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,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.

利用成熟的简单循环船用燃气轮机将其派生为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.

为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.

这台燃气轮机以它抽入的燃料为能。

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

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机,通过模型预测分析了其性能,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,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,了一种改进的概括性卡诺循环燃气轮机,通过模预测分析了其性能,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.

利用成熟的简单循环船用燃气轮机将其派生为一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.

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,提了一种改进的概括性卡诺循环燃气轮机,通过测分析了其性能,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.

提成熟的简单循环船燃气轮机将其派生为一间冷循环大功率船燃气轮机的新构想,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.

为了充分液氢的低温火，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.

这台气轮机以它抽入的料为能源。

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术,提出了一种改进的概括性卡诺气轮机,通过模型预测分析了其性能,并与传气轮机进行了比较。

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船用气轮机将其派生为一型间冷功率船用气轮机的新构想,并且原发动机气发生器的通流部分和结构部分保持不变,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.

为了充分利用液氢的低温火用，在氢能气轮机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,出了一种改进的概括性卡诺循环燃气轮机,通过模型预了其性能,并与传燃气轮机进行了。

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.

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预冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台机以它抽入的料为能源。

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烧技术,提出了一种改进的概诺循环机,通过模型预测分析了其能,并与传机进行了比较。

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机将其派生为一型间冷循环大功率船用机的新构想,并且原发动机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。

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，在氢能机循环中附加了一个空预冷器和氢透平。