Automatic throttle actuator excitation method for ground tests

A technology of automatic throttle and actuator, applied in the direction of electrical testing/monitoring, etc., can solve the problems of large investment resources and large test scale, and achieve the effects of saving resources, comprehensive verification, and increasing fault simulation functions

Active Publication Date: 2014-11-19
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] During the autothrottle ground test, the autothrottle actuator needs to be involved, and the autothrottle actuator needs to be stimulated to work normally. If the plan on the real aircraft is used, the flight control system needs to be put into the test to stimulate it accordingly. The disadvantage is that the scale of the experiment is large and the investment of resources is large.

Method used

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  • Automatic throttle actuator excitation method for ground tests
  • Automatic throttle actuator excitation method for ground tests
  • Automatic throttle actuator excitation method for ground tests

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Embodiment Construction

[0020] The present invention will be described in further detail below through specific embodiments and in conjunction with the accompanying drawings.

[0021] The automatic throttle mechanism used is connected to a load throttle, and there is a position feedback sensor on the throttle. The automatic throttle mechanism contains two motors of channel A and channel B. The required excitation signals are shown in Table 1.

[0022] Table 1

[0023]

[0024]

[0025] 1. Normal working condition

[0026] a) Control the 400Hz / 36V power supply, 27V DC power supply, + / -15V DC power supply and 5V DC power supply through the switch on the operation panel, 400Hz / 36V power supply, 27V DC power supply, + / -15V DC power supply, and 5V DC power supply through the power supply side terminals The row reaches the terminal block on the side of the automatic throttle actuator through the operation panel, and reaches the A and B channel motors of the automatic throttle actuator through cable...

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Abstract

The invention discloses an automatic throttle actuator excitation method for ground tests, and belongs to the field of aircraft design. In an automatic throttle ground test, a simulation device is often used for excitation of an automatic throttle actuator to achieve control simulation, power supply and interface communication necessary to the automatic throttle ground test. According to the invention, an automatic throttle actuator excitation device is used, in accordance with certain steps, for completing proper excitation of the automatic throttle actuator and detection, determination and disposal of fault statuses of the automatic throttle actuator. The automatic throttle actuator excitation method for the ground tests have the beneficial effects of reducing the scale of the tests, shortening the cycle of the tests and verifying the automatic throttle actuator more comprehensively.

Description

technical field [0001] The invention belongs to the field of aircraft design and relates to an excitation method for an automatic throttle actuator suitable for ground tests. Background technique [0002] During the autothrottle ground test, the autothrottle actuator needs to be involved, and the autothrottle actuator needs to be stimulated to work normally. If the plan on the real aircraft is used, the flight control system needs to be put into the test to stimulate it accordingly. The disadvantage is that the scale of the experiment is relatively large and the input of resources is large. Contents of the invention [0003] The purpose of the present invention is to use the excitation device of the automatic throttle actuator to operate according to certain steps to complete the normal excitation of the automatic throttle actuator and the detection, judgment and disposal of the failure state of the automatic throttle actuator. [0004] A technical scheme of an excitation...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
Inventor 田慧超张明高茜
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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