Invention Grant
- Patent Title: Configuration for vertical take-off and landing system for aerial vehicles
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Application No.: US15456450Application Date: 2017-03-10
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Publication No.: US10464668B2Publication Date: 2019-11-05
- Inventor: Andrei Evulet
- Applicant: Jetoptera, Inc.
- Applicant Address: US WA Edmonds
- Assignee: JETOPTERA, INC.
- Current Assignee: JETOPTERA, INC.
- Current Assignee Address: US WA Edmonds
- Agency: Foster Pepper PLLC
- Agent P. G. Scott Born
- Main IPC: B64C29/04
- IPC: B64C29/04 ; B64C39/12 ; B64D27/20 ; B64C11/00 ; B64C39/02 ; B64C9/38 ; B64C15/00 ; B64C21/00 ; B64C29/02 ; B64D27/10 ; B64D29/02 ; B64D33/02 ; B64D33/04

Abstract:
A vehicle, includes a main body. A fluid generator is coupled to the main body and produces a fluid stream. At least one fore conduit and at least one tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the fore conduit, coupled to the main body and respectively coupled to a starboard side and port side of the vehicle. The fore ejectors respectively comprise an outlet structure out of which fluid flows. At least one tail ejector is fluidly coupled to the tail conduit. The tail ejector comprises an outlet structure out of which fluid flows. A primary airfoil element is coupled to the tail portion. A surface of the primary airfoil element is located directly downstream of the first and second fore ejectors such that the fluid from the first and second fore ejectors flows over the such surface.
Public/Granted literature
- US20170240275A1 CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES Public/Granted day:2017-08-24
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