height, the on-site technician starts the motor 210, and then the gear 220 rotates. Under mechanical transmission, the tooth plate 230 pushes the sleeve 240 and the gentle slope 250 to move outward, and then the gentle slope 250 squeezes the roller 400, and then multiple rollers 400 and two lifting plates 140 cooperate to realize the rise of the horizontal platform 150. Then, after the horizontal platform 150 reaches the required height, the motor 210 is turned off, thereby fixing the horizontal platform 150.

[0042] Although the embodiments of the present invention have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and purpose of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. The aircraft rudder and steering gear test bench is easy to move and position, and is characterized by: include: A support mechanism (100) includes a U-shaped base (110), a plurality of springs (120) embedded in two side walls of the U-shaped base (110), a slider (130) connected to the bottom end of the spring (120), a lifting plate (140) connected between two adjacent sliders (130), and a horizontal platform (150) connected between the two lifting plates (140), wherein two side walls of the U-shaped base (110) are each provided with two sliding grooves suitable for lifting the sliders (130); An adjusting mechanism (200) includes a motor (210) embedded in the bottom of the U-shaped base (110), a gear (220) sleeved on the outside of the output shaft of the motor (210), two toothed plates (230) meshing with the gears (220), a clamping sleeve (240) clamped with one end of the toothed plates (230), and a gentle slope (250) installed on one side of the clamping sleeve (240), wherein the lifting plate (140) is located at the top of the gentle slope (250).

2. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 1 is characterized in that: The thickness of the gear (220) is equal to that of the tooth plate (230), and both are in contact with the bottom of the inner cavity of the U-shaped base (110).

3. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 1 is characterized in that: The two tooth plates (230) are vertically symmetrical with respect to the gear (220), and the two tooth plates (230) slide in opposite directions.

4. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 1 is characterized in that: The top of the gentle slope (250) is configured as an inclined surface, and a convex plate is integrally formed at the outer end.

5. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 1 is characterized in that: A socket suitable for plugging the tooth plate (230) is provided on the inner side of the gentle slope (250).

6. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 1 is characterized in that: Two pads (300) are installed at the bottom of the U-shaped base (110), the two pads (300) are vertically symmetrical with respect to the motor (210), and the thickness of the pads (300) is greater than the height of the motor (210).

7. The aircraft rudder and steering gear test bench that is easy to move and position according to claim 4 is characterized in that: Two rollers (400) are installed at the bottom of the lifting plate (140), and the two rollers (400) are both attached to the top of the inclined surface.

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