US 11,873,097 B2
Aircraft interior lavatory
Donald F. Cook, Arlington, WA (US); Liberty Harrington, Seattle, WA (US); Philipp Steiner, Seattle, WA (US); Robert K. Brauer, Seattle, WA (US); and Trevor Skelly, Mercer Island, WA (US)
Assigned to B/E Aerospace, Inc., Winston-Salem, NC (US)
Filed by B/E Aerospace, Inc., Winston-Salem, NC (US)
Filed on Jun. 29, 2021, as Appl. No. 17/362,163.
Application 17/362,163 is a continuation of application No. 16/819,878, filed on Mar. 16, 2020, granted, now 11,077,946.
Application 16/819,878 is a continuation of application No. 16/283,471, filed on Feb. 22, 2019, granted, now 10,625,862.
Application 16/283,471 is a continuation of application No. 15/258,529, filed on Sep. 7, 2016, granted, now 10,259,558.
Application 15/258,529 is a continuation of application No. 15/141,494, filed on Apr. 28, 2016, granted, now 9,463,878.
Application 15/141,494 is a continuation of application No. 14/709,378, filed on May 11, 2015, granted, now 9,365,292.
Application 14/709,378 is a continuation of application No. 14/043,500, filed on Oct. 1, 2013, granted, now 9,073,641.
Application 14/043,500 is a continuation of application No. 13/089,063, filed on Apr. 18, 2011, granted, now 8,590,838.
Claims priority of provisional application 61/346,835, filed on May 20, 2010.
Claims priority of provisional application 61/326,198, filed on Apr. 20, 2010.
Prior Publication US 2022/0119116 A1, Apr. 21, 2022
This patent is subject to a terminal disclaimer.
Int. Cl. B64D 11/02 (2006.01); B64C 1/10 (2006.01); B64D 11/06 (2006.01); B64F 5/00 (2017.01)
CPC B64D 11/02 (2013.01) [B64C 1/10 (2013.01); B64D 11/06 (2013.01); B64D 11/064 (2014.12); B64F 5/00 (2013.01); Y02T 50/40 (2013.01)] 26 Claims
OG exemplary drawing
 
1. An enclosure for a cabin of an aircraft, comprising:
an aft wall; and
a forward wall comprising:
an upper portion;
a lower portion; and
a middle portion below the upper portion;
wherein the lower portion of the forward wall is adapted to receive at least a portion of a seat support of a seat aftward of at least a portion of the lower portion for mounting the seat support to the aircraft; and
wherein the forward wall is adapted to receive loads from a structure within the cabin.