Pair of aircraft wings

Gall , et al. October 5, 2

Patent Grant D624868

U.S. patent number D624,868 [Application Number D/354,314] was granted by the patent office on 2010-10-05 for pair of aircraft wings. This patent grant is currently assigned to Airbus Operations S.A.S.. Invention is credited to Pierre-Emmanuel Gall, Julien Ricouard.


United States Patent D624,868
Gall ,   et al. October 5, 2010

Pair of aircraft wings

Claims

CLAIM The ornamental design for pair of aircraft wings, as shown and described.
Inventors: Gall; Pierre-Emmanuel (Toulouse, FR), Ricouard; Julien (Toulouse, FR)
Assignee: Airbus Operations S.A.S. (Toulouse Cedex, FR)
Appl. No.: D/354,314
Filed: January 22, 2010

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/319-345 ;244/12.5,12.6,13,15,45A,45R,46,55,91,198,199.2,199.4,211,213,215 ;446/56,57

References Cited [Referenced By]

U.S. Patent Documents
D351131 October 1994 Inoue et al.
D369776 May 1996 Kraft et al.
D494531 August 2004 Fraser
D495988 September 2004 Beaunis et al.
D566031 April 2008 Beaunis et al.
D569783 May 2008 Beaunis et al.
D598361 August 2009 Beaunis et al.

Other References

US. Appl. No. 29/354,311, filed Jan. 22, 2010; Title: Aircraft Tail. cited by other .
U.S. Appl. No. 29/354,310, filed Jan. 22, 2010; Title: Aircraft Wings. cited by other .
U.S. Appl. No. 29/343,961, filed Sep. 22, 2009; Title: Aircraft Wings. cited by other .
ATR Pictures Media Gallery, ATR GIE [online], 2008, [retrieved on Feb. 18, 2010]. 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. Easiwood [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: Olser, Hoskin & Harcourt LLP

Description



FIG. 1 is a perspective view taken from a top, front, left side of pair of aircraft wings according to our design shown on an aircraft shown in dotted lines;

FIG. 2 is a top plan view of the pair of aircraft wings of FIG. 1 with engine nacelles and pylons of the aircraft removed for clarity;

FIG. 3 is a bottom plan view of the pair of aircraft wings of FIG. 1;

FIG. 4 is a front elevation view thereof;

FIG. 5 is an enlarged partial bottom plan view thereof as seen from line 5--5 in FIG. 9, shown separately for clarity of illustration;

FIG. 6 is a rear elevation view of the pair of aircraft wings of FIG. 1;

FIG. 7 is an enlarged rear elevation view thereof as seen from line 7--7 in FIG. 2;

FIG. 8 is a front elevation view thereof as seen from line 8--8 in FIG. 2;

FIG. 9 is a left side elevation view of the pair of aircraft wings of FIG. 1; and,

FIG. 10 is a right side elevation view thereof.

Throughout the Figures, where shown: (i) the dotted lines showing environment are for illustrative purposes only and form no part of the claimed design; (ii) the unshaded surfaces do not form part of the claimed design; and (iii) the dash-dot lines illustrate unclaimed boundaries of surfaces claimed as part of the design.

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References


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