Member for locking ring sectors onto a turbomachine casing,...

Details Member for locking ring sectors onto a turbomachine casing,... Member for locking ring sectors onto a turbomachine casing,...

2008-09-05

2011-10-18

Fourson, III, George (Department: 2823)

Rotary kinetic fluid motors or pumps

Working fluid passage or distributing means associated with...

Casing having multiple parts releasably clamped

Reexamination Certificate

active

08038393

ABSTRACT:
The present invention relates to a locking member (24) for a device for attaching ring sectors to an aircraft turbomachine casing, said member comprising two longitudinal clamping branches (28, 30) extending rearward and connected at their rear ends by a transverse connecting branch (32), their front ends being intended, between them, to press at least one ring sector (16) against at least one casing element (14). According to the invention, the member (24) further comprises means (42) allowing it to be grasped, these means being arranged such that they project rearward from the transverse branch (32).

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patent: 2010/0058765 (2010-03-01), Duval et al.
patent: 2011/0076135 (2011-03-01), Gendraud et al.
patent: 0 967 364 (1999-12-01), None
patent: 1 099 826 (2001-05-01), None
patent: 2 887 920 (2007-01-01), None

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