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Carrier aircraft

An aircraft and controller technology, applied in the field of carrier aircraft, can solve problems such as loss, aircraft landing failure, and easy damage to parachutes and parachute ropes, so as to avoid damage.

Pending Publication Date: 2019-05-03
COOL HIGH TECH BEIJING CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Realizing the emergency landing of low-altitude aircraft through parachutes is a relatively conventional and technically easy way to realize at present. One-piece structure, the two cannot be separated, the parachute mechanism of this aircraft is set on the top of the aircraft, the parachute and the parachute itself need to bear a lot of tension during the descent of the aircraft, which makes the parachute and the parachute very easy to damage, serious Under the circumstances, the aircraft will fail to land and cause losses

Method used

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Embodiment Construction

[0035] The core of the present invention is to provide a carrier aircraft, so as to effectively reduce the tension on the parachute and the parachute rope during the emergency landing of the carrier aircraft.

[0036] In order to enable those skilled in the art to better understand the solutions of the present invention, the technical solutions in the embodiments of the present invention are clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only Some, but not all, embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0037] see Figure 1 to Figure 7 , the carrier aircraft disclosed in this embodiment includes an aircraft body 1 and a carrier cabin 2, wherein the role of the aircraft b...

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Abstract

The invention discloses a carrier aircraft that comprises an aircraft main body used for providing a lifting force and a carrying bin connected to the aircraft main body and providing a carrying function; the aircraft main body is connected with the carrying bin through a docking mechanism, and when the docking mechanism is in a locked state, the carrying bin and the aircraft main body are connected into a whole; when the docking mechanism is in a disengaged state, the carrying bin is disengaged from the aircraft main body; and a parachute is arranged on the carrying bin. The carrying bin in the carrier aircraft can achieve independent landing; compared with the situation of overall landing of an existing aircraft, the weight of the carrying bin is remarkably reduced, the pulling force borne by the parachute and parachute cords is greatly reduced, in this way, damage to the parachute and the parachute cords is effectively avoided, and a guarantee is provided for safe landing of the carrying bin.

Description

technical field [0001] The invention relates to the technical field of aircraft design and production, and more specifically relates to a carrier aircraft. Background technique [0002] With the advancement of urban three-dimensional transportation technology, low-altitude aircraft (such as flying cars) with carrying functions have become a development trend. This low-altitude aircraft is mainly used in urban low-altitude environments, and its buffer distance with the ground is very short during landing. How to land safely and smoothly is one of the focus of attention of those skilled in the art. [0003] Realizing the emergency landing of low-altitude aircraft through parachutes is a relatively conventional and technically easy way to realize at present. One-piece structure, the two cannot be separated, the parachute mechanism of this aircraft is set on the top of the aircraft, the parachute and the parachute itself need to bear a lot of tension during the descent of the a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/08B64D17/00
Inventor 李桐德徐彬项昌乐甄鹏飞邢志强
Owner COOL HIGH TECH BEIJING CO LTD
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