Aircraft crew rest

Sethapun , et al. September 20, 2

Patent Grant D766790

U.S. patent number D766,790 [Application Number D/506,200] was granted by the patent office on 2016-09-20 for aircraft crew rest. This patent grant is currently assigned to Gulfstream Aerospace Corporation. The grantee listed for this patent is Gulfstream Aerospace Corporation. Invention is credited to Aram Kasparian, Kevin Sethapun.


United States Patent D766,790
Sethapun ,   et al. September 20, 2016

Aircraft crew rest

Claims

CLAIM The ornamental design for an aircraft crew rest, as shown and described.
Inventors: Sethapun; Kevin (Savannah, GA), Kasparian; Aram (Savannah, GA)
Applicant:
Name City State Country Type

Gulfstream Aerospace Corporation

Savannah

GA

US
Assignee: Gulfstream Aerospace Corporation (Savannah, GA)
Appl. No.: D/506,200
Filed: October 14, 2014

Current U.S. Class: D12/195
Current International Class: 1208
Field of Search: ;D12/195,193,414,190,196 ;D15/17,28 ;D10/46,98,102-103 ;D8/302-303

References Cited [Referenced By]

U.S. Patent Documents
D244442 May 1977 Greiss
4884767 December 1989 Shibata
D524211 July 2006 Tsuchiya
D687360 August 2013 Gagnon
D687362 August 2013 Gagnon
8925862 January 2015 Ehlers
2013/0248654 September 2013 Henshaw
2014/0062884 March 2014 Davies
2014/0246886 September 2014 Savard
2015/0136904 May 2015 Savard
2016/0052632 February 2016 Mbanefo
Primary Examiner: Betton; Katrina A
Attorney, Agent or Firm: Lorenz & Kopf, LLP (LKGlobal)

Description



FIG. 1 is a first front perspective view of an aircraft crew rest showing our new design;

FIG. 2 is a front view thereof;

FIG. 3 is a cross section view thereof taken along line 3-3 of FIG. 2;

FIG. 4 is a front perspective view thereof with a front wall removed for further illustration of the interior of the aircraft crew rest;

FIG. 5 is a front view thereof with the front wall removed;

FIG. 6 is a cross section view thereof taken along line 6-6 of FIG. 5;

FIG. 7 is a cross section view thereof taken along line 8-8 of FIG. 6; and,

FIG. 8 is a cross section view thereof taken along line 8-8 of FIG. 6.

The broken lines illustrate structures and environment that form no part of the claimed design.

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