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Taking-off method of aircraft and device thereof

An aircraft and propulsion device technology, applied in aircraft parts, rotorcraft, aircraft, etc., can solve the problems of short battery life, inability to hover in the air on the runway, restricting the development and popularization of fixed-wing aircraft, etc., to reduce the construction of runways, favorable effect

Inactive Publication Date: 2017-06-23
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the opening of low-altitude airspace, the aircraft market will grow rapidly. Both fixed-wing aircraft and multi-rotor aircraft have their own advantages and disadvantages; The landing process needs to use the runway and cannot hover in the air; the multi-rotor aircraft can take off and land vertically, the technology is simple, the maneuverability is simple, the operation is simple, and the flight vibration is small, but the endurance time is short and the safety is low; for safety and In consideration of endurance, fixed-wing aircraft has become the first choice for people to travel, but due to space constraints, most customers cannot satisfy their desire to fly, which greatly limits the development and popularization of fixed-wing aircraft

Method used

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  • Taking-off method of aircraft and device thereof
  • Taking-off method of aircraft and device thereof
  • Taking-off method of aircraft and device thereof

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Embodiment Construction

[0012] The present invention is described in detail below in conjunction with accompanying drawing: a kind of take-off mode of aircraft is realized by following take-off device, and this take-off device comprises child body 1 and mother body 2; Child body 1 comprises fixed-wing aircraft 11, connecting groove 12, movable The baffle plate 13 and the baffle plate groove 14; the fixed-wing aircraft 11 includes a wing, a fuselage, an empennage, a landing gear, a propulsion device and a control device. Connecting groove 12 is positioned at fixed-wing aircraft 11 fuselage back, and effect is to allow connecting structure 22 fit; Described connecting groove 12 comprises column groove 121 and spherical groove 122; Movable baffle 13 is positioned at fixed-wing aircraft 11 fuselage back rears, The effect is to close the connection slot 12 when the fixed-wing aircraft 11 is flying, so as to reduce the influence of the airflow at the connection slot 12 on the fixed-wing aircraft during flig...

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PUM

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Abstract

The invention provides a taking-off method of an aircraft and a device thereof, belongs to the technical field of aviation, and particularly relates to the taking-off method of the aircraft and the device thereof. The device comprises a daughter and a parent, and the daughter comprises a fixed wing aircraft, a connecting groove, a mobile baffle and a baffle groove; the parent comprises a multi-rotor type aircraft and a connecting structure; when the daughter needs to take off, the parent is hoisted above the daughter by adopted a hoisting method, and the connecting structure of the parent is embedded into the connecting groove of the daughter; after the parent supports and carries the daughter to lift to a certain altitude, the parent hoists the daughter to fly forwards together, after the daughter reaches a speed needed by taking-off, the parent tilts forwards slightly to make the connecting structure separate from the connecting groove, and the daughter separates from the parent; the daughter continues to fly, the parent returns, and taking-off of the fixed wing aircraft is smoothly completed. According to the taking-off method of the aircraft and the device thereof, the multi-rotor type aircraft is utilized to be combined with the fixed wing aircraft, an aerial runway is created for taking-off of the aircraft, and building of runways needed by the aircraft is reduced, which facilitates popularization of the fixed wing aircraft.

Description

technical field [0001] An aircraft take-off method and its device belong to the field of aviation technology, and in particular relate to an aircraft take-off method and its device. Background technique [0002] With the opening of low-altitude airspace, the aircraft market will grow rapidly. Both fixed-wing aircraft and multi-rotor aircraft have their own advantages and disadvantages; The landing process needs to use the runway and cannot hover in the air; the multi-rotor aircraft can take off and land vertically, the technology is simple, the maneuverability is simple, the operation is simple, and the flight vibration is small, but the endurance time is short and the safety is low; for safety and In consideration of endurance, fixed-wing aircraft has become the first choice for people to travel, but due to space constraints, most customers cannot satisfy their desire to fly, which greatly limits the development and popularization of fixed-wing aircraft. Contents of the i...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64C27/08
CPCB64D5/00B64C27/08
Inventor 王志成李玉龙罗哲远谭俭辉
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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