Device for launching and landing aircrafts

A recovery device and aircraft technology, which is applied in the field of aircraft, can solve the problems of large time and fuel consumption, and achieve the effects of saving time, good controllability, and small mechanical damage

Inactive Publication Date: 2014-09-24
杨举 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the take-off method of carrier-based aircraft, it is necessary to take off in sequence, and it takes a long time to complete the formation flight, which leads to a lot of time and fuel consumption until the formation is completed

Method used

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  • Device for launching and landing aircrafts

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Embodiment Construction

[0018] A launch and recovery device for an aircraft includes a fixed rotating launch tower 1, which is a fixed rotating mechanism that passes through the ground (or equivalent to the ground). A rotating shaft 4 is provided in the middle of the rotating tower; the rotating shaft can gradually rise and fall along the rotating tower as required. A group of 3 rotating arms 2 protruding outward are arranged on the rotating shaft, the root end of the rotating arm is hinged on the rotating shaft, and the extending end of the rotating arm is provided with a receiving platform 3 that can adjust the inclination angle; the section size of the rotating arm Decreases along the protruding end. And along with the rotation of the rotating shaft, the rotating arm is gradually raised. A stretchable flexible elastic cable 5 matched with the aircraft is provided at the extended end of the rotating arm; the flexible elastic cable is wound on the rotating arm. The flexible elastic cable has certa...

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Abstract

The invention discloses a device for launching and landing aircrafts. The device comprises a fixedly arranged rotary launching tower, wherein a rotating shaft is arranged at the middle part of the rotary launching tower; a group of rotating arms extending outwards is arranged on the rotating shaft, one end of each rotating arm is hinged to the rotating shaft, and a bearing platform capable of adjusting an angle of inclination is arranged at the extending end of each rotating arm; telescopic flexible elastic ropes matched with the aircrafts are arranged at the extending ends of the rotating arms. The device adopts a brand-new launching and landing manner for the aircrafts, and a large-area runway is not needed, so that a heavy investment is saved; a plurality of aircrafts can be launched at the same during launching, so that the time is reduced compared with the time used during conventionally successive launching; the device is high in controllability and high in reliability, and the requirement for the operant level of navigating mates of the aircrafts is low.

Description

technical field [0001] The invention relates to an aircraft, in particular to an aircraft launch and recovery device. Background technique [0002] At present, the commonly used launch methods for aircraft are generally sliding type (mainly used for aircraft) and recoil type (mainly used for aerospace). The requirements for the site are high, and an open and flat launch site is required. The launch process can only be completed by fully utilizing the fuel carried by itself, which reduces or reduces the endurance of the aircraft to a certain extent. For the take-off mode of carrier-based aircraft, it is necessary to take off sequentially, and the formation flight can be completed after a long period of time, which leads to the consumption of a lot of time and fuel until the formation is completed. It has a huge impact on fleeting precious fighters. Contents of the invention [0003] The purpose of the present invention is to provide a launch and recovery device for aircr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/02
Inventor 杨举杨冠
Owner 杨举
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