Combined aircraft and take-off and landing way thereof

A combined aircraft and multi-rotor aircraft technology, applied in the aviation field, can solve the problems of low safety and stability, small flight radius, low endurance, etc., and achieve the effect of safe and reliable performance, low operational requirements, and high degree of intelligence

Inactive Publication Date: 2017-06-30
新疆博新智航航空科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Helicopters can take off and land vertically, but the structure is complex, and it takes a lot of money to train helicopter pilots, and requires high driving skills for the pilots
Multi-rotor aircraft can also achieve vertical take-off and landing, and the operation is simple, the operability is strong, and it can enter some narrow areas to operate. However, the flight radius is small and the endurance is low. The serious problem is that the safety and stability are low. Since the multi-rotor aircraft is multi-axis and multi-motor working together, as long as one of the motors fails, it will inevitably cause irreparable accidents in the air.

Method used

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  • Combined aircraft and take-off and landing way thereof
  • Combined aircraft and take-off and landing way thereof
  • Combined aircraft and take-off and landing way thereof

Examples

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Embodiment Construction

[0012] Now in conjunction with accompanying drawing the present invention is described in detail, a kind of combination aircraft, comprises fixed-wing aircraft 36, controller 31, connection platform 17, electromagnetic interlocking post 15 and multi-rotor aircraft 35.

[0013] Connecting platform 17 comprises first battery 12, first controller 14, control switch 11, electromagnetic mother post 16, monitoring radar 13, sensor 19 and rigid support 18; Above the rotorcraft 35, the connection platform 17 is higher than the rotor; the first battery 12, the sensor 19, the first controller 14, the control switch 11 and the monitoring radar 13 are placed in the connection platform 17, and the sensor 19 is placed in the electromagnetic engagement female post 16 At the bottom of the groove, detect whether the electromagnetic occlusal sub-column 21 is engaged with the electromagnetic occlusal female column 16, and output the occlusal state to the first controller 14, the first controller ...

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Abstract

The invention relates to a combined aircraft and a take-off and landing way thereof, which belong to the technical field of aviation. The combined aircraft comprises a fixed wing aircraft, a multi-rotary-wing aircraft, a connecting platform, electromagnetic occlusion columns, a communication system and a radar criterion apparatus, wherein the radar criterion apparatus comprises a monitoring radar and a transmitting radar; each electromagnetic occlulation column comprises an electromagnetic occlusion sub column and an electromagnetic occlusion main column; the electromagnetic occlusion main columns and the monitoring radar are disposed in the connecting platform, the connecting platform is disposed on the multi-rotary-wing aircraft at a certain oblique angle, and the electromagnetic occlusion sub columns and the transmitting radar are arranged in the fixed wing aircraft. When the combined aircraft takes off, the multi-rotary-wing aircraft drives the fixed wing aircraft to take off, and when the fixed wing aircraft reaches take-off speed, the multi-rotary-wing aircraft is separated from the fixed wing aircraft; and when the fixed wing aircraft lands, the multi-rotary-wing aircraft lifts for handover, a radar calibration apparatus is used for accurate docking, and the multi-rotary-wing aircraft carries the fixed wing aircraft to land. The take-off and landing way of the combined aircraft is not limited by fields, and the vertical take-off and landing of the fixed wing aircraft can be realized.

Description

technical field [0001] A combined aircraft and its take-off and landing method belong to the field of aviation technology, and in particular relate to a combined aircraft and its take-off and landing method. Background technique [0002] Traditional aviation aircraft can be divided into fixed-wing aircraft, helicopters and multi-rotor aircraft. Among them, the fixed-wing aircraft has fast flight speed, high maneuverability, large flight radius, and high safety performance factor. However, due to its own limitations, the conditions for take-off and landing are harsh, and the take-off and landing of fixed-wing aircraft must have a long enough runway. . Helicopters can take off and land vertically, but their structures are complex, and it takes a lot of money to train helicopter pilots, which requires high driving skills. Multi-rotor aircraft can also achieve vertical take-off and landing, and the operation is simple, the operability is strong, and it can enter some narrow ar...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D5/00B64C27/08G05D1/12
CPCG05D1/12B64C27/08B64D5/00B64U10/10B64U2101/00
Inventor 王志成党先红李玉龙黄小席罗哲远谭俭辉
Owner 新疆博新智航航空科技有限责任公司
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