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:
Dec. 01, 1998

Filed:

Feb. 21, 1997
Applicant:
Inventors:

Heinz Adolf Gerhardt, Redondo Beach, CA (US);

James Franklin Kerswell, Los Angeles, CA (US);

Richard Thomas Priestley, La Quinta, CA (US);

Berry Thomas Gibson, Kennesaw, GA (US);

Assignee:

Northrop Grumman Coporation, Los Angeles, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C / ; B64D / ;
U.S. Cl.
CPC ...
244 15 ; 244 / ; 244 / ; 244214 ; 244 55 ; 244204 ; D123 / ; D123 / ;
Abstract

The present invention is a laminar supersonic transport aircraft having a reverse delta wing located between a forward section and a distal end of the aircraft, a set of jet engines superposed on another set of jet engines, a stabilizing vertical tail located near the distal end of the aircraft, a stabilizing canard surface located near the forward section of said aircraft. Also, a laminar flow control device can be incorporated within the wing. The reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending from respective ends of the leading edge toward a trailing apex point and respective span-wise wing extensions in a natural laminar boundary layer wing region extending chordwise from the leading edge by a fraction of the chordlength of the wing and extending span-wise from opposing sides of said wing.


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