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A jet manned aircraft

An aircraft and jet-type technology, applied in the field of aircraft, can solve the problems of inconvenient, long time, and high cost to pass through obstacles, and achieve the effect of free and easy operation of flight, convenient operation, and simple structure

Active Publication Date: 2018-12-04
康研机器人(重庆)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In real life, people mostly rely on vehicles for travel, and for short-distance travel, especially when the road conditions are poor, conventional vehicles are large in size, expensive, inconvenient to pass through obstacles, and detours. Therefore, there is a need for a time-saving and labor-saving means of transportation for short-distance travel

Method used

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  • A jet manned aircraft
  • A jet manned aircraft
  • A jet manned aircraft

Examples

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Embodiment Construction

[0010] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.

[0011] Such as figure 1 , figure 2 , image 3 As shown, a jet manned aircraft includes a flight seat 1, two elastic buffer frames 5, four main thrusters 2, a hand arm 6 and an operating handle 7, two sets of side flight systems, and a rear turbojet Engine 15, battery 1. Two elastic buffer frames 5 are symmetrically installed on the lower part of the flight seat 1 . Four main thrusters 2 are installed on the lower part of the flight seat 1 . The hand arm 6 is installed on one side of the flight seat 1 , and the operating handle 7 is installed on the hand arm 6 . The rear turbojet engine 15 is mounted on the flight seat 1 rear portion. The battery 16 is installed at the rear of the flight seat 1 and above the r...

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PUM

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Abstract

The invention discloses a jet manned aerial vehicle, comprising a flight seat, two elastic buffer racks, four main propelling rockets, an armrest, an operating handle, two side flight systems, a rear turbojet engine, and a battery; the two elastic buffer racks are mounted symmetrically on the lower portion of the flight seat, the four main propelling rockets are mounted on the lower portion of the flight seat, the side flight systems are mounted symmetrically on two sides of the flight seat respectively, large parallel plates are mounted on the lateral side of the flight seat, one sides of upper and lower hinging plates are hinged to the large parallel plates respectively, the other sides of the upper and lower hinging plates are hinged to small parallel plates respectively, the small parallel plates and the large parallel plates are parallel to each other, cylinder block ends of hinging plate adjusting cylinders are hinged to the lower portions of the large parallel plates, and a piston rod end of an engine adjusting cylinder is hinged to the side turbojet engine. By providing the multi-angle adjustable flight system, flight is free and simple; the jet manned aerial vehicle is simple in structure and convenient to operate.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a jet-type manned aircraft. Background technique [0002] In real life, people mostly rely on vehicles for travel, and for short-distance travel, especially when the road conditions are poor, conventional vehicles are large in size, expensive, inconvenient to pass through obstacles, and detours. Therefore, there is a need for a time-saving and labor-saving means of transportation for short-distance travel. Contents of the invention [0003] In view of the above problems, the present invention provides a jet manned aircraft, which realizes the purpose of free and easy operation and flight by providing a multi-angle adjustable flight system. [0004] The technical solution used in the present invention is: a jet manned aircraft, including flight seats, two elastic buffer frames, four main thrusters, hand arm and operating handle, two sets of side flight systems, rear vortex Th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02
CPCB64C39/026
Inventor 不公告发明人
Owner 康研机器人(重庆)有限公司
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