F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 3/06 (2006.01) F02C 3/06 (2006.01)
Patent
CA 2583083
The invention relates to a gas turbine intermediate structure (14) for being arranged between a first and a second gas turbine structure (8 and 9) in an axial direction (18) of a gas turbine (1). The intermediate structure (14) comprises a gas duct (5c) arranged for guiding a gas flow from a gas duct (5a) in the first structure (8) to a gas duct (5b) in the second structure (9). An inlet (19) of the intermediate structure gas duct (5c) is substantially displaced in a radial direction in relation to an outlet (20) of the intermediate structure gas duct (5c). At least one guide vane (28,29) is arranged in the intermediate structure gas duct (5c) for guiding the gas flow.
L'invention concerne une structure intermédiaire (14) de turbine à gaz destinée à être placée entre une première et une seconde structure (8 et 9) de turbine à gaz dans le sens axial (18) de ladite turbine à gaz (1). La structure intermédiaire (14) comprend un conduit de gaz (5c) agencé afin de guider un flux gazeux d'un conduit de gaz (5a) de la première structure (8) vers un conduit de gaz (5b) de la seconde structure (9). Une entrée (19) de conduit de gaz (5c) de la structure intermédiaire est sensiblement déplacée dans le sens radial en relation avec une sortie (20) de conduit de gaz (5c) de la structure intermédiaire. Au moins une ailette de guidage (28, 29) est installée dans le conduit de gaz (5c) de la structure intermédiaire afin de guider l'écoulement gazeux.
Larsson Jonas
Stroem Linda
Dennison Associates
Volvo Aero Corporation
LandOfFree
Gas turbine intermediate structure and a gas turbine engine... 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 intermediate structure and a gas turbine engine..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine intermediate structure and a gas turbine engine... will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1711647