Some content of this application is unavailable at the moment.
If this situation persist, please contact us atFeedback&Contact
1. (WO1998051917) METHOD AND APPARATUS FOR COOLING A TURBINE WITH COMPRESSED COOLING AIR FROM AN AUXILIARY COMPRESSOR SYSTEM
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/1998/051917 International Application No.: PCT/US1998/008628
Publication Date: 19.11.1998 International Filing Date: 29.04.1998
Chapter 2 Demand Filed: 14.12.1998
IPC:
F02C 7/18 (2006.01)
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
C
GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
7
Features, component parts, details or accessories, not provided for in, or of interest apart from, groups F02C1/-F02C6/158; Air intakes for jet-propulsion plants
12
Cooling of plants
16
characterised by cooling medium
18
the medium being gaseous, e.g. air
Applicants:
SIEMENS WESTINGHOUSE POWER CORPORATION [US/US]; 186 Wood Avenue South Iselin, NJ 08830, US
Inventors:
BRIESCH, Michael, Scot; US
ALBA, Jorge, J.; US
BOHINSKY, Brian; US
Agent:
LENART, Robert, P.; Westinghouse Electric Corporation Law Dept. 11 Stanwix Street Pittsburgh, PA 15222-1384, US
ABELES, Daniel, C.; Eckert Seamans Cherin & Mellott, LLC 600 Grant Street, 44th Floor Pittsburgh, PA 15219, US
Priority Data:
08/855,42813.05.1997US
Title (EN) METHOD AND APPARATUS FOR COOLING A TURBINE WITH COMPRESSED COOLING AIR FROM AN AUXILIARY COMPRESSOR SYSTEM
(FR) PROCEDE ET DISPOSITIF DE REFROIDISSEMENT DE TURBINE RECEVANT DE L'AIR DE REFROIDISSEMENT COMPRIME PRODUIT PAR UN SYSTEME DE COMPRESSEUR AUXILIAIRE
Abstract:
(EN) A combustion turbine system (10) is provided with compressed cooling air (50) by an auxiliary air compressor (54) system. The combustion turbine system (10) has a system air compressor (12), a combustor (14) and a turbine (16). The auxiliary air compressor (59) system receives an air stream and produces a compressed cooling air stream (50) therefrom. The cooling air stream (50) is then directed to the combustion turbine system (10) and is used to cool the turbine (16).
(FR) L'invention concerne un système de turbine à combustion (10) recevant de l'air de refroidissement comprimé (50) produit par un système de compresseur d'air auxiliaire (54). Le système de turbine à combustion (10) possède un compresseur d'air (12), une chambre de combustion (14) et une turbine (16). Le système de compresseur d'air auxiliaire (54) reçoit un flux d'air à partir duquel il fournit un flux d'air de refroidissement comprimé (50). Ce flux d'air de refroidissement (50) est ensuite fourni au système de turbine à combustion (10) et utilisé pour refroidir la turbine (16).
front page image
Designated States: CA, CN, KR, MX, PL
European Patent Office (AT, BE, CH, CY, DE, DK, ES, FI, FR, GB, GR, IE, IT, LU, MC, NL, PT, SE)
Publication Language: English (EN)
Filing Language: English (EN)