Aircraft landing device and method

A technology for an aircraft and a detection device, applied in the aviation field, can solve the problems of short battery life, low safety, and the runway cannot be hovered in the air, and achieves the effect of reducing the construction of the runway and being flexible and flexible.

Inactive Publication Date: 2017-07-04
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 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 endurance Due to the consideration of the fixed-wing aircraft, it has become the first choice for people to travel, but due to the limitation of the venue, most customers cannot satisfy their desire to fly, which greatly limits the development and popularization of aircraft.

Method used

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  • Aircraft landing device and method
  • Aircraft landing device and method

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Embodiment Construction

[0012] The present invention is described in detail below in conjunction with accompanying drawing: a kind of landing mode of aircraft is realized by following landing device, and this landing device comprises child body 1 and mother body 2, and described child body 1 comprises fixed-wing aircraft 11, network connection platform 12, connection slot 13, sensor response device 14 and movable baffle 15; Fixed-wing aircraft 11 is similar in structure to conventional fixed-wing aircraft, and fixed-wing aircraft 11 comprises wing, fuselage, empennage, landing gear, propulsion device and control device; the network connection platform 12 is placed in the fuselage of the fixed-wing aircraft 11, and the effect is to call service to the service platform 22, so that the mother body 2 welcomes the daughter body 1 to land; The structure 23 fits; the connection groove 13 includes a support column groove 131 and a curved surface groove 132; the sensor response device 14 is located at the bell...

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Abstract

The invention belongs to the technical field of aviation, and particularly relates to an aircraft landing device and method. The landing device comprises a subsidiary body and a maternal body, wherein the subsidiary body comprises a fixed-wing aircraft, a network connection platform, a connection groove, sensing and responding devices and a movable baffle; the maternal body comprises a multi-rotor aircraft, a service platform, a connection structure and alignment detection devices; the alignment detection devices detect the orientation of the subsidiary body, and meanwhile, the alignment detection devices position the sensing and responding devices of the subsidiary body precisely; when the subsidiary body needs to land, the maternal body lifts off, and the three alignment detection devices respectively are aligned with the three sensing and responding devices to achieve precise positioning; and the connection structure is embedded into the connection groove, the maternal body is connected with the subsidiary body, the maternal body starts a power system, and the maternal body carries the subsidiary body to land. The aircraft landing device and method can utilize the advantages of the multi-rotor aircraft, the multi-rotor aircraft is utilized to combine with the aircraft to manufacture an air runway for take-off and landing of the aircraft, construction of a runway needed by the aircraft is reduced, and popularization of the fixed-wing aircraft is facilitated.

Description

technical field [0001] The invention relates to an aircraft landing device and method, belonging to the field of aviation technology, and in particular to an aircraft landing device and method. 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 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 endurance Due to the considerations, 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 aircraft. Contents of the in...

Claims

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Application Information

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