System Study for Axial Vane Engine Technology

 
9781287236108: System Study for Axial Vane Engine Technology

The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i.e., Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems.

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Patrick R Badley
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ISBN 10: 1287236103 ISBN 13: 9781287236108
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Book Description Bibliogov, United States, 2013. Paperback. Book Condition: New. Language: English . Brand New Book ***** Print on Demand *****.The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i.e., Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems. Bookseller Inventory # AAV9781287236108

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Patrick R Badley
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Book Description Bibliogov, United States, 2013. Paperback. Book Condition: New. Language: English . Brand New Book ***** Print on Demand *****. The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i.e., Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems. Bookseller Inventory # AAV9781287236108

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Patrick R. Badley
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Book Description BiblioGov. Paperback. Book Condition: New. This item is printed on demand. 84 pages. Dimensions: 9.7in. x 7.4in. x 0.2in.The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i. e. , Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems. This item ships from La Vergne,TN. Paperback. Bookseller Inventory # 9781287236108

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NASA Technical Reports Server (NTRS)
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Book Description BiblioGov, 2016. Paperback. Book Condition: New. PRINT ON DEMAND Book; New; Publication Year 2016; Not Signed; Fast Shipping from the UK. No. book. Bookseller Inventory # ria9781287236108_lsuk

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Badley, Patrick R.
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Book Description BiblioGov. Book Condition: New. Worldwide shipping. FREE fast shipping inside USA (express 2-day delivery also available). Tracking service included. Ships from United States of America. Bookseller Inventory # 1287236103

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