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Multi-axis 360-degree omnidirectional rotating motion flight simulator

A technology of rotational motion and flight simulation, which is applied to simulators, simulators, instruments, etc. of space navigation conditions, to achieve the effects of reduced training costs, simple maintenance, and low cost

Inactive Publication Date: 2017-01-04
杨小波
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to overcome the deficiencies of the existing flight simulation simulators, the present invention provides a multi-axis 360-degree omnidirectional rotary motion simulation simulator to solve the technical problems of the appeal

Method used

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  • Multi-axis 360-degree omnidirectional rotating motion flight simulator
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  • Multi-axis 360-degree omnidirectional rotating motion flight simulator

Examples

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Embodiment Construction

[0026] exist figure 1 In the shown embodiment, the yaw rotating frame (2) is fixed on the upper and lower bearing positions (6) of the base through the upper and lower rotating shafts (5), and the pitch rotating frame (3) is fixed on the left and right rotating shafts (7). ) is fixed on the left and right bearing positions (8) of the yaw rotating frame, the roll simulation cabin (4) is fixed on the front and rear bearing positions (10) of the pitch rotating frame through the front and rear rotating shafts (9), and the rotating frame is installed The direction can be changed as needed.

[0027] exist figure 1 In the shown embodiment, position (11) is the drive motor reducer and transmission of the yaw rotating frame, the motor (26) reducer (27) driving wheel (28) is installed on the yaw rotating frame, the driven wheel (24) Installed at the bearing position under the base, they are connected by a belt or chain, the motor (26) reducer (27) driving wheel (28) pushes the yaw fra...

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Abstract

The invention relates to a multi-axis 360-degree omnidirectional rotating motion flight simulator, which is a multi-axis rotating motion platform combined by multiple groups of rotating bodies with different sizes and volumes in a crossed manner from the outside in, and is characterized in that a simulation cabin is installed on rotating frames in the multi-axis rotating platform, each rotating frame and an outer frame rotating shaft which supports and fixes the corresponding rotating frame are respectively provided with a set of motor-reducer with a driving wheel, a driven wheel is installed at an outer frame rotating bearing which supports and fixes the corresponding rotating frame, the driving wheel and the driven wheel are connected through a belt, a synchronous belt or a chain, the motor-reducer drives the rotating frame to perform rotating motion around the corresponding driven wheel, coordinate motion among the multiple groups of rotating frames is controlled by a control system so as to enable the simulation cabin installed inside the rotating frames to realize 360-degree omnidirectional rotating motion, and three-dimensional attitudes of an aircraft are completely simulated.

Description

technical field [0001] The invention relates to a multi-axis rotary flight simulation device, in particular to a multi-axis 360-degree omnidirectional rotary motion flight simulation simulator capable of realizing 360-degree omnidirectional rotary motion. Background technique [0002] At present, the known flight simulators are divided into two categories: solid-state simulation and dynamic simulation. Dynamic simulation mostly uses a multi-degree-of-freedom motion platform with mature technology. The limited multi-degree-of-freedom simulation platform cannot meet the needs in this regard. In the current reality, there is a so-called 360-degree omnidirectional motion flight simulation simulator product. This type of product is mainly a two-axis simulation simulator composed of two sets of rotating frames. However, the two-axis simulation simulator cannot completely simulate various complex movements of the aircraft with a large amount of flight movements and an unstable flig...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/12
Inventor 杨小波
Owner 杨小波
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