POWER PLANT WITH VARIABLE THRUST DIRECTION, AND AIRCRAFT

WIPO Patent Application WO/2024/088114

A1

A power plant with variable thrust direction, the power plant comprising a fan (10), a housing (20) and an adjusting mechanism (30). The housing (20) is internally provided with an air intake duct (23), a first air output duct (21) and a second air output duct (22). The fan (10) is arranged in the air intake duct (23). The adjusting mechanism (30) is located at the junction of the air intake duct (23), the first air output duct (21) and the second air output duct (22); and the adjusting mechanism (30) is movably connected to the housing (20). The adjusting mechanism (30) is provided with an air guide duct (31); after the adjusting mechanism (30) moves relative to the housing (20), the air guide duct (31) causes the air intake duct (23) to be in communiation with the first air output duct (21) and/or the second air output duct (22).

JP2016107958	BOUNDARY LAYER CONTROLLER FOR AIRCRAFT
WO/2020/239470	AIR INTAKE LIP FOR A TURBOMACHINE NACELLE, COMPRISING AN ACOUSTIC DEVICE, AND METHOD FOR PRODUCING SUCH A LIP
JPH01301496	AIR INTAKE AND DUCT OF AIRCRAFT

HU HUAZHI (CN)
DING KAI (CN)

PCT/CN2023/125020

May 02, 2024

October 17, 2023

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EHANG INTELLIGENT EQUIPMENT GUANGZHOU CO LTD (CN)

B64D33/02; B64C27/22; B64C27/28; B64D33/04

CN115593640A	2023-01-13
CN212921968U	2021-04-09
CN207539377U	2018-06-26
CN213057502U	2021-04-27
CN101818703A	2010-09-01
CN217124490U	2022-08-05

SHENZHEN XIECHENG INTELLECTUAL PROPERTY AGENCY (GENERAL PARTNERSHIP) (CN)

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