Aircraft body fairing

Saint-Jalmes , et al. September 21, 2

Patent Grant D624002

U.S. patent number D624,002 [Application Number D/343,962] was granted by the patent office on 2010-09-21 for aircraft body fairing. This patent grant is currently assigned to Airbus SAS. Invention is credited to Bernard Rumeau, Bruno Saint-Jalmes, Jason Zaneboni.


United States Patent D624,002
Saint-Jalmes ,   et al. September 21, 2010

Aircraft body fairing

Claims

CLAIM The ornamental design for an aircraft body fairing, as shown and described.
Inventors: Saint-Jalmes; Bruno (Toulouse, FR), Zaneboni; Jason (Blagnac, FR), Rumeau; Bernard (Cornebarrieu, FR)
Assignee: Airbus SAS (Blagnac Cedex, FR)
Appl. No.: D/343,962
Filed: September 22, 2009

Related U.S. Patent Documents

Application Number Filing Date Patent Number Issue Date
29335123 Apr 9, 2009 D617724

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/181,319,345 ;244/129.1,130 ;440/66

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5031836 July 1991 Ward
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D375925 November 1996 Griffin
6425507 July 2002 Allen
D466858 December 2002 Carroll et al.
D497586 October 2004 Ferguson
D541207 April 2007 Seidel
D582832 December 2008 Dornier
D612317 March 2010 Stinemetze et al.

Other References

ATR Pictures Media Gallery, ATR GIE [online], 2008, [retrieved on Aug. 4, 2009]. Retrieved from the Internet: < URL: http://www.atr.fr/public/atr/html/media/pictures.php>. cited by other .
Q400 NextGen, Bombardier [online], 1997-2008, [retrieved on Aug. 4, 2009]. Retrieved from the Internet: < URL: http://www.q400.com/q400/en/home.jsp>. cited by other .
Turbo Prop Airliner Production List; J Roach, A.B. Eastwood [online], [retrieved on Aug. 4, 2009]. Retrieved from the Internet: < URL: http://www.tahs.com/books/turbo.htm>. cited by other.

Primary Examiner: Brooks; Cathron C.
Assistant Examiner: Stevens; Maurice
Attorney, Agent or Firm: Osler, Hoskin & Harcourt LLP

Description



FIG. 1 is a perspective view taken from a top, front, left side of an aircraft body fairing according to our new design;

FIG. 2 is another perspective view taken from a top, front, left side of the aircraft body fairing of FIG. 1;

FIG. 3 is a left side elevation view thereof;

FIG. 4 is a right side elevation view thereof;

FIG. 5 is a top plan view thereof;

FIG. 6 is a front elevation view thereof;

FIG. 7 is a rear elevation view thereof;

FIG. 8 is a perspective view taken from a top, front, left side of the aircraft body fairing of FIG. 1 shown on an aircraft shown in broken lines; and,

FIG. 9 is a top, rear, left perspective view of FIG. 8 shown with wing tips removed for clarity.

Throughout the Figures, broken lines showing environment or structure are for illustrative purposes only and form no part of the claimed design. Dash-dot broken lines represent the boundary between claimed and unclaimed areas and form no part of the claimed design.

* * * * *

References


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