Simulation aircraft and system thereof

An aircraft and rotating shaft technology, applied in the field of simulated flight, can solve the problems of large volume, high manufacturing cost, and complex structure of the simulated aircraft, and achieve the effects of improving power supply security, low manufacturing cost, and simple structure

Inactive Publication Date: 2014-12-17
喻明
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] For this reason, the technical problem to be solved by the present invention is that the existing simulated aircraft occupies a large volume, is inconvenient to install, has many parts, complex structure, and high manufacturing cost. Therefore, the present invention proposes a simple structure, Simulated aircraft with smaller size and lower production cost

Method used

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  • Simulation aircraft and system thereof
  • Simulation aircraft and system thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0045] see Figure 1-3 , a simulated aircraft, which includes a bracket 50, a first rotating shaft 10 is horizontally arranged on the bracket 50, and one end of the first rotating shaft 10 extending out of the bracket 50 is fixedly connected with a transmission box 8, the The transmission box is fixed by means of welding or bolting, and one side of the transmission box 8 is connected to the cockpit 9, and the cockpit 9 is vertically arranged with the first rotation axis 10, that is, the simulated trainee is sitting in the cockpit 9 When inside, facing away from the axis of the first rotating shaft 10; the first driving device 11 arranged on the side of the first rotating shaft 10 drives the cockpit 9 to rotate around the first rotation with the first rotating shaft 10 The axis of the shaft 10 rotates forward and reverse to realize the rotation of any angle of ±N×360 degrees in the first plane, and completes the simulation of the front and rear direction rotation (somersault ac...

Embodiment 2

[0063] see Figure 7 , a simulated flight system, which includes several simulated aircrafts, all of which are connected to the general controller, and the simulated aircrafts are the simulated aircrafts described in the above-mentioned embodiments. The connection mode in this embodiment can realize remote connection through broadband, optical fiber, etc., through the centralized control of the general controller, and the projection device can project according to the preset picture, and can realize remote cooperation between training bases to simulate aircraft combat drills , which in turn can improve the trainee's flying skills and combat effectiveness.

Embodiment 3

[0065] see Figure 8-10 , On the basis of the first and second embodiments above, the linkage mechanism between the second rotating shaft 20 and the fourth rotating shaft 40 can also be replaced by the following form:

[0066] Described linkage mechanism comprises the 3rd rotating shaft 30 that is fixed on the relative two sidewalls of described transmission case 8 (the described transmission case 8 is cube structure) by two bearings, and the axis of described 3rd rotating shaft 30 and described The axes of the second rotating shaft 20 are parallel, and the end of the second rotating shaft 20 extending out from the first rotating shaft 10 is sleeved with a first gear 22, and the first gear 22 is sleeved on the third rotating shaft 22. The second gear 32 on the rotating shaft 30 meshes; the position of the third rotating shaft 30 facing the fourth rotating shaft 40 is sleeved with a second worm 33, and the fourth rotating shaft 40 is sleeved with a The second worm gear 42 coop...

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Abstract

The invention discloses a simulation aircraft and a system thereof. The simulation aircraft comprises a support, a first rotation shaft is horizontally arranged on the support, a transmission case is fixedly connected at one end of the first rotation shaft extending out of the support, and one side of the transmission case is connected with a cockpit. The first rotation shaft is provided with a hollow cavity, a second rotation shat is arranged in the cavity, the second rotation shaft and the first rotation shaft are coaxially arranged, one end of the second rotation shaft extending into the transmission case is in linkage with a fourth rotation shaft through a linkage mechanism, the fourth rotation shaft is perpendicular to the first rotation shat in horizontal projection, and the cockpit is hinged to an end portion of the fourth rotation shaft extending out of the transmission case through a hinge pin. The second rotation shaft is creatively arranged in the first rotation shaft, so the whole simulation aircraft is simple in structure, small in space occupation, complete in functions, low in manufacturing cost and convenient to mount.

Description

technical field [0001] The invention relates to the technical field of simulated flight, in particular to design a simulated aircraft and a system thereof for pilots' daily training or flight enthusiasts' simulated flight experience. Background technique [0002] With the development of my country's aviation technology and the urgent needs of national defense, the serious shortage of pilots has become increasingly prominent. Therefore, for a long period of time, training high-quality and high-quality pilots will be the top priority of the defense sector. In the process of initial training and skill improvement training, pilots obviously cannot completely learn various flight actions and skills on the real aircraft, while the simulated aircraft is low in training cost, good in safety, easy to operate and control, and has realistic flight experience. The best training gear for training. [0003] Such as Chinese patent document CN102779438A discloses a kind of simulated aircra...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/08
Inventor 喻明陆晓军
Owner 喻明
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