Six-degree-of-freedom flight simulation equipment

A technology of flight simulation and degree of freedom, which is applied in the direction of space navigation simulators, simulators, space navigation equipment, etc. It can solve problems such as difficult to meet the needs of simulation training, and achieve the effect of dispersing self-weight and ensuring the accuracy of arm guidance

Pending Publication Date: 2020-09-18
GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Limited by the freedom of space movement, the above-mentioned flight simulation tra...

Method used

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  • Six-degree-of-freedom flight simulation equipment
  • Six-degree-of-freedom flight simulation equipment
  • Six-degree-of-freedom flight simulation equipment

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Embodiment Construction

[0030] The following will be attached Figure 1-5 The technical solution of the present invention is described clearly and completely. Obviously, the described embodiments are part of the embodiments of the present invention, rather than all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0031] In the description of the present invention, it should be understood that the directions or positional relationships indicated by the terms "upper", "lower", "front", "rear", "inner", and "outer" are based on the drawings shown The orientation or positional relationship is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the pointed device or element must have a specific orientation, be constructed and operated in a specific or...

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Abstract

The invention discloses six-degree-of-freedom flight simulation equipment, which is characterized by comprising a pitching unit, a yawing unit, a rolling unit, a vertical actuating unit, a variable diameter adjusting unit, a rotating arm and a main driving unit, wherein the main driving unit is used for driving the rotating arm to rotate, the vertical actuating unit is slidably connected with therotating arm, the variable diameter adjusting unit is used for driving the vertical actuating unit to longitudinally slide along the rotating arm, the rolling unit is slidably connected with the vertical actuating unit, and the vertical actuating unit is used for driving the rolling unit to slide up and down; the rotating axis of the rolling unit is longitudinally perpendicular to the rotating arm; the rotating axis of the yawing unit is perpendicular to the rotating axis of the rolling unit; and the rotating axis of the pitching unit is perpendicular to the plane where the rotating axis of the yawing unit and the rotating axis of the rolling unit are located together. Therefore, the technical problems that, for example, six-degree-of-freedom flight simulation cannot be carried out in a centrifugal field in the prior art are solved.

Description

Technical field [0001] The invention relates to the field of flight simulation equipment, in particular to a six-degree-of-freedom flight simulation equipment. Background technique [0002] Flight simulation equipment is a simulation platform for the development and training of pilot equipment. It is mainly used for the operation and use of airborne equipment, pilot overload simulation training, space disorientation training, technical and tactical simulation training, etc. [0003] The currently public flight simulation equipment is divided into two categories according to whether it has continuous overload simulation function: one is training equipment such as swivel chair, simulation cabin, parallel platform, etc., which are mainly used for flight phenomenon demonstration teaching or small load simulation training, and do not have continuous overload simulation. Environment; the other is training equipment based on manned centrifuges, which can realize continuous overload simula...

Claims

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Application Information

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IPC IPC(8): G09B9/12G09B9/20
CPCG09B9/12G09B9/20
Inventor 宋琼尹娇妹舒杨尹鹏杨永生蒋春梅牛红攀
Owner GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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