F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 17/16 (2006.01) F01D 9/02 (2006.01)
Patent
CA 2427060
The invention relates to a stator (1) for a gas tubrine comprising a stator structure (2) having a through-duct (3) for a gas through-flow, a circumferential member (6), which is arranged at a radial distance from the stator structure and is operatively coupled to the stator structure, and at least one member for keeping a distance between the stator structure and the circumferential member. The spacing member has resilient characteristics in the radial direction of the stator.
L'invention concerne un stator (1) convenant pour une turbine à gaz. Ce stator comprend une structure (2) qui comporte un passage (3) traversant pour le flux de gaz, un élément (6) périphérique disposé à une distance radiale de la structure du stator et connecté de manière opérationnelle avec cette dernière, et au moins un élément permettant de maintenir la distance séparant la structure de l'élément périphérique. Cet élément espaceur présente des propriétés élastiques dans la direction radiale du stator.
Dennison Associates
Volvo Aero Corporation
LandOfFree
Gas turbine stator does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Gas turbine stator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine stator will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1677376