The gas turbine feeds on the fuel it pumps.

这台燃气轮机入燃料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩及等温涡轮燃烧技术,提出了一种改进概括性卡诺循环燃气轮机,通过模型预测分析了其性能,并与传燃气轮机进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟简单循环船用燃气轮机将其派为一型间冷循环大功率船用燃气轮机新构想,并且原发动机燃气发通流部分和结构大部分保持不变,继承原机可靠性。

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.

为了充分利用液氢低温火用，在氢能燃气轮机循环中附加了一个空气预冷和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮机以它抽入的燃料能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩以及等温涡轮燃烧技术,提出了进的概括性卡诺循环燃气轮机,通过模型预测分析了其性能,并与传燃气轮机进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟的简单循环船用燃气轮机将其型间冷循环大功率船用燃气轮机的新构想,并且原发动机燃气发器的通流部分和结构大部分保持不变,以继承原机的可靠性。

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.

了充分利用液氢的低温火用，在氢能燃气轮机循环中附加了个空气预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气它抽入燃料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩及等温涡燃烧技术,提出了一种改进概括性卡诺循环燃气,过模型预测分析了其性能,并与传燃气进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟简单循环船用燃气将其派生为一型间冷循环大功率船用燃气新构想,并且原发动燃气发生器部分和结构大部分保持不变,继承原可靠性。

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.

为了充分利用液氢低温火用，在氢能燃气循环中附加了一个空气预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮机它抽入的燃料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多压缩及等温涡轮燃烧技术,提出了一种改进的概括性卡诺循环燃气轮机,通过模型预测分析了其性能,并与传燃气轮机进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟的简单循环船用燃气轮机将其派生为一型间冷循环大功率船用燃气轮机的新构想,并且原发动机燃气发生器的通流部分和结构大部分保持,继承原机的可靠性。

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.

为了充分利用液氢的低温火用，在氢能燃气轮机循环中附加了一个空气预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台轮机以它抽料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于体多变压缩以及等温涡轮烧技术,提出了一种改进概括性卡诺循环轮机,通过模型预测分析了其性能,并与传轮机进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟简单循环船用轮机将其派生为一型间冷循环大功率船用轮机新构想,并且原动机生器通流部分和结构大部分保持不变,以继承原机可靠性。

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.

为了充分利用液氢低温火用，在氢能轮机循环中附加了一个空预冷器和氢透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮机以它抽入的燃料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩以及等温涡轮燃烧技术,了一种改进的概括性卡诺循环燃气轮机,通过模型析了其性能,并与传燃气轮机进行了比。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

利用成熟的简单循环船用燃气轮机将其派生为一型间冷循环大功率船用燃气轮机的新构想,并且原发动机燃气发生器的通流部和结构大部保持不变,以继承原机的可靠性。

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.

为了充利用液氢的低温火用，在氢能燃气轮机循环中附加了一个空气冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮以它抽入的燃源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩以及等温涡轮燃烧技术,提出了一种改进的概括性卡诺循环燃气轮,通过模型预测分析了其性,并与传燃气轮进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟的简单循环船用燃气轮将其派生一型间冷循环大功率船用燃气轮的新构想,并且原燃气生器的通流部分和结构大部分保持不变,以继承原的可靠性。

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.

了充分利用液氢的低温火用，在氢燃气轮循环中附加了一个空气预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮机以它抽入的燃料能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体多变压缩以及等温涡轮燃烧技术,提种改进的概括性卡诺循环燃气轮机,通过模预测分析其性能,并与传燃气轮机进行比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提利用成熟的简单循环船用燃气轮机将其派生间冷循环大功率船用燃气轮机的新构想,并且原发动机燃气发生器的通流部分和结构大部分保持不变,以继承原机的可靠性。

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.

充分利用液氢的低温火用，在氢能燃气轮机循环中附加个空气预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃气轮以它抽入燃料为能源。

Based on polytrophic process of air compression and isothermal gas combustion inside the turbine, an improved gas turbine with generality Carnot cycle is suggested.

基于气体缩以及等温涡轮燃烧技术,提出了一种改进概括性卡诺循环燃气轮,通过模型预测分析了其性能,并与传燃气轮进行了比较。

A new concept is proposed,under which by utilizing a proven simple-cycle marine gas turbine a type of intercooling-cycle high-power marine gas turbine has been derived.

提出利用成熟简单循环船用燃气轮将其派生为一型间冷循环大功率船用燃气轮构想,并且原发动燃气发生器通流部分和结构大部分保持不,以继承原可靠性。

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.

为了充分利用液氢低温火用，在氢能燃气轮循环中附加了一个空气预冷器和氢气透平。