Turbine shroud segment apparatus for reusing cooling air
申请公布号:US6899518(B2)
申请号:US20020325941
申请日期:2002.12.23
申请公布日期:2005.05.31
发明人:LUCAS TERRENCE;BEDARD DOMINIC;DANIEL AMIR;SYNNOTT REMY
分类号:F01D9/04;F01D11/08;F01D25/12;(IPC1-7):F04D31/00
主分类号:F01D9/04
摘要:A cooled turbine shroud segment for a gas turbine engine, having an axially extending shroud ring segment with an inner surface, an outer surface, an upstream flange and a downstream flange. The flanges mount the shroud ring within an engine casing. A perforated cooling air impingement plate is disposed on the outer surface of the shroud ring between the upstream flange and the downstream flange, with an impingement plenum defined between the impingement plate and the outer surface. Axially extending cooling bores in the ring segment extend between the impingement plenum and an outlet. A trough adjacent the outlet directs cooling air from the outlet towards a downstream stator vane to cool the stator vane.
METHOD OF RESOLVING BICYCLIC IMINO-ALPHA-CARBOXYLIC ACID ESTER RACEMATES
THIAZOLO-AND THIAZINOBENZIMIDAZOLES
Method for synthesis gas generation used in methanol synthesis.
Process for the preparation of S-alkyl-isothioureidoazines.
GAS PERMEABLE THROMBO-RESISTANT COATINGS AND METHODS OF MANUFACTURE
NOVEL SUBSTITUTED TAXANES AND PHARMACEUTICAL COMPOSITIONS CONTAINING THEM
ALKOXY SUBSTITUTED TAXANES AND PHARMACEUTICAL COMPOSITIONS CONTAINING THEM
IMPROVEMENTS IN OR RELATING TO A MICROWAVABLE FOOD PRODUCT
REGISTRATION OF SERVO INDEXED WEBS