Control column test excitation device

By designing a driving rod test incentive device for the iron bird ground test, the power sensor and the operator realize the application of high -frequency frequency sweeping and step signals, solving the problem of manipulating the problem that it is difficult to meet high -frequency testing, and improves. The accuracy and efficiency of the test data.

CN119370333APending Publication Date: 2025-01-28SHAANXI AIRCRAFT CORPORATION
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Patent Information

Application Number
CN202411490989.9
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-24
Publication Date
2025-01-28

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Abstract

The invention belongs to the technical field of aircraft simulation tests, and particularly relates to a joystick test excitation device which is used for performing excitation input on a joystick during a ground joystick dynamic and static performance test. Comprising a clamp fixing bolt (1), a control rod (2), a clamp (3), a first double-lug plug (4), a force sensor (5), a second double-lug plug (6), an actuator (7) and a support (9), and one end of the force sensor (5) is connected with the clamp (3) through the first double-lug plug (4); the hoop (3) is arranged on the control rod (2) and is fixed through the hoop fixing bolt (1); the other end of the force sensor (5) is connected with the output end of an actuator (7) through a second double-lug plug (6); the actuator (7) is fixed on the support (9); and the support (9) is fixed on the ground or the floor of an aircraft cockpit.
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Description

Technical Field

[0001] The invention belongs to the technical field of aircraft simulation test, and in particular relates to a control stick test excitation device, which is used for performing excitation input on a control stick during a ground control stick dynamic and static performance test. Background Art

[0002] In the iron bird ground test, it is often necessary to perform dynamic and static performance tests on the joystick. In order to obtain accurate aircraft control system test data, it is necessary to input an excitation signal to the joystick. Since manual control of the joystick for dynamic and static performance tests can no longer meet the increasingly high-frequency sweep and step test requirements, the accuracy of the test data is affected. Summary of the invention

[0003] Purpose of the invention: To provide a joystick test excitation device that can accurately provide excitation signal input, improve the accuracy and consistency of test data, and improve test efficiency and quality.

[0004] Technical solution:

[0005] A control column test excitation device comprises: a clamp fixing bolt 1, a control column 2, a clamp 3, a first double-ear plug 4, a force sensor 5, a second double-ear plug 6, an actuator 7, and a support 9, wherein one end of the force sensor 5 is connected to the clamp 3 through the first double-ear plug 4; the clamp 3 is arranged on the control column 2 and fixed by the clamp fixing bolt 1; the other end of the force sensor 5 is connected to the output end of the actuator 7 through the second double-ear plug 6; the actuator 7 is fixed on the support 9; and the support 9 is fixed on the ground or the floor of the cockpit of an aircraft.

[0006] Furthermore, the actuator 7 includes a hydraulic servo actuator and an electric servo actuator.

[0007] Furthermore, the installation plane of the actuator 7 is perpendicular to the axis of the steering column 2 in the initial state.

[0008] Furthermore, the displacement of the actuator 7 is greater than or equal to the movement displacement of the steering column 2 .

[0009] Furthermore, the actuator 7 is fixed on the support 9 by means of actuator bolts 8 .

[0010] Furthermore, the support 9 is fixed to the ground by support bolts 10 .

[0011] Furthermore, the measuring range of the force sensor 5 is greater than or equal to the maximum force value of the steering column 2 .

[0012] Furthermore, the force sensor 5 includes a cylindrical force sensor and an S-shaped force sensor.

[0013] Beneficial effects:

[0014] By adopting the present invention, the actuator 7 applies an excitation signal, drives the power sensor 5 to move through the binocular plug 6, and the sensor 5 drives the steering column 2 to move through the binocular plug 4. The force sensor 5 feeds back the force signal to the test equipment during the movement. The operator can accurately apply high-frequency sweep and step signals through the control mechanism of the actuator 7, thereby realizing the dynamic and static performance test function of the steering column, improving the stability and consistency of the test data, and improving the test efficiency and quality. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the structure of the control column test excitation device;

[0016] Reference numerals:

[0017] 1——Clamp fixing bolt

[0018] 2 - Control stick

[0019] 3——Clamp

[0020] 4——Dual ear plug

[0021] 5 - Force sensor

[0022] 6——Double ear plug

[0023] 7——Actuator

[0024] 8——Actuator bolt

[0025] 9——Support

[0026] 10——Support bolt. DETAILED DESCRIPTION

[0027] In order to make the purpose, technical scheme and advantages of the implementation of this application clearer, the technical scheme in the implementation of this application will be described in more detail in combination with the drawings in the implementation of this application. In the drawings, the same or similar reference numerals throughout represent the same or similar elements or elements with the same or similar functions. The described implementation is a part of the implementation of this application, not all of the implementations. The implementation described below with reference to the drawings is exemplary and is intended to be used to explain this application, and cannot be understood as a limitation on this application. Based on the implementation in this application, all other implementations obtained by ordinary technicians in this field without making creative work are within the scope of protection of this application. The implementation of this application is described in detail below in combination with the drawings.

[0028] In the description of the present invention, it is necessary to understand that the terms "center", "axial", "vertical", "up", "down", "upper end", "bottom end", "inside", "outside", etc., indicating the orientation or position relationship, are based on the orientation or position relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the scope of protection of the present invention.

[0029] In order to apply excitation input to the joystick and obtain accurate test data, and solve the data accuracy error caused by manual manipulation of the joystick for dynamic and static performance testing, which affects the accuracy of the test data, it is necessary to provide a joystick test excitation device that can accurately provide excitation signal input, improve the accuracy and consistency of the test data, and improve the test efficiency and quality.

[0030] In order to solve the above technical problems, the present invention proposes a steering column test excitation device. Figure 1 As shown: it includes a clamp fixing bolt 1, a steering column 2, a clamp 3, a first double-ear plug 4, a force sensor 5, a second double-ear plug 6, an actuator 7, and a support 9.

[0031] One end of the force sensor 5 is connected to the clamp 3 through the first double-ear plug 4; the clamp 3 is set on the control column 2 and fixed by the clamp fixing bolt 1; the other end of the force sensor 5 is connected to the output end of the actuator 7 through the second double-ear plug 6; the actuator 7 is fixed on the support 9; the support 9 is fixed on the ground or the floor of the aircraft cockpit.

[0032] In a possible embodiment, the actuator 7 includes a hydraulic servo actuator and an electric servo actuator.

[0033] In a possible embodiment, the installation plane of the actuator 7 is perpendicular to the axis of the steering column 2 in the initial state.

[0034] In a possible embodiment, the displacement of the actuator 7 is greater than or equal to the movement displacement of the steering column 2 .

[0035] In a possible embodiment, the actuator 7 is fixed to the support 9 by an actuator bolt 8 .

[0036] In a possible embodiment, the support 9 is fixed to the ground by support bolts 10 .

[0037] In a possible embodiment, the measuring range of the force sensor 5 is greater than or equal to the maximum force value of the steering column 2 .

[0038] In a possible embodiment, the force sensor 5 includes a cylindrical force sensor or an S-shaped force sensor.

[0039] The present invention fixes the clamp 3 on the steering column 2 through the clamp fixing bolt 1, connects the force sensor 5 to the clamp 3 through the double ear plug 4, connects the force sensor 5 to the actuator 7 through the double ear plug 6, fixes the actuator 7 to the support 9 through the actuator bolt 8, and fixes the support 9 to the bolt hole reserved on the ground through the support bolt 10. The actuator 7 applies an excitation signal, drives the power sensor 5 to move through the double ear plug 6, and the sensor 5 drives the steering column 2 to move through the double ear plug 4. The force sensor 5 feeds back the force signal to the test equipment during the movement, thereby realizing the dynamic and static performance test function of the steering column.

[0040] The actuator 7 applies an excitation signal, drives the power sensor 5 to move through the binocular plug 6, and the sensor 5 drives the steering column 2 to move through the binocular plug 4. The force sensor 5 feeds back the force signal to the test equipment during the movement.

[0041] The operator can accurately apply high-frequency sweep and step signals through the control mechanism of the actuator 7, thereby realizing the dynamic and static performance test function of the control column, improving the stability and consistency of the test data, and improving the test efficiency and quality.

[0042] By adopting the present invention, the operator can accurately apply high-frequency sweep and step signals through the control mechanism of the actuator, thereby realizing the dynamic and static performance test function of the steering column, improving the stability and consistency of the test data, and improving the test efficiency and quality.

[0043] The above is only a specific implementation of the present application, but the protection scope of the present application is not limited thereto. Any changes or substitutions that can be easily thought of by a person skilled in the art within the technical scope disclosed in the present application should be included in the protection scope of the present application. Therefore, the protection scope of the present application shall be based on the protection scope of the claims.

Claims

1. A steering column test excitation device, characterized in that: include: A clamp fixing bolt (1), a steering column (2), a clamp (3), a first double-ear plug (4), a force sensor (5), a second double-ear plug (6), an actuator (7), and a support (9), wherein one end of the force sensor (5) is connected to the clamp (3) via the first double-ear plug (4); the clamp (3) is arranged on the steering column (2) and fixed by the clamp fixing bolt (1); the other end of the force sensor (5) is connected to the output end of the actuator (7) via the second double-ear plug (6); the actuator (7) is fixed on the support (9); and the support (9) is fixed on the ground or the floor of the cockpit of an aircraft.

2. The steering column test excitation device according to claim 1, characterized in that: The actuator (7) includes a hydraulic servo actuator and an electric servo actuator.

3. The steering column test excitation device according to claim 1, characterized in that: The installation plane of the actuator (7) is perpendicular to the axis of the steering column (2) in the initial state.

4. The steering column test excitation device according to claim 1, characterized in that: The displacement of the actuator (7) is greater than or equal to the movement displacement of the steering column (2).

5. The steering column test excitation device according to claim 1, characterized in that: The actuator (7) is fixed on the support (9) by means of actuator bolts (8).

6. The driving stick test excitation device according to claim 1, characterized in that: The support (9) is fixed to the ground via support bolts (10).

7. The steering column test excitation device according to claim 1, characterized in that: The measuring range of the force sensor (5) is greater than or equal to the maximum force value of the steering rod (2).

8. The steering column test excitation device according to claim 1, characterized in that: The force sensor (5) comprises a cylindrical force sensor and an S-shaped force sensor.