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:
Aug. 23, 2022

Filed:

Mar. 25, 2019
Applicant:

Japan Aerospace Exploration Agency, Tokyo, JP;

Inventors:

Atsushi Ueno, Tokyo, JP;

Tatsunori Yuhara, Tokyo, JP;

Masashi Kanamori, Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/34 (2006.01); B64C 5/02 (2006.01); B64C 30/00 (2006.01); B64D 27/20 (2006.01); B64D 29/04 (2006.01);
U.S. Cl.
CPC ...
B64D 33/06 (2013.01); B64C 5/02 (2013.01); B64C 30/00 (2013.01); B64D 27/20 (2013.01); B64D 29/04 (2013.01);
Abstract

[Object] To provide a supersonic aircraft and a method of reducing sonic booms, by which sonic booms due to engine exhaust can be reduced. [Solving Means] A supersonic aircraft includes: a pair of engine nacellesR,L mounted on a fuselageof an airframe; finsR,L as a pair of shielding plates that inhibits engine exhaustdischarged from jet engines (not shown) accommodated in the engine nacellesR,L from wrapping downward around the airframe; and a pair of horizontal tailsR,L disposed behind the engine nacellesR,L. The finsR,L are disposed on the horizontal tailsR,L so as to sandwich the engine exhaust, respectively.


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