Joseph William Pawlowski

US Patent:

D504654, May 3, 2005

Filed:

Aug 18, 2004

Appl. No.:

29/211542

Inventors:

David Herbert Graham - San Pedro CA, US
Domenic J. Maglieri - Williamsburg VA, US
Hideo Ikawa - Huntington Beach CA, US
Jay Lee Vadnais - Torrance CA, US
Keith Brian Meredith - Carson CA, US
Joseph William Pawlowski - Granada Hills CA, US
John Albert Dahlin - Rancho Palos Verdes CA, US
Marvin LeRoy Martin - Lancaster CA, US

Assignee:

Northrop Grumman Corporation - Los Angeles CA

International Classification:

1212

US Classification:

D12319

US Patent:

20060038063, Feb 23, 2006

Filed:

Aug 18, 2004

Appl. No.:

10/920616

Inventors:

David Graham - San Pedro CA, US
Domenic Maglieri - Williamsburg VA, US
Hideo Ikawa - Huntington Beach CA, US
Jay Vadnais - Torrance CA, US
Keith Meredith - Carson CA, US
Joseph Pawlowski - Granada Hills CA, US
John Dahlin - Rancho Palos Verdes CA, US
Marvin Martin - Lancaster CA, US

Assignee:

Northrop Grumman Corporation - Los Angeles CA

International Classification:

B64C 30/00

US Classification:

24403500A

Abstract:

An aircraft comprises a fuselage, wings extending from the fuselage, and engine nacelles, wherein the fuselage has contours shaped to create shock and expansion zones to compensate for expansion zones and shocks produced by the wings and engine nacelles when the aircraft travels at supersonic speeds. The fuselage shape can be achieved by including a main fairing positioned along a bottom surface of the fuselage. The nacelles can be positioned adjacent to the fuselage and integral with the wings, and the aircraft can further include auxiliary fairings positioned along bottom surfaces of the nacelles.

US Patent:

51730235, Dec 22, 1992

Filed:

Aug 12, 1991

Appl. No.:

7/743926

Inventors:

Joseph W. Pawlowski - Granada Hills CA
J. Ford Johnston - Sunland CA

Assignee:

Cannon Energy Corporation - Mojave CA

International Classification:

B63H 120

US Classification:

416207

Abstract:

A propeller blade cuff having a root end and a first annular flange at the root end, and a wind turbine generator hub having a second annular flange to be attached to the first flange comprising a clamp ring having multiple sections, the sections having flange-receiving and clamping grooves, each extending part way about the annular flanges; and fastener structure interconnecting the ring sections to exert adjustable tension for adjustably retaining the flanges in the grooves.