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Title: Louver construction for liner of gas turbine engine combustor

Abstract

This invention relates to an improved combustor liner for a gas turbine power plant. The liner is constructed from a plurality of louvers that include a lip and cooling means for defining a cooling film of air flow adjacent the liner. Means are provided for preventing lip closure which in turn is detrimental to film cooling.

Inventors:
;
Publication Date:
OSTI Identifier:
5811486
Patent Number(s):
US 4184326
Assignee:
United Technologies Corp IFI; EDB-82-057223
Resource Type:
Patent
Resource Relation:
Patent File Date: Filed date 30 Aug 1977; Other Information: PAT-APPL-829120
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; COMBUSTORS; DESIGN; LINERS; GAS TURBINE ENGINES; AIR FLOW; COOLING; ENGINES; FLUID FLOW; GAS FLOW; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; 330103* - Internal Combustion Engines- Turbine

Citation Formats

Pane, F.C., and Sepulveda, D. Louver construction for liner of gas turbine engine combustor. United States: N. p., 1980. Web.
Pane, F.C., & Sepulveda, D. Louver construction for liner of gas turbine engine combustor. United States.
Pane, F.C., and Sepulveda, D. Tue . "Louver construction for liner of gas turbine engine combustor". United States.
@article{osti_5811486,
title = {Louver construction for liner of gas turbine engine combustor},
author = {Pane, F.C. and Sepulveda, D.},
abstractNote = {This invention relates to an improved combustor liner for a gas turbine power plant. The liner is constructed from a plurality of louvers that include a lip and cooling means for defining a cooling film of air flow adjacent the liner. Means are provided for preventing lip closure which in turn is detrimental to film cooling.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {1980},
month = {1}
}