F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 25/24 (2006.01) F16B 2/24 (2006.01)
Patent
CA 2724256
The invention relates to a locking member (24) for a device used to fasten ring sectors on the casing of an aircraft turbine engine, wherein the member has two clamping arms (28, 30) connected together at the rear end thereof by a connection arm (32) extending substantially parallel to the general spacing direction between the two clamping arms. According to the invention, the member is provided, on either side of a virtual median plane (P2) orthogonal to the circumferential direction, with a passage (42) for gripping the member, each passage being formed through said connection arm (32) and extending along a guide line (44) substantially parallel to the spacing direction.
La présente invention se rapporte à un organe de verrouillage (24) pour dispositif de fixation de secteurs d'anneau sur un carter de turbomachine d'aéronef, l'organe présentant deux branches de serrage (28, 30) raccordées entre elles à leur extrémité arrière par une branche de raccord (32) s'étendant sensiblement parallèlement à une direction générale d'espacement des deux branches de serrage. Selon l'invention, l'organe est pourvu, de part et d'autre d'un plan médian fictif (P2) orthogonal à ladite direction circonférentielle, d'un passage (42) permettant la préhension de l'organe, chaque passage étant pratiqué dans la branche de raccord (32), en s'étendant selon une ligne directrice (44) sensiblement parallèle à la direction d'espacement.
Goudreau Gage Dubuc
Snecma
LandOfFree
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