Flight simulator 3DOF cockpit

A flight simulator and 3DOF technology, applied in the field of flight simulators, can solve problems such as the inability to use the built-in coordinate system, the fact that there is still a distance to fully simulate the flight attitude of the aircraft, and the problem of three degrees of freedom rotation control cannot be well solved. , to achieve the effect of hardware cost reduction

Active Publication Date: 2020-11-06
王晨曦
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Existing flight simulators have the following problems: for the controlled object in the innermost cockpit, its rotation axis is an absolute stationary coordinate system, rather than the controlled object's own coordinate system, which is determined by its structural complexity and principle It cannot use the built-in coordinate system
This is a flaw caused by the structural design of existing flight simulators
[0005] Therefore, the prior art cannot well solve the rotation control problem of the three degrees of freedom, and there is still a long way to go before fully simulating the flight attitude of the aircraft.

Method used

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  • Flight simulator 3DOF cockpit

Examples

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Embodiment 1

[0030] Such as figure 2 As shown, this specific embodiment provides a flight simulator 3DOF cockpit, including an inner cabin 30 and an outer cabin 20 .

[0031] Wherein, the outer cabin 20 is fixed, for example, the 3DOF cockpit further includes a base 50 on which the outer cabin 20 is fixed. The inner cabin 30 is a controlled part and can rotate. The 3DOF cockpit also includes a first drive motor, a second drive motor, and a third drive motor. The three groups of motors are completely independent from each other and do not interfere with each other.

[0032] A console is arranged inside the inner cabin 30, and the console includes a control device. The control device is respectively connected to the driving motors and sends control instructions to the corresponding driving motors to control the operation of the first driving motor, the second driving motor and the third driving motor. During specific work, the control device of the inner cabin 30 is manipulated to drive...

Embodiment 2

[0054] Different from Embodiment 1, in this embodiment, the number of gears can be reduced according to the rotation angle requirements. For example, when the axis of the drive shaft 40 of the first group of universal gears 11 is the X axis, if the first group The number of the universal gear 11 is set to one, and the rotation of the 3DOF cockpit along the X axis is at most 180 degrees. Therefore, the quantity of any one set of cardan gears can be one or two.

[0055] Preferably, in a specific embodiment, the number of the first set of universal gears 11, the second set of universal gears 12, and the third set of universal gears 13 is one respectively, and the three universal gears are orthogonal to each other in pairs place.

[0056] Compared with the prior art, the present invention has the following beneficial effects:

[0057] In the flight simulator 3DOF cockpit of the present application, the inner cabin and the outer cabin are concentric spherical, and the inner cabin...

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Abstract

The invention discloses a flight simulator 3DOF cockpit which comprises an inner cabin and an outer cabin, the outer cabin is fixed, and the inner cabin is provided with a control device; the 3DOF cockpit further comprises a first driving motor, a second driving motor and a third driving motor; the outer surface of the inner cabin and the inner surface of the outer cabin are concentric spherical;the three groups of universal gears are mounted in the inner cabin; the connecting lines of the centers of the three groups of universal gears and the sphere center of the outer surface of the inner cabin are three mutually orthogonal axes; the inner surface of the outer cabin is rough, driven wheels of the three sets of universal gears are coupled with the inner surface of the outer cabin, and the inner cabin is supported in the outer cabin; and the three groups of universal gears are independently driven by a driving motor respectively. The inner cabin is supported in the outer cabin throughcoupling of the three groups of universal gears and the rough inner surface of the outer cabin. And under the action of the driving motor, the universal gears rotate on the inner surface of the outercabin and drive the inner cabin to rotate. During rotation, the rotation in three axial directions is completely independent, and the multi-angle and multi-attitude flight of the aircraft in space can be simulated.

Description

technical field [0001] The invention relates to the technical field of flight simulators, in particular to a flight simulator 3DOF cockpit structure. Background technique [0002] The structure of the existing flight simulator, disclosed as known CN201210297245.6: multi-axis flight simulator, including the outer ring, the center ring, the inner ring of the nest connection, the outer ring is fixedly arranged on the base, the outer ring, the center The ring and the inner ring are respectively driven by independent servo motors, and the center ring connects to the simulator cockpit inward. The three-dimensional rotation is realized by adopting the connection mode of three groups of rotation axes orthogonally nested. This structure is similar to the structure of the gyroscope. The schematic diagram of the structure is as follows: figure 1 shown. [0003] Existing flight simulators have the following problems: for the controlled object in the innermost cockpit, its rotation axi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/12
CPCG09B9/12
Inventor 王晨曦
Owner 王晨曦
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