Energy and Power Engineering

氢燃烧

Hydrogen combustion

A thermodynamic process involving the controlled reaction of hydrogen fuel with air to produce energy, analyzed here for retrofitting a gas turbine in an aviation lab. / 一种涉及氢燃料与空气受控反应以产生能量的热力学过程，本文针对航空实验室燃气轮机的改造进行了分析。

Knowledge type: 工艺技术
First proposed or discovered
Proposer: Turkey Farm member
Creator: 农场主
Last updated: 2026-10-28 21:01:23

Sub-knowledge points

Thermodynamic feasibility analysisRetrofitting existing gas turbine infrastructureCombustion stability controlDilution air mixing optimization

Higher-order knowledge points

Hydrogen Aviation Lab (HAL) infrastructureZero carbon emissions in aviationAuxiliary Power Unit (APU) operation

Main parameters and performance indicators

Fuel-to-air ratio (FAR): 0.016173Hydrogen mass flow: 0.016006 kg/sEquivalence ratio: 0.24737Turbine entry temperature (TET): 1,293.15 KDilution air fraction (ε): 55.012%Air mass flow: 2.2 kg/s

Open problems

No unresolved problem recorded yet

Related literature

ranked by community stars

Retrofitting the Hydrogen Aviation Lab for hydrogen combustion: a thermodynamic analysisOpen source

氢燃烧

Sub-knowledge points

Higher-order knowledge points

Main parameters and performance indicators

Open problems

Related products and links