Aircraft tail

Gall , et al. December 7, 2

Patent Grant D628530

U.S. patent number D628,530 [Application Number D/354,311] was granted by the patent office on 2010-12-07 for aircraft tail. This patent grant is currently assigned to Airbus Operations S.A.S.. Invention is credited to Pierre-Emmanuel Gall, Julien Ricouard.


United States Patent D628,530
Gall ,   et al. December 7, 2010

Aircraft tail

Claims

CLAIM The ornamental design for an aircraft tail, 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/354,311
Filed: January 22, 2010

Current U.S. Class: D12/345
Current International Class: 1207
Field of Search: ;D12/319-345 ;D21/447,448 ;244/4R,7B,12.1,13,15,21,117R,119,130

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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 tail according to our design shown on an aircraft shown in dotted lines with engine nacelles and pylons of the aircraft removed for clarity;

FIG. 2 is a top plan view thereof;

FIG. 3 is a bottom plan view of the aircraft tail of FIG. 1 shown on the aircraft with engine nacelles and pylons of the aircraft shown in dotted lines;

FIG. 4 is an enlarged front elevation view of the aircraft tail as seen from line 4--4 in FIG. 2;

FIG. 5 is a rear elevation view of the aircraft tail of FIG. 1 shown on an aircraft with engine nacelles and pylons of the aircraft shown in dotted lines;

FIG. 6 is a left side elevation view thereof; and,

FIG. 7 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.

* * * * *

References


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