A comprehensive test system for horizontal stabilizer actuator performance test

Abstract

The application discloses a kind of for horizontal stabilizer actuator performance test comprehensive test system, it is related to performance test system technical field.The present application includes rack, the left side of the rack is provided with lifting platform, the lower portion of lifting platform is provided with control platform, the top of lifting platform is installed with hydraulic drive system and loading system in turn from front to back, the right side of hydraulic drive system is provided with hydraulic connection component, the top of the rack is installed with hoisting system, the lower portion of hoisting system is provided with hoisting fixture, the inner bottom of the rack is provided with manual drive system, the inner wall of the rack is installed with displacement speed detection system and visual positioning system.The present application passes through hoisting system, so that horizontal stabilizer actuator can adopt assembly line through type, can be connected with automatic and test system, horizontal stabilizer actuator comprehensive test system can realize the automatic test of whole process without manual intervention, and production efficiency is greatly improved.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of performance test systems, in particular to a comprehensive test system for horizontal stabilizer actuator performance test. BACKGROUND

[0002] With the rapid development of civil aviation technology, the design and manufacture of aircraft gradually move towards higher safety, reliability and performance requirements. The stability and control performance of the aircraft is one of the key factors for the safe operation of the aircraft, and the horizontal stabilizer, as an important part of the stability of the aircraft, plays a crucial role. The main function of the horizontal stabilizer is to ensure the stability of the aircraft during flight by adjusting the pitch angle of the aircraft, and the actuator, as the driving device of the horizontal stabilizer, is responsible for adjusting the angle of the tail wing, thereby achieving precise control of the flight attitude. In the process of research and production of aircraft, the performance test of horizontal stabilizer actuator is crucial.

[0003] In Chinese patent (publication number: CN115535291A), a horizontal stabilizer trim actuator test bench is disclosed, which is characterized by: for horizontal stabilizer trim actuator performance test; the horizontal stabilizer trim actuator test bench comprises a test mechanism, a mechanical input unit, a lifting control unit, a center distance measurement unit, a dynamic loading unit, a hydraulic test unit, a measurement and control system unit and a static loading unit.

[0004] The patent and the prior art have the following technical problems in actual use:

[0005] 1. Lack of automatic test capability: although the existing equipment has certain automatic test capability, it cannot realize full-automatic test without manual intervention after the test starts; during the test process, the test must be interrupted, and the equipment must be adjusted to the next test configuration by the test personnel before the next test can be performed.

[0006] 2. Shortcomings in light load control capability: the existing equipment is a double-load cylinder loading. Under light load working condition, the heavy load cylinder is not disconnected, which has a great influence on the actual loading effect and stability of the light load.

[0007] 3. Risk of horizontal stabilizer actuator clamping and dismounting: the existing equipment uses manual lifting of the horizontal stabilizer actuator, which has the risk of collision and damage during clamping and dismounting.

[0008] 4. No manual driving performance detection: in the normal flight process of the aircraft, the actuator is usually controlled by the automatic flight control system (such as the autopilot). However, in some extreme or emergency situations, the automatic flight system may fail, and the pilot needs to maintain the stability of the aircraft through manual control. In this case, the manual input response performance of the horizontal stabilizer actuator is particularly critical. SUMMARY

[0009] The present application aims at solving the above problems, and provides a comprehensive test system for horizontal stabilizer actuator performance test.

[0010] In order to achieve the above-mentioned purpose, the present application specifically adopts the following technical solutions:

[0011] A comprehensive test system for horizontal stabilizer actuator performance test, comprising a rack, a lifting platform is arranged on the left side of the rack, a control platform is arranged below the lifting platform, a hydraulic drive system and a loading system are sequentially installed on the top of the lifting platform from front to back, a hydraulic connection assembly is arranged on the right side of the hydraulic drive system, a hoisting system is installed on the top of the rack, a hoisting clamp is arranged below the hoisting system, a manual drive system is arranged on the inner bottom of the rack, the manual drive system is located behind the loading system, a displacement speed detection system and a visual positioning system are installed on the inner wall of the rack;

[0012] The control platform comprises hardware and control software, and is used for automatic control, data acquisition and analysis, fault diagnosis, process display and test report generation of the whole system;

[0013] The loading system is used for applying heavy load and light load to the horizontal stabilizer actuator;

[0014] The hydraulic drive system is used for hydraulic motor drive control and heavy load loading control on the horizontal stabilizer actuator;

[0015] The hydraulic connection assembly is used for realizing automatic connection and disconnection of pipelines between the hydraulic drive system and the hydraulic motor;

[0016] The displacement speed detection system is used for detecting the moving position and speed of the horizontal stabilizer actuator;

[0017] The visual positioning system is used for detecting the ground clearance of the hydraulic motor oil way interface and the actuator nut on the horizontal stabilizer actuator;

[0018] The manual drive system is used for testing the manual input function of the horizontal stabilizer actuator;

[0019] The hoisting clamp is used for protecting the horizontal stabilizer actuator, and can transmit the load applied by the loading system and the drive provided by the manual drive system to the actuator nut.

[0020] Further, the loading system is composed of a heavy load hydraulic cylinder, a heavy load pressure sensor, a heavy load head, a light load cylinder, a light load pressure sensor and a light load head, the heavy load pressure sensor is arranged between the heavy load head and the telescopic end of the heavy load hydraulic cylinder, and the light load pressure sensor is arranged between the light load head and the telescopic end of the light load cylinder.

[0021] Further, the hydraulic connection assembly comprises a mounting plate fixedly installed on the telescopic end of the light-load cylinder, a servo motor one is fixedly installed on one side of the mounting plate close to the hydraulic drive system, a set of driving wheels and two sets of driven wheels are rotatably installed on the other side of the mounting plate, the two sets of driven wheels are simultaneously engaged with the driving wheels, the driving wheels are connected with the output end of the servo motor one, the outside of the driven wheels is provided with a joint sleeve, the pipeline joint on the hydraulic drive system can be inserted into the joint sleeve, and the pipeline penetrates through the driven wheels and the mounting plate, a pipe winder is arranged between the hydraulic drive system and the mounting plate, and the pipe winder can wind or loosen the pipeline.

[0022] Further, the hoisting system is composed of a sliding rail, a sliding carriage, a lead screw nut, a lead screw motor and a lead screw, the bottom of the sliding carriage is provided with an electric lifting hoist, the bottom end of the steel wire on the electric lifting hoist is fixedly installed with a bottom frame, the bottom of the bottom frame is fixedly installed with a lifting clamp, the lower portion of the sliding rail is provided with a sub-guide rail, the bottom frame is slidingly connected in the sub-guide rail, and the entrance of the sub-guide rail is arranged in an eight-character shape.

[0023] Further, the hoisting clamp comprises an upper protective shell rotatably installed on the bottom of the bottom frame, an insertion window is formed in the outer side of the upper protective shell, and the hydraulic motor oil way interface of the horizontal stabilizer actuator is located opposite to the insertion window, the bottom of the upper protective shell is provided with a lower protective shell, the front surface of the lower protective shell is fixedly installed with a lifting cylinder, the bottom of the telescopic end of the lifting cylinder is fixedly installed with a telescopic bottom shell, the telescopic bottom shell can hold the bottom end of the driving lead screw on the horizontal stabilizer actuator, four groups of hanging claws are slidingly connected in the inside of the lower protective shell, a hanging groove is formed in the inside of the hanging claw, an opening is formed in the lower half of the hanging groove, and the actuator nut can enter the hanging groove through the opening, loading grooves are formed in the two sides of the lower protective shell, and the heavy load head and the light load head can be inserted into the loading grooves.

[0024] Further, a servo motor two is fixedly installed on the front surface of the lower protective shell, a driving bevel gear is fixedly installed on the output end of the servo motor two, a transmission shaft is rotatably installed on the outer side of the lower protective shell, a driven bevel gear is fixedly installed on the outer side of the transmission shaft, the driven bevel gear is engaged with the driving bevel gear, four groups of threaded grooves are formed in the outer side of the transmission shaft, the rotation directions of the two groups of threaded grooves at the same end are opposite, and the four groups of hanging claws are threadedly connected in the four groups of threaded grooves respectively.

[0025] Further, a plurality of balls are annularly rotatably installed on the lifting surface of the telescopic bottom shell.

[0026] Further, the manual drive system is composed of a low-speed motor and a driving wheel, a manual driving wheel is fixedly installed on the bottom of the telescopic bottom shell, the length of the manual driving wheel is 20-50 cm, and the upper protective shell is rotatably installed on the bottom of the bottom frame through a telescopic connecting piece.

[0027] Further, the loading slot is arranged in a V shape, and the plug-in ends of the heavy load head and the light load head are matched with the loading slot.

[0028] Further, the left side of the rack is provided with a lifting cylinder and a pneumatic control system, the telescopic end of the lifting cylinder is connected with the lifting platform, and the pneumatic control system is used for loading control of the light load cylinder and telescopic control of the lifting cylinder and the lifting cylinder.

[0029] The present application has the following advantages:

[0030] The horizontal stabilizer actuator can pass through the hydraulic driving system, the loading system and the manual driving system in sequence by the hoisting system, and the automatic and test system can be connected by the setting of the hydraulic connection assembly and the hoisting clamp, so that the horizontal stabilizer actuator comprehensive test system can realize automatic test without manual intervention in the whole process, and the production efficiency is greatly improved.

[0031] The horizontal stabilizer actuator can be moved to the heavy load position after being separated from the light load by the flow line setting, so that mutual influence between the two load systems is avoided.

[0032] The special hoisting clamp designed by optimization provides good protection for the horizontal stabilizer actuator, provides convenience for loading and unloading of the horizontal stabilizer actuator, and also acts as a load transmission medium, so that the connection with the loading system and the manual driving system can be quickly realized, and the test efficiency is high. BRIEF DESCRIPTION OF DRAWINGS

[0033] Figure 1 is a schematic diagram of the overall structure of the comprehensive test system of the present application Figure One ;

[0034] Figure 2 is a schematic diagram of the overall structure of the comprehensive test system of the present application Figure Two ;

[0035] Figure 3 is a schematic diagram of the lower half structure of the comprehensive test system of the present application

[0036] Figure 4 is a schematic diagram of the hoisting system structure of the present application

[0037] Figure 5 is a schematic diagram of the hoisting clamp structure of the present application Figure One ;

[0038] Figure 6 is a schematic diagram of the hoisting clamp structure of the present application Figure Two ;

[0039] Figure 7 is a schematic diagram of the hanging claw driving structure of the present application

[0040] Figure 8 This is a schematic diagram of the hydraulic connection component structure of the present invention.

[0041] Reference numerals: 1. Frame; 2. Control platform; 3. Hydraulic drive system; 31. Hose reel; 4. Loading system; 41. Heavy-duty hydraulic cylinder; 42. Heavy-duty pressure sensor; 43. Heavy-duty head; 44. Light-duty cylinder; 45. Light-duty pressure sensor; 46. Light-duty head; 5. Hydraulic connection assembly; 51. Mounting plate; 52. Servo motor 1; 53. Drive wheel; 54. Driven wheel; 55. Connector sleeve; 6. Lifting system; 61. Slide rail; 62. Slide carriage; 63. Screw nut; 64. Screw motor; 65. Screw; 66. Electric lifting hoist; 67. Base frame; 68. Lifting device; 6 9. Secondary guide rail; 7. Displacement speed detection system; 8. Vision positioning system; 9. Manual drive system; 10. Lifting clamp; 101. Upper protective shell; 102. Telescopic connector; 103. Plug-in window; 104. Lower protective shell; 105. Telescopic bottom shell; 106. Manual transmission wheel; 107. Ball bearing; 108. Loading groove; 109. Hanging claw; 110. Lifting cylinder; 111. Servo motor II; 112. Driving bevel gear; 113. Drive shaft; 114. Driven bevel gear; 11. Lifting cylinder; 12. Lifting platform; 13. Horizontal stabilizer actuator; 14. Actuator nut. Detailed Implementation

[0042] To make the objectives, technical solutions, and advantages of the embodiments of the present invention clearer, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings.

[0043] Example 1, as Figures 1-8 As shown, a comprehensive test system for testing the performance of a horizontal stabilizer actuator includes a frame 1, a lifting platform 12 on the left side of the frame 1, a control platform 2 below the lifting platform 12, a hydraulic drive system 3 and a loading system 4 installed sequentially from front to back on the top of the lifting platform 12, a hydraulic connection assembly 5 on the right side of the hydraulic drive system 3, a hoisting system 6 installed on the top of the frame 1, a hoisting clamp 10 below the hoisting system 6, a manual drive system 9 installed at the bottom inner side of the frame 1, the manual drive system 9 being located behind the loading system 4, and a displacement velocity detection system 7 and a visual positioning system 8 installed on the inner wall of the frame 1.

[0044] Control platform 2 includes hardware and control software, used for automatic control of the entire system, data acquisition and analysis, fault diagnosis, process display and generation of test reports;

[0045] Loading system 4 is used to apply heavy and light loads to horizontal stabilizer actuator 13;

[0046] The hydraulic drive system 3 is used for the control of the hydraulic motor drive and the heavy load loading on the horizontal stabilizer actuator 13.

[0047] The hydraulic connection assembly 5 is used for the automatic connection and disconnection of the pipeline between the hydraulic drive system 3 and the hydraulic motor.

[0048] The displacement speed detection system 7 is used for detecting the moving position and speed of the horizontal stabilizer actuator 13.

[0049] The visual positioning system 8 is used for detecting the ground clearance between the hydraulic motor oil way interface on the horizontal stabilizer actuator 13 and the actuator nut 14.

[0050] The manual drive system 9 is used for testing the manual input function of the horizontal stabilizer actuator 13.

[0051] The hoisting clamp 10 is used for protecting the horizontal stabilizer actuator 13 and transmitting the load applied by the loading system 4 and the drive provided by the manual drive system 9 to the actuator nut 14.

[0052] The test procedure is as follows: the horizontal stabilizer actuator 13 is hoisted on the hoisting system 6, and then the hoisting clamp 10 is clamped on the actuator nut 14 of the horizontal stabilizer actuator 13, the hoisting clamp 10 plays a protective role and provides good protection for the horizontal stabilizer actuator 13, and then the hoisting system 6 drives the horizontal stabilizer actuator 13 and the hoisting clamp 10 to move to the setting position, the displacement speed detection system 7 is used to detect the moving position and speed of the horizontal stabilizer actuator 13, and the visual positioning system 8 is used to detect the hydraulic motor oil port on the horizontal stabilizer actuator 13, when the horizontal stabilizer actuator 13 moves to the hydraulic drive system 3 station, according to the feedback result of the visual positioning system 8, the control platform 2 controls the lifting platform 12 to lift, the lifting platform 12 drives the hydraulic connection assembly 5 to be flush with the hydraulic motor oil port, the hydraulic connection assembly 5 connects the oil line on the hydraulic drive system 3 with the hydraulic motor oil port, after the connection is completed, the hoisting system 6 transports the horizontal stabilizer actuator 13 to the loading system 4 station, and then the light load loading and the heavy load loading are carried out, and both are loaded on the hoisting clamp 10, the hoisting clamp 10 is connected with the actuator nut 14 quickly, the load condition of the horizontal stabilizer actuator 13 in the actual operation process is simulated, after the loading is completed, the hoisting system 6 transports the horizontal stabilizer actuator 13 to the manual drive system 9 station, the manual drive system 9 directly drives the drive lead screw on the horizontal stabilizer actuator 13, tests the manual input function of the horizontal stabilizer actuator 13, completes the overall test of the horizontal stabilizer actuator 13, after the test is completed, the hoisting system 6 transports the horizontal stabilizer actuator 13 back to the hydraulic drive system 3 station, the hydraulic connection assembly 5 separates the oil line from the hydraulic motor oil port, and then the horizontal stabilizer actuator 13 is transported out of the equipment, and the hoisting clamp 10 is disassembled, the whole process is automatically tested without manual intervention, the test efficiency is high, and the test result is comprehensive.

[0053] In the above embodiment, the loading system 4 is composed of a heavy load hydraulic cylinder 41, a heavy load pressure sensor 42, a heavy load head 43, a light load air cylinder 44, a light load pressure sensor 45 and a light load head 46.

[0054] The horizontal stabilizer actuator 13 is first moved to the light load cylinder 44 position, the light load cylinder 44 drives the light load head 46 to be inserted into the lifting clamp 10, to realize the quick connection of the light load test, and the loading condition is fed back through the light load pressure sensor 45; then the lifting system 6 transports the horizontal stabilizer actuator 13 to the heavy load hydraulic cylinder 41 position, the horizontal stabilizer actuator 13 is directly separated from the light load cylinder 44, to ensure that the two load systems do not affect each other, and then the heavy load hydraulic cylinder 41 drives the heavy load head 43 to be inserted into the lifting clamp 10, to realize the quick connection of the heavy load test, and the loading condition is fed back through the light load pressure sensor 45.

[0055] In the above embodiment, the hydraulic connection assembly 5 further includes a mounting plate 51 fixedly installed on the telescopic end of the light load cylinder 44, a servo motor 52 is fixedly installed on one side of the mounting plate 51 close to the hydraulic drive system 3, a set of driving wheels 53 and two sets of driven wheels 54 are rotatably installed on the other side of the mounting plate 51, the two sets of driven wheels 54 are simultaneously engaged with the driving wheels 53, the driving wheels 53 are connected with the output end of the servo motor 52, a joint sleeve 55 is arranged on the outer side of the driven wheels 54, the pipeline joint of the hydraulic drive system 3 can be inserted into the joint sleeve 55, and the pipeline penetrates through the driven wheels 54 and the mounting plate 51, and a pipe winder 31 is arranged between the hydraulic drive system 3 and the mounting plate 51, and the pipe winder 31 can wind or loosen the pipeline.

[0056] When the horizontal stabilizer actuator 13 is moved to the hydraulic drive system 3 station, the light load cylinder 44 is controlled to operate, at this time, the light load cylinder 44 serves as the telescopic driving source of the hydraulic connection assembly 5, because the hydraulic connection assembly 5 is distributed before and after the loading system 4, the light load head 46 will not contact the horizontal stabilizer actuator 13, and the two will not affect each other, the light load cylinder 44 drives the mounting plate 51 to extend, the mounting plate 51 drives the oil line pipeline on the hydraulic drive system 3 to be close to the hydraulic motor oil line interface, whether the oil line pipeline is on the hydraulic motor oil line interface can be judged through the feedback of the light load pressure sensor 45, then the servo motor 52 is controlled to be powered on, the servo motor 52 drives the driving wheels 53 to rotate, the driving wheels 53 drive the driven wheels 54 to rotate, the driven wheels 54 make the oil line pipeline be threadedly connected to the hydraulic motor oil line interface through the joint sleeve 55, to realize automatic connection. When the horizontal stabilizer actuator 13 is moved to the loading system 4 position, the pipe winder 31 loosens the oil line pipeline, so that the horizontal stabilizer actuator 13 can normally operate, when reset, the pipe winder 31 automatically winds the oil line pipeline, so that the joint sleeve 55 can be sleeved on the interface position again, to realize automatic oil line pipeline automatic dismounting.

[0057] It should be noted that the hydraulic connection assembly 5 can be provided with two sets according to the actual specifications of the horizontal stabilizer actuator 13, for example, the horizontal stabilizer actuator 13 has hydraulic motors on both sides, and the two sets are symmetrically arranged on both sides of the lifting system 6.

[0058] The embodiment four, on the basis of the above embodiment, further comprises that the hoisting system 6 is composed of a slide rail 61, a slide carriage 62, a screw nut 63, a screw rod motor 64 and a screw rod 65, the bottom of the slide carriage 62 is provided with an electric lifting cage 66, the bottom end of the steel wire of the electric lifting cage 66 is fixedly provided with a bottom frame 67, the bottom of the bottom frame 67 is fixedly provided with a lifting device 68, the lower side of the slide rail 61 is provided with a sub guide rail 69, the bottom frame 67 is slidingly connected in the sub guide rail 69, and the entrance of the sub guide rail 69 is provided in an eight-character form.

[0059] The slide carriage 62 is driven to slide along the slide rail 61 by the screw rod 65, the horizontal stabilizer actuator 13 is transported, the electric lifting cage 66 realizes the hoisting of the horizontal stabilizer actuator 13, and the sub guide rail 69 and the bottom frame 67 are arranged, so that the lifting device 68 of the horizontal stabilizer actuator 13 can be limited, the lifting device 68 and the horizontal stabilizer actuator 13 below the lifting device 68 are prevented from swinging in the transportation process, and the stable transportation of the test is ensured.

[0060] The embodiment five, on the basis of the above embodiment, further comprises that the hoisting clamp 10 comprises an upper protective shell 101 rotatably arranged at the bottom of the bottom frame 67, a plug-in window 103 is formed in the outer side of the upper protective shell 101, the hydraulic motor oil way interface on the horizontal stabilizer actuator 13 is located opposite to the plug-in window 103, a lower protective shell 104 is arranged at the bottom of the upper protective shell 101, a lifting cylinder 110 is fixedly arranged on the front side of the lower protective shell 104, a telescopic bottom shell 105 is fixedly arranged at the bottom of the telescopic end of the lifting cylinder 110, the telescopic bottom shell 105 can hold the bottom end of the driving screw rod on the horizontal stabilizer actuator 13, four groups of hanging claws 109 are slidingly connected in the inside of the lower protective shell 104, a hanging groove is formed in the inside of the hanging claw 109, an opening is formed in the lower half of the hanging groove, the actuator nut 14 can enter the hanging groove through the opening, and a loading groove 108 is formed in the two sides of the lower protective shell 104.

[0061] A servo motor two 111 is fixedly arranged on the front side of the lower protective shell 104, a driving bevel gear 112 is fixedly arranged at the output end of the servo motor two 111, a transmission shaft 113 is rotatably arranged at the outer side of the lower protective shell 104, a driven bevel gear 114 is fixedly arranged at the outer side of the transmission shaft 113, the driven bevel gear 114 is engaged with the driving bevel gear 112, four groups of thread grooves are formed in the outer side of the transmission shaft 113, the rotation directions of the two groups of thread grooves at the same end are opposite, and the four groups of hanging claws 109 are threadedly connected in the four groups of thread grooves respectively.

[0062] The rolling ball 107 is annularly rotatably arranged on the holding surface of the telescopic bottom shell 105, because the telescopic bottom shell 105 is in contact with the driving screw rod, the telescopic bottom shell 105 will not additionally load the driving screw rod through the arrangement of the rolling ball 107, and the subsequent loading test result is not affected.

[0063] The loading slot 108 is V-shaped, and the insertion end of the heavy load head 43 and the light load head 46 is matched with the loading slot 108. Through this design, even if there is a slight height difference between the loading slot 108 and the light load head 46 or the heavy load head 43, the heavy load head 43 and the light load head 46 can be inserted into the loading slot 108, reducing the difficulty of loading connection. At the same time, the loading force given by the light load head 46 or the heavy load head 43 is a horizontal force, which is converted into a vertical load force of the actuator nut 14 through the inclined surface of the loading slot 108. Therefore, a smaller loading force can be converted into a larger load force, and the selection range of the light and heavy load driving source is wider.

[0064] When lifting: the horizontal stabilizer actuator 13 is hung on the lifting tool 68, and the horizontal stabilizer actuator 13 is inserted into the lifting clamp 10, the hydraulic motor is located in the upper protective shell 101, the actuator nut 14 is located in the lower protective shell 104, and the hydraulic motor oil way interface is located at the insertion window 103 position, the connecting part on the actuator nut 14 enters the hanging groove from the opening below the inner hanging groove of the hanging claw 109, then the lifting cylinder 110 drives the telescopic bottom shell 105 to rise, the telescopic bottom shell 105 supports the horizontal stabilizer actuator 13 drive screw bottom from below, after the telescopic bottom shell 105 is on the drive screw bottom, the telescopic bottom shell 105 gives the lower protective shell 104 a downward force through the lifting cylinder 110 in reverse, the connecting part on the actuator nut 14 is completely inserted into the hanging groove upward, at the same time, the control servo motor two 111 is powered on, the servo motor two 111 drives the transmission shaft 113 to rotate through the driving bevel gear 112 and the driven bevel gear 114, the transmission shaft 113 drives the two hanging claws 109 on the same end to move away from each other through the thread groove, the hanging claw 109 is attached to the connecting part on the actuator nut 14, and the lifting clamp 10 is automatically clamped on the actuator nut 14.

[0065] When loading, the light load head 46 or the heavy load head 43 is inserted into the loading slot 108, and the actuator nut 14 is loaded by the lifting clamp 10. It should be noted that during the loading process, the actuator nut 14 is subjected to a driving force in the upward direction, so that the hanging claw 109 and the lifting clamp 10 can stably apply a load. During load testing, the pressure sensor detects data, and when the pressure exceeds the threshold value, the light load head 46 or the heavy load head 43 retracts, the actuator nut 14 drives the lifting clamp 10 to rise as a whole, and by controlling the retraction speed of the light load head 46 or the heavy load head 43, the actuator nut 14 is always subjected to the same load when rotating upward, thereby realizing the loading test.

[0066] In the above embodiment, the manual driving system 9 is composed of a low-speed motor and a driving wheel, the bottom of the telescopic bottom shell 105 is fixedly installed with a manual transmission wheel 106, the length of the manual transmission wheel 106 is 20-50 cm, and the upper protective shell 101 is rotatably installed at the bottom of the bottom frame 67 through the telescopic connecting piece 102.

[0067] The lifting system 6 transports the horizontal stabilizer actuator 13 to the manual driving system 9 station, the manual transmission wheel 106 is engaged with the driving wheel, the actuator nut 14 is given a rotating force through the manual transmission wheel 106 first, until it rotates to the top, the actuator nut 14 cannot rise, at this time the manual transmission wheel 106 drives the driving screw on the horizontal stabilizer actuator 13 to rotate through the actuator nut 14, realizes manual test, the manual transmission wheel 106 has enough length, and will not be separated from the driving wheel, and the test is stable.

[0068] Through the setting of the telescopic connecting piece 102, the lifting clamp 10 will not be affected by the bottom frame 67 when the actuator nut 14 rotates.

[0069] In the above embodiment, the left side of the rack 1 is provided with a lifting cylinder 11 and a pneumatic control system, the telescopic end of the lifting cylinder 11 is connected with the lifting platform 12, and the pneumatic control system is used for loading control of the light load cylinder 44 and telescopic control of the lifting cylinder 110 and the lifting cylinder 11.

[0070] The above description of the disclosed embodiments enables those skilled in the art to carry out or use the present application. Various modifications to these embodiments will be apparent to those skilled in the art, and the general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present application. Therefore, the present application will not be limited to these embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. A comprehensive test system for horizontal stabilizer actuator performance testing, comprising a frame (1), characterized in that, The left side of the frame (1) is provided with a lifting platform (12), the lower side of the lifting platform (12) is provided with a control platform (2), the top of the lifting platform (12) is sequentially provided from front to back with a hydraulic drive system (3) and a loading system (4), the right side of the hydraulic drive system (3) is provided with a hydraulic connection assembly (5), the top of the frame (1) is provided with a hoisting system (6), the lower side of the hoisting system (6) is provided with a hoisting clamp (10), the inner bottom of the frame (1) is provided with a manual drive system (9), the manual drive system (9) is located behind the loading system (4), the inner wall of the frame (1) is provided with a displacement speed detection system (7) and a visual positioning system (8); The control platform (2) comprises hardware and control software, and is used for automatic control of the whole system, data acquisition and analysis, fault diagnosis, process display and generation of test reports; The loading system (4) is used for applying heavy load and light load to the horizontal stabilizer actuator (13); The hydraulic drive system (3) is used for hydraulic motor drive control and heavy load loading control on the horizontal stabilizer actuator (13); The hydraulic connection assembly (5) is used for realizing automatic connection and disconnection of pipelines between the hydraulic drive system (3) and the hydraulic motor; The displacement speed detection system (7) is used for detecting the moving position and speed of the horizontal stabilizer actuator (13); The visual positioning system (8) is used for detecting the ground clearance of the hydraulic motor oil way interface and the actuator nut (14) on the horizontal stabilizer actuator (13); The manual drive system (9) is used for testing the manual input function of the horizontal stabilizer actuator (13); The hoisting clamp (10) is used for protecting the horizontal stabilizer actuator (13), and can transmit the load applied by the loading system (4) and the drive provided by the manual drive system (9) to the actuator nut (14).

2. The integrated test system for performance test of a horizontal stabilizer actuator according to claim 1, wherein, The loading system (4) is composed of a heavy load hydraulic cylinder (41), a heavy load pressure sensor (42), a heavy load head (43), a light load cylinder (44), a light load pressure sensor (45) and a light load head (46), the heavy load pressure sensor (42) is arranged between the heavy load head (43) and the telescopic end of the heavy load hydraulic cylinder (41), and the light load pressure sensor (45) is arranged between the light load head (46) and the telescopic end of the light load cylinder (44).

3. The integrated test system for performance test of aileron actuator according to claim 2, characterized in that, The hydraulic connection assembly (5) includes a mounting plate (51) fixedly installed on the telescopic end of the light load cylinder (44), a servo motor I (52) is fixedly installed on the side of the mounting plate (51) close to the hydraulic drive system (3), a set of driving wheels (53) and two sets of driven wheels (54) are rotatably installed on the other side of the mounting plate (51), the two sets of driven wheels (54) are simultaneously engaged with the driving wheels (53), the driving wheels (53) are connected with the output end of the servo motor I (52), the outer side of the driven wheels (54) is provided with a joint sleeve (55), the pipeline joint of the hydraulic drive system (3) can be inserted into the joint sleeve (55), and the pipeline penetrates through the driven wheels (54) and the mounting plate (51), and the pipe winder (31) is arranged between the hydraulic drive system (3) and the mounting plate (51), and the pipe winder (31) can wind or loosen the pipeline.

4. The integrated test system for performance test of a horizontal stabilizer actuator according to claim 3, wherein, The hoisting system (6) is composed of a slide rail (61), a slide carriage (62), a screw nut (63), a screw motor (64) and a screw (65), the bottom of the slide carriage (62) is provided with an electric lifting hoist (66), the bottom end of the steel wire on the electric lifting hoist (66) is fixedly installed with a bottom frame (67), the bottom of the bottom frame (67) is fixedly installed with a lifting tool (68), the lower side of the slide rail (61) is provided with a secondary guide rail (69), and the bottom frame (67) is slidably connected in the secondary guide rail (69), and the entrance of the secondary guide rail (69) is arranged in an eight-character shape.

5. The integrated test system for performance test of aileron actuator according to claim 4, characterized in that, The hoisting clamp (10) comprises an upper protective shell (101) rotatably installed on the bottom of the bottom frame (67), an insertion window (103) is formed in the outer side of the upper protective shell (101), and the hydraulic motor oil way interface of the horizontal stabilizer actuator (13) is located opposite to the insertion window (103), a lower protective shell (104) is arranged at the bottom of the upper protective shell (101), a lifting cylinder (110) is fixedly installed on the front surface of the lower protective shell (104), a telescopic bottom shell (105) is fixedly installed at the bottom of the telescopic end of the lifting cylinder (110), the telescopic bottom shell (105) can be lifted at the bottom end of the driving screw of the horizontal stabilizer actuator (13), four sets of hanging claws (109) are slidably connected in the lower protective shell (104), a hanging groove is formed in the inner side of the hanging claw (109), an opening is formed in the lower half of the hanging groove, and the actuator nut (14) can enter the hanging groove through the opening, loading grooves (108) are formed in the two sides of the lower protective shell (104), and the heavy load head (43) and the light load head (46) can be inserted into the loading grooves (108).

6. The integrated test system for performance test of a horizontal stabilizer actuator according to claim 5, wherein, The front of the lower protective shell (104) is fixedly installed with a servo motor two (111), the output end of the servo motor two (111) is fixedly installed with a driving bevel gear (112), the outer side of the lower protective shell (104) is rotatably installed with a transmission shaft (113), the outer side of the transmission shaft (113) is fixedly installed with a driven bevel gear (114), the driven bevel gear (114) is engaged with the driving bevel gear (112), the outer side of the transmission shaft (113) is provided with four groups of thread grooves, the thread directions of the two thread grooves at the same end are opposite, and four groups of hanging claws (109) are respectively threadedly connected on the four groups of thread grooves.

7. The integrated test system for performance test of aileron actuator according to claim 6, wherein, The lifting surface of the telescopic bottom shell (105) is annularly rotatably installed with a ball (107).

8. The integrated test system for performance test of aileron actuator according to claim 7, characterized in that, The manual driving system (9) is composed of a low-speed motor and a driving wheel, the bottom of the telescopic bottom shell (105) is fixedly installed with a manual transmission wheel (106), the length of the manual transmission wheel (106) is 20-50 cm, and the upper protective shell (101) is rotatably installed at the bottom of the chassis (67) through a telescopic connecting piece (102).

9. The integrated test system for performance test of a horizontal stabilizer actuator according to claim 8, wherein, The loading groove (108) is V-shaped, and the plug-in ends of the heavy load head (43) and the light load head (46) are matched with the loading groove (108).

10. The integrated test system for performance test of a horizontal stabilizer actuator according to claim 9, wherein, The left side of the rack (1) is installed with a lifting cylinder (11) and a gas pressure control system, the telescopic end of the lifting cylinder (11) is connected with a lifting platform (12), and the gas pressure control system is used for loading control of the light load cylinder (44) and telescopic control of the lifting cylinder (110) and the lifting cylinder (11).

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