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,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,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冷器和氢气透平。

The gas turbine feeds on the fuel it pumps.

这台燃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轮机,通过模型预测分析了其性能,并与传燃轮机进行了比较。

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轮机将其派生为一型间冷循环大功率船用燃轮机的,并且原发动机燃发生器的通流部分和结大部分保持不变,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.

基于气体多变压缩以及等温涡燃烧技术,提出了一种改进性卡诺循环燃气,通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通流部分和结构大部分保持不变,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,提出了一的概括性卡诺循环燃气轮机,通过模型预测分析了性能,并与传燃气轮机行了比较。

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涡轮烧技术,提出了一种改进的概括性卡诺循环气轮机,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.

提出利成熟的简单循环气轮机将其派生为一型间冷循环大功率气轮机的新构想,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.

为了充分利液氢的低火，在氢能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.

提出利成熟的简单循环燃气轮机将其派生为一型间冷循环大功燃气轮机的新构想,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.

为了充分利液氢的低火，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.

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想,并且原发动机燃气发生器的通流部分大部分保持不变,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冷器氢气透平。

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,提出了一种改进的概括性卡燃气轮机,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.

提出利成熟的简单燃气轮机将其派生为一型间冷大功率燃气轮机的新构想,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.

为了充分利液氢的低温火，在氢能燃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。