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Parachute with aircraft

A parachute and aircraft technology, applied in the field of parachutes, can solve the problems of large size, inability to hover and move up and down, and achieve the effect of enhancing the ability to stay in the air and facilitating rescue

Inactive Publication Date: 2015-12-23
施侃超
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] An existing parachute is used to reduce the speed of a free-falling body when it lands, but it cannot keep hovering and moving up and down when the parachute is opened, and its volume is sometimes too large for purposes such as high-rise lifesaving

Method used

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Embodiment 1

[0014] In Embodiment 1, a parachute with an aircraft is manufactured, including a parachute 1 and a multi-axis rotorcraft 2, the top of the parachute 1 is opened in a symmetrical manner with the central vertical axis 3, and the edge of the hole is seamlessly connected to a multi-axis rotor aircraft 2; 2 includes several electric rotors 4, isolation layer 5, flight state computer control system, power supply, external power supply 6, remote controller 7 and man-machine connection interface 8, isolation layer 5 is a planar object, isolation layer 5 and rotor blade The horizontal plane where 9 is located is parallel and the distance from the horizontal plane where rotor blade 9 is located is no more than ±340 mm, preferably no more than ±100 mm from the horizontal plane where rotor blade 9 is located. The flight state computer control system includes a satellite positioning terminal, an accelerometer, a magnetometer, an air pressure sensor, a gyroscope and a communication module. ...

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PUM

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Abstract

Disclosed is a parachute with an aircraft. The parachute with the aircraft is characterized by comprising a parachute body and the rotor aircraft. A hole is formed in the top of the parachute body, and the rotor aircraft is in seamless connection with the hole formed in the top of the parachute body. The aircraft comprises a plurality of electric rotors, an isolating layer, a flight state computer-control system, a power source, an external power source, a remote controller and a man-machine connecting interface. The isolating layer is a planar object. The flight state computer-control system comprises a satellite positioning terminal, an accelerometer and a communication module. Two or more power transmission lines which are combined with the external power source and a power utilization load of the aircraft to form a circuit are adopted by the aircraft. According to the invention, the parachute with the aircraft can maintain a suspension state and a stretched state of the parachute body at any position, and therefore persons in high buildings can be conveniently rescued. Due to the fact that two or more power transmission lines which are combined with the external power source and the power utilization load of the aircraft to form the circuit are adopted, the external power source can continuously supply electric energy to the aircraft through the power transmission lines, and the air-staying capacity of the aircraft can be enhanced in an almost unlimited mode.

Description

technical field [0001] The invention relates to a parachute with an aircraft. Background technique [0002] An existing parachute is used to reduce the speed of a free-falling body when landing, but it cannot maintain hovering and mobile lifting when the parachute is opened, and its volume is sometimes too large for purposes such as high-rise lifesaving. Contents of the invention [0003] The object of the present invention is to provide a parachute capable of hovering and loading while the parachute is deployed. [0004] The technical solution for realizing the purpose of the present invention: manufacture a parachute with aircraft, including a parachute and a rotorcraft, the top of the parachute has a hole symmetrical to the central vertical axis, and the edge of the hole is seamlessly connected with a rotorcraft; the aircraft includes several Electric rotor, isolation layer, flight state computer control system, power supply, external power supply, remote control and m...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D17/00B64D17/80
Inventor 施国樑
Owner 施侃超
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