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Simulation device of airborne automatic throttle actuating mechanism

A technology of an actuator and a simulation device, applied in the field of aircraft simulators, can solve the problems of difficulty in providing aircraft system signals, high cost of an automatic throttle actuator, and difficulty in maintaining, overhauling, and maintaining the automatic throttle actuator, and achieves a fixed position and height. , controllable production cycle, high integration effect

Active Publication Date: 2021-03-16
青岛蓝天航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] 1. The cost of automatic throttle actuators is high, and the use of aircraft simulators greatly increases the manufacturing cost of aircraft simulators, and the procurement methods and procurement time are uncontrollable;
[0005] 2. The maintenance personnel of the aircraft simulator do not have the experience and ability of the airport ground maintenance personnel, so it is difficult to carry out normal maintenance, overhaul and maintenance of the automatic throttle actuator; it is not conducive to the aircraft simulator to find professionals for normal maintenance, overhaul and maintenance use and cost control;
[0006] 3. The automatic throttle actuator needs to be electrically connected to the aircraft system to collect the necessary aircraft system signals. It is difficult for the aircraft simulator to provide the aircraft system signals required by the automatic throttle actuator;
[0007] 4. The volume of the aircraft simulator is limited, and it can only be simulated in a limited space. The vacant space of the aircraft simulator is not enough to install the automatic throttle actuator;

Method used

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  • Simulation device of airborne automatic throttle actuating mechanism
  • Simulation device of airborne automatic throttle actuating mechanism
  • Simulation device of airborne automatic throttle actuating mechanism

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Embodiment Construction

[0069] The present invention will be described in further detail below in conjunction with the accompanying drawings. The detailed description, which is a description made in conjunction with exemplary embodiments of the present invention, includes various details of the embodiments of the present invention to facilitate understanding, and they should be considered as exemplary only. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the embodiments described herein can be made without departing from the scope and spirit of the invention. Also, descriptions of well-known functions and constructions are omitted in the following description for clarity and conciseness.

[0070] Such as Figure 1-5 As shown, the simulation device of the airborne automatic throttle actuator of the present invention includes:

[0071] Bottom plate 1 is respectively provided with front wall plate 21 and rear wall plate 22 on its front side and ...

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Abstract

The invention relates to a simulation device of an airborne automatic throttle actuating mechanism, which comprises a bottom plate, a front wall plate and a rear wall plate are respectively arranged on the front side surface and the rear side surface of the bottom plate, a left wall plate and a right wall plate are respectively arranged on the left side surface and the right side surface of the bottom plate, and a top cover is arranged above the bottom plate; a power line outlet hole and a network cable outlet hole are formed in the rear wall plate, the power supply processing plate and the data processing plate are both fixed on the rear wall plate, a power line is connected with the power supply processing plate after passing through the power line outlet hole, and a network cable is connected with the data processing plate after passing through the network cable outlet hole; an executing mechanism assembly is arranged on the bottom plate, an output shaft of the executing mechanism assembly is connected with the accelerator, and automatic adjustment of the accelerator is completed. According to the invention, a highly centralized design is adopted, the functions of power supply processing, data processing, mechanical transmission, information feedback and the like are integrally realized, and the simulation of the airborne automatic throttle actuating mechanism can be realized by only providing a working power supply required by equipment and an Ethernet cable connected with a host when the airborne automatic throttle actuating mechanism is used in an aircraft simulator.

Description

technical field [0001] The invention relates to the technical field of aircraft simulators, in particular to a simulation device for an airborne automatic throttle actuator. Background technique [0002] Modern large and medium-sized airliners or military aircraft are equipped with automatic throttle actuators (also known as onboard automatic throttle actuators). The onboard computer calculates the required flight speed and thrust elements according to the data, and realizes automatic control of the throttle. Under normal circumstances, there is no need to correct the throttle, and you can focus on other places. [0003] Aircraft simulators are devices used to train pilots. They can be roughly divided into passenger aircraft simulators and military aircraft simulators. If an aircraft simulator is equipped with an on-board auto-throttle actuator, there are the following deficiencies: [0004] 1. The cost of automatic throttle actuators is high, and the use of aircraft simula...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/08H05K7/20B08B17/02
CPCG09B9/08H05K7/20145H05K7/20172H05K7/20181B08B17/02
Inventor 孙付友申慧青张帆赵立武遇泓霏
Owner 青岛蓝天航空科技有限公司
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