ROTARY AIRCRAFT LAUNCHING APPARATUS AND SYSTEM

WIPO Patent Application WO/2024/041584

A1

A rotary aircraft launching apparatus and system, comprising a support body (1), at least one rotary body (2) rotating about the axis of the support body (1), and a driving apparatus (4) for supplying power for the rotation of the rotary body (2). At least one attitude adjustment apparatus (5) is provided on the rotary body (2), the attitude adjustment apparatus (5) is used for adjusting in real time the attitude of an aircraft during rotation acceleration and at the time of launching, a launching rack (6) for holding and releasing the aircraft is provided on the attitude adjustment apparatus (5), and a base (3) for providing a stable support for the whole launching apparatus is provided at the bottom of the support body (1). In the rotary launching apparatus and system, an attitude adjustment apparatus (5) controls and adjusts the attitude of an aircraft in a targeted manner, such that the linear velocities of left and right wings of the aircraft, in particular a fixed-wing aircraft, with respect to the air at a launching moment are the same, thereby avoiding the potential take-off safety issues caused by a lift force difference between the left and right wings.

JP2018039495	FLYING MOBILE BODY
WO/2000/068630	THERMAL CONTROL SYSTEM FOR SPACECRAFT
WO/2018/229761	UNMANNED VEHICLES DEPLOYMENT AND RETRIEVAL MECHANISM

JIANG JUN (CN)
WANG XUEZHU (CN)

PCT/CN2023/114544

February 29, 2024

August 23, 2023

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SHENYANG JIDONG TECH CO LTD (CN)

B64F1/04

US9126699B1	2015-09-08
US20150239578A1	2015-08-27
US20200079505A1	2020-03-12
CN210503239U	2020-05-12
JP2014040186A	2014-03-06
US1748663A	1930-02-25
US3989206A	1976-11-02
CN112298594A	2021-02-02

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