US 11,772,772 B2
Buffer zone for interior aircraft features
Bruce Malek, Senneville (CA); Stefan Holowka, Montreal (CA); and Nikolas Beaudin, Montreal (CA)
Assigned to BOMBARDIER INC., Dorval (CA)
Filed by BOMBARDIER INC., Dorval (CA)
Filed on Apr. 14, 2021, as Appl. No. 17/230,340.
Application 17/230,340 is a continuation of application No. 15/306,241, granted, now 11,001,361, previously published as PCT/IB2015/052876, filed on Apr. 20, 2015.
Claims priority of provisional application 61/984,631, filed on Apr. 25, 2014.
Prior Publication US 2021/0237844 A1, Aug. 5, 2021
Int. Cl. B64C 1/06 (2006.01); B64D 11/00 (2006.01); B64F 5/10 (2017.01); B64C 1/10 (2006.01)
CPC B64C 1/066 (2013.01) [B64C 1/10 (2013.01); B64D 11/0023 (2013.01); B64F 5/10 (2017.01); B64D 2011/0046 (2013.01)] 2 Claims
OG exemplary drawing
 
1. An aircraft personal service unit configuration, comprising:
a personal service unit;
a bulkhead;
a transition end cap disposed on the bulkhead, the transition end cap comprising an attachment end attached to the bulkhead and a protrusion protruding from the attachment end and extending behind an end of the personal service unit, wherein the attachment end and the protrusion of the transition end cap form a L-shaped angle bracket; and
a soft seal element for biasing the transition end cap against the personal service unit, wherein the soft seal element is located at an end of the protrusion of the transition end cap;
wherein the protrusion of the transition end cap and the personal service unit are in sliding engagement with one another.