Invention Application
- Patent Title: FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
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Application No.: US16221397Application Date: 2018-12-14
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Publication No.: US20190118958A1Publication Date: 2019-04-25
- Inventor: Andrei Evulet
- Applicant: JETOPTERA, INC.
- Main IPC: B64D29/02
- IPC: B64D29/02 ; B64C39/02 ; B64C15/00 ; B64C21/04 ; B64D27/18 ; B64D33/02 ; B64D33/04 ; B64C9/38 ; B64D27/10 ; B64C21/00

Abstract:
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.
Public/Granted literature
- US11059600B2 Fluidic propulsive system and thrust and lift generator for aerial vehicles Public/Granted day:2021-07-13
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