Patent · US Active

Device and method for the detachable connection of structural parts, in particular in an aircraft

US7976078B2 · kind B2 · utility

3Cited by

18References

18Claims

0Family size

Assignee

AIRBUS DEUTSCHLAND GMBH · DE

Inventors

Herbert Steinbeck · Hamburg, DE
Konstantin Wagner · Laupheim, DE

Key dates

Filing date	Feb 23, 2009
Grant date	Jul 12, 2011
Priority date	—
Expiry date	Feb 23, 2029

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY10T292/1043
WIPO fieldCivil engineering
WIPO sectorOther fields

Abstract

A device (10) for the detachable connection of structural parts (80, 84) in an aircraft, comprising a clamping lever arrangement (12) associated with a first structural part (80) and a clamping pin (14) associated with a second structural part (84), wherein the clamping lever arrangement (12) comprises an eccentric shaft (20) rotatably mounted about a rotation axis (A) on the first structural part (80), a clamping lever (16) mounted eccentrically and swivellably with respect to the eccentric shaft (20) and a driving bushing (18) rotatably mounted relative to the eccentric shaft (20) about the rotation axis (A) and coupled in a geared manner to the clamping lever (16), wherein the clamping lever arrangement (12) can furthermore be displaced between a release position, a readiness position and a locking position.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.