About 461 results
Showing the first 200 results.
https://drivepatents.com/patents/979078 · 5 Feb 2014
A turbine is provided which can reduce variations in mass flow at throats even when the flow rate of fluid is low or high, to prevent a decrease in performance. The invention employs a turbine including a turbine rotor (80) which has turbine blades (82); a...
https://drivepatents.com/patents/979033 · 5 Feb 2014
It is an object to reduce the pumping work, and to improve the fuel consumption rate by preventing the injection path part of a fuel gas supply device from protruding from the wall surface of the inlet path, and reducing the circulation resistance against ...
https://drivepatents.com/patents/979024 · 5 Feb 2014
Provided is a turbocharger that compresses combustion air in an internal combustion engine and that force-feeds the high-density air into a combustion chamber of the internal combustion engine. The turbocharger includes a turbine rotor blade that is rotati...
https://drivepatents.com/patents/979006 · 5 Feb 2014
A combustor (10) according to the invention includes: a combustor basket (14) in which compressed air and fuel are mixed with each other and the mixture is combusted; a transition piece (17) in which a tip portion of the combustor basket (14) is inserted w...
https://drivepatents.com/patents/979001 · 5 Feb 2014
A pilot nozzle, a gas turbine combustor and a gas turbine are provided with: a nozzle main body (71) having a fuel passage way (72); a covering (75) that forms an interior air passageway (78) by being positioned so as to form a predetermined gap in the ext...
https://drivepatents.com/patents/979008 · 5 Feb 2014
Disclosed is a method for operating a gas compressor which compresses a gas fuel, a supply condition of which fluctuates, and is provided with a suction flow rate adjustment mechanism, wherein the limit pressure ratio that defines the operational limit of ...
https://drivepatents.com/patents/978984 · 5 Feb 2014
A gas turbine is provided with: a turbine rotor blade (33); a turbine stator blade (32); a dividing ring (52) surrounding the turbine rotor blade (33) in a circumferential direction; an outer shroud (51) surrounding the turbine stator blade (32) in the cir...
https://drivepatents.com/patents/978982 · 5 Feb 2014
This turbine exhaust structure and gas turbine are configured with a turbine cylinder (26) being provided that configures a combustion gas pathway (›) by forming a tubular shape, and an exhaust diffuser (31) that configures an exhaust gas pathway (B) by ...
https://drivepatents.com/patents/978974 · 5 Feb 2014
A cylinder structure satisfies the following conditions: 12% ¤ d/a ¤ 27%, where d is a distance between a cylinder inner surface 12a and an exhaust valve member 20b, and a is a diameter of the exhaust valve member; 40% ¤ c/b ¤ 50%, where c is a length ...
https://drivepatents.com/patents/978965 · 5 Feb 2014
It is an object of the present invention to achieve the improvement of the combustion efficiency in the combustion chamber and the improvement of the fuel consumption rate by forming, in the inner circumferential surface of a sleeve into which a projection...