川崎重工完成氢燃料航空发动机测试 实现世界顶尖低氮氧化物排放Kawasaki Heavy Industries Completes Hydrogen Fuel Aircraft Engine Test, Achieves World-Leading Low Nitrogen Oxide Emissions

日本当地时间10月8日,川崎重工宣布成功完成一款氢燃料航空发动机的测试,在日本首次实现了世界领先的低氮氧化物(NOx)排放水平。这台小型航空发动机全程采用100%氢燃料供给,搭载川崎重工新开发的低NOx氢燃烧器。
纯氢燃烧能够彻底消除二氧化碳排放,但氢气层流燃烧速度约为传统航空煤油Jet A-1的十倍量级,绝热火焰温度超过2200摄氏度。在常规燃气轮机燃烧室中,这类局部高温区会加速Zeldovich机理反应,使热力型氮氧化物生成呈指数式上升。为破解这一难题,川崎重工将原本为发电用燃气轮机开发并已实现商业化的专利微混合燃烧技术,引入到航空领域。
该技术的核心思路,是把整体燃烧分散为众多微型火焰,而不是把燃料集中送入单一的大型火焰区。具体做法是将纯氢燃料分配到大量微型燃料喷注点,与局部横向气流相互作用,使反应区扩散分布于众多微火焰之中,从而大幅缩短单个火焰区的物理体积以及燃烧气体在峰值温度下的停留时间,抑制局部高温热点的形成,显著降低氮氧化物排放浓度。测试结果表明,该燃烧室在纯氢燃烧条件下能够提供稳定的火焰锚定、不发生回火,同时实现世界顶尖水平的低氮氧化物排放。
本次测试在秋田县日本宇宙航空研究开发机构(JAXA)能代火箭试验中心进行,试验范围覆盖航空发动机实际工作的全部运行区间,并非单一稳态工况测试。验证参数依次包括点火启动与冷态起动动态、发动机转速提升并跨越怠速区间、模拟中空巡航条件的稳态运行、瞬态加速与减速扫掠,直至受控断油与发动机停车全流程。在所有工况切换过程中,设备均维持稳定燃烧状态,推力输出符合预期。
该项目隶属于日本新能源产业技术综合开发机构(NEDO)“下一代飞机开发”绿色创新基金项目下的“氢燃料飞机核心技术开发”项目,项目周期设定为2021年至2030年,研发目标是攻克可实际应用于氢燃料航空发动机的氢燃烧技术与配套系统,为商业化应用打下基础。在此之前,川崎重工已于2024年10月完成小型氢燃料航空发动机运行试验,并于2025年11月完成日本首次航空器液氢储罐加注验证演示,航发燃烧环节与燃料储存环节同步推进,补齐氢飞机两大核心硬件。
从此次试验结果看,该燃烧室可以实现全球顶尖水平的低氮氧化物排放,有助于满足国际民航组织(ICAO)持续收紧的航空动力排放规则要求,解决氢航空动力落地过程中的排放难题。下一步,川崎重工将开展整机一体化地面试验,评估飞行器机体、发动机、液氢储罐与各类配套系统协同工作的性能与可行性,进一步加快实现氢燃料飞机所需关键技术的开发。
On October 8, local time in Japan, Kawasaki Heavy Industries announced that it had successfully completed testing of a hydrogen-fueled aircraft engine, achieving a world-leading low nitrogen oxide (NOx) emission level in Japan for the first time. This small aircraft engine uses 100% hydrogen fuel throughout and is equipped with Kawasaki Heavy Industries' newly developed low-NOx hydrogen burner.
Pure hydrogen combustion can completely eliminate carbon dioxide emissions, but the laminar combustion speed of hydrogen is about ten times that of conventional aviation kerosene Jet A-1, and the adiabatic flame temperature exceeds 2200 degrees Celsius. In conventional gas turbine combustors, such local high-temperature zones accelerate Zeldovich mechanism reactions, causing thermal NOx formation to rise exponentially. To solve this problem, Kawasaki Heavy Industries introduced its patented micro-mixing combustion technology, originally developed for power generation gas turbines and already commercialized, into the aviation field.
The core idea of this technology is to disperse the overall combustion into numerous micro flames, rather than concentrating the fuel into a single large flame zone. The specific approach is to distribute pure hydrogen fuel to a large number of micro fuel injection points, interacting with local crossflows, so that the reaction zones are diffusely distributed among many micro flames. This greatly reduces the physical volume of a single flame zone and the residence time of combustion gases at peak temperatures, suppresses the formation of local high-temperature hotspots, and significantly lowers nitrogen oxide emission concentrations. Test results show that under pure hydrogen combustion conditions, this combustion chamber can provide stable flame anchoring without flashback, while achieving world-class low nitrogen oxide emissions.
This test was conducted at the Noshiro Rocket Test Center of the Japan Aerospace Exploration Agency (JAXA) in Akita Prefecture. The scope of the test covered the entire operational range of an aircraft engine, rather than a single steady-state condition test. The verification parameters included ignition start and cold start dynamics, engine speed increase passing through the idle range, steady-state operation simulating hollow cruise conditions, transient acceleration and deceleration sweeps, up to controlled fuel cut-off and full engine shutdown. Throughout all operating mode transitions, the equipment maintained stable combustion, and the thrust output met expectations.
This project is part of the Japan New Energy and Industrial Technology Development Organization (NEDO) 'Next-Generation Aircraft Development' Green Innovation Fund project under the 'Hydrogen Fuel Aircraft Core Technology Development' initiative. The project period is set from 2021 to 2030, with the research and development goal of overcoming hydrogen combustion technology and supporting systems that can be practically applied to hydrogen-fueled aircraft engines, laying the foundation for commercial application. Prior to this, Kawasaki Heavy Industries completed the operation test of a small hydrogen-fueled aircraft engine in October 2024 and carried out Japan's first hydrogen aircraft liquid hydrogen tank fueling verification demonstration in November 2025. The advancement of the engine combustion stage and the fuel storage stage is simultaneous, completing the two core hardware components of hydrogen aircraft.
Based on the results of this test, the combustion chamber can achieve globally leading levels of low nitrogen oxide emissions, helping to meet the increasingly stringent aviation power emission regulations of the International Civil Aviation Organization (ICAO) and addressing the emission challenges during the implementation of hydrogen aircraft propulsion. The next step for Kawasaki Heavy Industries is to conduct integrated ground tests of the entire machine to evaluate the performance and feasibility of the coordinated operation of the aircraft body, engine, liquid hydrogen tank, and various supporting systems, further accelerating the development of key technologies required for hydrogen-powered aircraft.
[Source: Kawasaki Heavy Industries]
[Editor: Xiao Neng]
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