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11-20 trong số 56 kết quả
Airfoil cooling with internal cavity displacement features [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2019
Bộ sưu tập: Metadata
ddc:  629.132
 
Cooling system for fuel nozzles within combustor in a turbine engine [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2019
Bộ sưu tập: Metadata
ddc:  623.8
 
Advanced Liquid Cooling for a Traction Drive Inverter Using Jet Impingement and Microfinned Enhanced Surfaces [electronic resource] : Preprint
Tác giả:
Xuất bản: Golden Colo Oak Ridge Tenn: National Renewable Energy Laboratory US Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2014
Bộ sưu tập: Metadata
ddc:  621.3
 
Ducting arrangement for cooling a gas turbine structure [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2015
Bộ sưu tập: Metadata
ddc:  629.132
 
Industrial stator vane with sequential impingement cooling inserts [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2013
Bộ sưu tập: Metadata
ddc:  621.43
 
System, methods, and apparatus for engine cooling system management [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2017
Bộ sưu tập: Metadata
ddc:  629.28
 
Compressor bleed cooling fluid feed system [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2014
Bộ sưu tập: Metadata
ddc:  629.2
 
Compound cooling flow turbulator for turbine component [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2014
Bộ sưu tập: Metadata
ddc:  629.132
 
Integrated axial and tangential serpentine cooling circuit in a turbine airfoil [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2015
Bộ sưu tập: Metadata
ddc:  629.135
 
Sequential cooling insert for turbine stator vane [electronic resource]
Tác giả:
Xuất bản: Oak Ridge Tenn: Distributed by the Office of Scientific and Technical Information US Dept of Energy, 2017
Bộ sưu tập: Metadata
ddc:  629.28
 

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