gas turbine造句
61 In this dissertation one foreign gas turbine is researched systematically.
62 Making use of inlet air cooling system, the gas turbine output power can be increased in higher temperature ambient condition.
63 Effects of squealer tips on blade aerodynamic performances and tip heat transfer in a gas turbine were investigated.
64 Realize localization of IGCC generator unit and heavy gas turbine.
65 Gas turbine engines use the Brayton cycle. Wankel rotary engines use the Otto cycle, but they do it in a very different way than four-stroke piston engines.
66 A gas turbine combustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side.
67 Gas turbine power steam power and system net power all decline as atmosphere temperature increasing.
68 The throat area of turbine nozzle which is very important in gas turbine engine's design and manufacture must be controlled strictly.
69 Cutaway of the PW 4000112 - in ( 284.48 cm ) gas turbine engine, showing fan bypass section.
70 Take the natural gas booster station built in 9E class gas turbine combination cycle power plant for example, its function and system constitution were introduced and analyzed.
71 Mister Li is skilled at maintaining the gas turbine engine.
72 Introduces the materials selection, arrangement, force analysis and design points of catalyst cracking flue gas turbine.
73 With the model of steam - injected gas turbine, the closed - loop simulation research is done.
74 The overall level of operational reliability of conventional thermal units (excluding gas turbine units) in 2000 was higher than1999, the equivalent availability of thermal units was 90.30%.
75 This paper introduced the stator coil manufacturing technology of GE390H gas turbine generator.
76 The high temperature gas cooled reactor (HTGR) coupled with the gas turbine cycle is considered as one of the leading candidate concepts for future nuclear power deployment.
77 It can be used properly by adding a new designed regenerator in an existing simple cycle gas turbine to make this gas turbine system reach an optimal performance.
78 To fully utilize the low temperature exergy of liquid hydrogen, installed additionally in a hydrogen energy based gas turbine cycle is an air precooler and hydrogen turbine.
79 The numerical results agree well with the corresponding experimental data, which are the basis of the prediction of infrared radiation distribution of a marine gas turbine exhaust system.
80 The RE - aluminizing technique and coating structure of gas turbine blade made of alloy M 38 G are studied.
81 Stability of surface materials with changing temperature is a major consideration, given the wide operating temperature range experienced by supersonic gas turbine powered military aircraft.
82 The blade a gas turbine fractured and the unIt'stopped unnaturally a refinery.
83 Through calculation, some important conclusions for gas turbine with injecting water evaporative intercooling in compressor are obtained and a proposal for interstage water injecting is put forward.
84 This paper gives some experiences and views the author has gained in the manufacture of marine gas turbine split casings.
85 The operation test has shown that the said package features a good sound isolation performance, which approaches the world advanced level of sound proof quality of gas turbine packages.
86 In order to raise the efficiency and the specific output of the gas turbine, the method of the precool inlet is used.
87 Also, this is regimes invented the first airline gas turbine.
88 Aircrafts have continued to fly on aviation fuels, kerosene fuel or a wide-cut fuel blended from heavy naphtha and kerosene, burned in the gas turbine combustor for many years.
89 The invention relates to a gas turbine premixer with internal cooling. A system that includes a turbine fuel nozzle (144) comprising an air-fuel premixer (170).
90 Therefore, by lowering the temperature of inlet air power and efficiency of gas turbine generators.
1234