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121-130 trong số 313 kết quả
Variable volume combustor with nested fuel manifold system [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.13
 
Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section [electroni...
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.13
 
Low gloss UV-cured coatings for aircraft [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2014
Bộ sưu tập: Metadata
ddc:  629.133
 
Transition duct assembly with modified trailing edge in turbine system [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.132
 
Swirling midframe flow for gas turbine engine having advanced transitions [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.13
 
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, U.S. Dept. of Energy , 2014
Bộ sưu tập: Metadata
ddc:  629.132
 
Apparatus for mixing fuel in a gas turbine nozzle [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.133
 
Device for improved air and fuel distribution to a combustor [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2016
Bộ sưu tập: Metadata
ddc:  629.13
 
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, U.S. Dept. of Energy , 2015
Bộ sưu tập: Metadata
ddc:  629.135
 
Gas turbine engine with radial diffuser and shortened mid section [electronic resource]
Tác giả:
Xuất bản: Oak Ridge, Tenn: Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy , 2015
Bộ sưu tập: Metadata
ddc:  629.1343
 

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