skip to main content

Title: Gas turbine combustion chamber with air scoops

This patent describes a gas turbine combustion chamber. It comprises: means for admission of fuel to the upstream end thereof and discharge of hot gases from the downstream end thereof, and a combustion chamber wall, having an outer surface, with apertures therethrough, and air scoops provided through the apertures to direct air into the combustion chamber.
Authors:
;
Publication Date:
OSTI Identifier:
6911959
Report Number(s):
US 4887432; A
PPN: US 7-255577A
Resource Type:
Patent
Resource Relation:
Patent File Date: 7 Oct 1988
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; GAS TURBINE ENGINES; COMBUSTION CHAMBERS; AIR FLOW; APERTURES; DESIGN; FUEL SYSTEMS; ENGINES; FLUID FLOW; GAS FLOW; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; OPENINGS 330103* -- Internal Combustion Engines-- Turbine