The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Mar. 03, 2026
Filed:
Jul. 06, 2023
Applicant:
Jetoptera, Inc., Edmonds, WA (US);
Inventor:
Andrei Evulet, Edmonds, WA (US);
Assignee:
JETOPTERA, INC., Edmonds, WA (US);
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/04 (2023.01); B64C 9/38 (2006.01); B64C 15/00 (2006.01); B64C 15/14 (2006.01); B64C 21/00 (2023.01); B64C 23/00 (2006.01); B64C 39/02 (2023.01); B64D 27/10 (2006.01); B64D 27/18 (2006.01); B64D 29/02 (2006.01); B64D 33/02 (2006.01); B64D 33/04 (2006.01); B64U 30/10 (2023.01); B64U 50/15 (2023.01); F02C 3/04 (2006.01); F02C 6/04 (2006.01); F02K 1/00 (2006.01); F02K 1/36 (2006.01); B64U 10/25 (2023.01); B64U 20/65 (2023.01); B64U 30/00 (2023.01);
U.S. Cl.
CPC ...
B64D 33/04 (2013.01); B64C 9/38 (2013.01); B64C 15/00 (2013.01); B64C 15/14 (2013.01); B64C 21/00 (2013.01); B64C 21/04 (2013.01); B64C 23/00 (2013.01); B64C 23/005 (2013.01); B64C 39/024 (2013.01); B64D 27/10 (2013.01); B64D 27/18 (2013.01); B64D 29/02 (2013.01); B64D 33/02 (2013.01); B64U 30/10 (2023.01); B64U 50/15 (2023.01); F02C 3/04 (2013.01); F02C 6/04 (2013.01); F02K 1/002 (2013.01); F02K 1/36 (2013.01); B64C 2230/04 (2013.01); B64C 2230/06 (2013.01); B64C 2230/16 (2013.01); B64D 2033/0273 (2013.01); B64U 10/25 (2023.01); B64U 20/65 (2023.01); B64U 30/00 (2023.01); F05D 2220/90 (2013.01); Y02T 50/10 (2013.01); Y02T 50/30 (2013.01); Y02T 50/40 (2013.01);
Abstract
A propulsion system coupled to a vehicle. The system includes an ejector having an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity. A control surface having a leading edge is located directly downstream of the outlet structure such that propulsive fluid from the ejector flows over the control surface.