- 专利标题: FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
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申请号: EP24160112.9申请日: 2016-09-02
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公开(公告)号: EP4403760A3公开(公告)日: 2024-09-25
- 发明人: EVULET, Andrei
- 申请人: Jetoptera, Inc.
- 申请人地址: US Edmonds, WA 98020 123 Second Avenue, Suite 200
- 专利权人: Jetoptera, Inc.
- 当前专利权人: Jetoptera, Inc.
- 当前专利权人地址: US Edmonds, WA 98020 123 Second Avenue, Suite 200
- 代理机构: K2 IP Limited
- 优先权: US 1562213465P 2015.09.02
- 分案原申请号: 16843124.5 2016.09.02
- 主分类号: B64C21/04
- IPC分类号: B64C21/04 ; B64C23/00 ; B64C39/12 ; B64D27/02 ; B64D33/04 ; F02K1/28 ; F02C3/32
摘要:
A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore conduit. At least one tail ejector is fluidly coupled to the at least one tail conduit. The fore ejectors respectively include an outlet structure out of which gas from the at least one fore conduit flows. The at least one tail ejector includes an outlet structure out of which gas from the at least one tail conduit flows. First and second primary airfoil elements have leading edges respectively located directly downstream of the first and second fore ejectors. At least one secondary airfoil element has a leading edge located directly downstream of the outlet structure of the at least one tail ejector.
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