Cabin damping base for aircraft simulator

A technology for aircraft simulation and shock-absorbing base, which is applied to simulation devices, simulators, instruments and other directions of space navigation conditions, and can solve problems such as impact protection and protection that cannot be multi-directional

Pending Publication Date: 2021-09-14
上海和鸣与行航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The cockpit of a flight simulator is often adapted to a variety of driving modes, and in order to present the reality of the driving environment, the driving device on the seat has a large range of motion to meet the bumps or tilts in the simulated fli

Method used

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  • Cabin damping base for aircraft simulator
  • Cabin damping base for aircraft simulator

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Embodiment Construction

[0017] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments.

[0018] refer to Figure 1-2 As shown, a cockpit damping base for an aircraft simulator includes a top mounting plate 1, a lower fixing plate 2, a connecting seat plate 3, a buffer bend 4, a connecting shaft assembly 6 and a pressure relief assembly 7;

[0019] The top mounting plate 1 is used to connect the simulator cabin, the lower fixing plate 2 is fixedly arranged on the installation plane; the connecting seat plate 3 is used to assist in the installation of the pressure relief assembly 7; the upper end of the buffer bend 4 is connected The top mounting plate 1, the lower end is connected with the lower fixing plate 2; the upper end of...

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PUM

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Abstract

The invention relates to the technical field of flight simulator equipment, in particular to a cabin damping base for an aircraft simulator. A top protecting cover is installed on a middle carrying table, and a center console is installed below the middle carrying table in an embedded mode. A display split screen is embedded in a front side panel of the top protecting cover, and a control shifting button is fixedly installed on the end face table top of the middle carrying table. A main operating rod and an instrument assembly are both installed on a front panel of the middle carrying table. A positioner, a radio transceiver device and a radar transceiver are all mounted on the center console. According to the cabin damping base, the overall structure is simple, the operability of each module is optimized, diversified instruments and control units are adopted, and the authenticity of the overall simulator is improved; and moreover, interface UIs of different aircraft types can be further simulated by displaying the display split screen, so that the adaptation capability of the simulator to each aircraft type is improved, the reality sense of flight simulation experience is integrally improved, and the consumption demand of a hard core related enthusiast is met.

Description

technical field [0001] The invention relates to the technical field of flight simulator equipment, in particular to a cockpit shock-absorbing base for an aircraft simulator. Background technique [0002] In a broad sense, a flight simulator is a machine used to simulate the flight of an aircraft, such as a device that simulates the flight of an aircraft, missile, satellite, spacecraft, etc., which can be called a flight simulator. and capable of operating simulation devices; [0003] In order to adapt to various driving modes and to present a realistic driving environment, the cockpit of a flight simulator often has a large movement range of the driving device on the seat to meet the bumps or inclinations in simulated flight; therefore, for the user , the shock absorption and buffering of the seat are very important; the existing buffer device of the cockpit or seat can only absorb up and down vibration energy, and cannot provide good protection and protection against multi...

Claims

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Application Information

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IPC IPC(8): F16F3/04G09B9/08
CPCF16F3/04G09B9/08
Inventor 李奇东刘雁飞沙明工
Owner 上海和鸣与行航空科技有限公司
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