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.

Date of Patent:
Oct. 17, 2017

Filed:

Jun. 25, 2014
Applicant:

Forsvarets Materielverk, Stockholm, SE;

Inventor:

Erik Prisell, Vendelso, SE;

Assignee:

FORSVARETS MATERIELVERK, Stockholm, SE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/00 (2006.01); B64C 15/02 (2006.01); B64C 21/06 (2006.01); B64C 21/08 (2006.01); B64D 27/18 (2006.01); B64C 21/04 (2006.01); B64C 29/00 (2006.01); B64C 39/10 (2006.01);
U.S. Cl.
CPC ...
B64C 39/005 (2013.01); B64C 15/02 (2013.01); B64C 21/04 (2013.01); B64C 21/06 (2013.01); B64C 21/08 (2013.01); B64C 29/0025 (2013.01); B64D 27/18 (2013.01); B64C 2039/105 (2013.01); Y02T 50/166 (2013.01);
Abstract

The invention relates to a propulsion system concept that is a propulsion system that is integrated in the hull of an aerial vehicle (), which propulsion concept comprises at least one differential velocity fan (), which is arranged on a shaft driven by one or more power units (). The propulsion concept is intended to provide short takeoff and landing distances, high flight speed (high subsonic to transsonic) and to be able to provide low IR signature, low radar signature, a small cross section and low air resistance. The propulsion concept is called HPVO (High Performance Optimized Versatile propulsion). The invention is useful both for air vehicles of the type for conventional takeoff and landing, 'CTOL' (Conventional Take Off and Landing), 'Chair' and for vertical takeoff and landing, “V (t) OL” (Vertical (Take) Off and Landing') and the flying wing (blended-body). The concept is applicable to both large and small aircraft, manned as well as unmanned aerial vehicles.


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