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contributor authorK. H. Pech
contributor authorN. L. Downing
date accessioned2017-05-08T23:00:50Z
date available2017-05-08T23:00:50Z
date copyrightDecember, 1976
date issued1976
identifier issn0098-2202
identifier otherJFEGA4-26904#619_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88722
description abstractFuel pumps and metering systems are becoming more complex and expensive to meet the high performance requirements of advanced gas turbine engines. A simple, inlet throttled, centrifugal pump integrated with a retracting vane starting element provides the potential for a reliable, high performance design capable of reducing the cost, weight, and temperature rise of the fuel system. This paper presents the results of recent efforts to develop the retracting vane element and to integrate it with a vapor core centrifugal pump in order to meet the fuel performance and functional requirements of an advanced gas turbine main fuel pump.
publisherThe American Society of Mechanical Engineers (ASME)
titleDevelopment of a Retracting Vane/Centrifugal Main Fuel Pump for Gas Turbine Engines
typeJournal Paper
journal volume98
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448427
journal fristpage619
journal lastpage625
identifier eissn1528-901X
keywordsFuel pumps
keywordsGas turbines
keywordsCentrifugal pumps
keywordsFuel systems
keywordsDesign
keywordsWeight (Mass)
keywordsTemperature
keywordsVapors AND Fuels
treeJournal of Fluids Engineering:;1976:;volume( 098 ):;issue: 004
contenttypeFulltext


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