US 12,480,331 B1
Shear pin latch receptacle assembly for aircraft doors
Julian Rupert Barrett, Savannah, GA (US); and Marc R. Lambert, Reidsville, NC (US)
Assigned to AMERICAN HONDA MOTOR CO., INC., Torrance, CA (US)
Filed by American Honda Motor Co., Inc., Raymond, OH (US)
Filed on Jan. 21, 2025, as Appl. No. 19/032,968.
Int. Cl. E05B 15/02 (2006.01); B64C 1/14 (2006.01)
CPC E05B 15/024 (2013.01) [B64C 1/1461 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A shear pin latch receptacle assembly, comprising:
an inner bushing;
an outer eccentric bushing including a first inner bore configured to receive the inner bushing;
a stabilizer member configured to be assembled with the inner bushing and the outer eccentric bushing to form a subassembly; and
a housing including a mounting plate and a barrel, the barrel defining a second inner bore configured to receive the subassembly;
wherein the outer eccentric bushing is rotatable relative to the housing in order to adjust the receptacle assembly; and
wherein, when the receptacle assembly is assembled, the stabilizer member prevents rotation of the inner bushing with respect to the housing.