Isomer Energy Source in Hybrid Jet Engines for High Altitude Reconnaissance Flight

Christopher E. Hamilton; Paul I. King; Milton E. Franke

首页> 外文期刊>Journal of Aircraft >Isomer Energy Source in Hybrid Jet Engines for High Altitude Reconnaissance Flight

【24h】

Isomer Energy Source in Hybrid Jet Engines for High Altitude Reconnaissance Flight

机译：用于高空侦察飞行的混合动力喷气发动机中的异构能源

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

An investigation was performed on the possibility of employing a triggered isomer heat exchanger (TIHE) as part of a hybrid heat source in an otherwise conventional turbojet engine. Reported is the application of such a long duration engine in a high-altitude long endurance surveillance and reconnaissance mission. Two-phase operation would include a switchover point, that is, an altitude and Mach number at which conventional combustion is replaced by the TIHE. A comparison of conventional and hybrid engines indicates a hybrid mixed-stream turbofan engine flying a part conventional and part TIHE mission, with a switchover at a Mach number of 0.4 at 40,000 ft, could provide weeks of endurance. Takeoff weight would be reduced by 20% due to lower fuel requirements.

机译：对在其他常规涡轮喷气发动机中使用触发式异构体热交换器（TIHE）作为混合热源的一部分的可能性进行了研究。据报道，这种长时间引擎在高空长时间耐力监视和侦察任务中的应用。两阶段运行将包括一个切换点，即TIHE取代常规燃烧的高度和马赫数。常规发动机和混合动力发动机的比较表明，混合型混合流涡扇发动机可以执行部分常规任务和部分TIHE任务，在40,000英尺时转换马赫数为0.4，可以提供数周的耐力。由于燃油需求降低，起飞重量将减少20％。

著录项

来源
《Journal of Aircraft》 |2004年第1期|p.151-155|共5页
作者
Christopher E. Hamilton; Paul I. King; Milton E. Franke;
展开▼
作者单位

U.S. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433;

展开▼
收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
关键词

相似文献

外文文献
中文文献
专利

1. Fuzzy Energy Management Scheme for a Hybrid Power Sources of High-Altitude Pseudosatellite [J] . J. I. Corcau, L. Dinca Modelling and simulation in engineering . 2020,第1期

机译：高空伪卫星混合动力源的模糊能量管理方案
2. Correction of the method of assessing exhaust emission during the flight of the aircraft, including impact of changes in flight altitude on engine performance parameters [J] . Marcin Nowacki, Damian Olejniczak Transportation Research Procedia . 2019,第15期

机译：纠正了在飞行过程中评估排气排放的方法，包括飞行高度变化对发动机性能参数的影响
3. Investigating the effect of engine speed and flight altitude on the performance of throttle body injection (TBI) system of a two-stroke air-powered engine [J] . Hassantabar Ali, Najjaran Ahmad, Farzaneh-Gord Mahmoud Aerospace science and technology . 2019,第MARa期

机译：研究发动机速度和飞行高度对两冲程气动发动机节气门喷油（TBI）系统性能的影响
4. Nuclear Energy Source in a Hybrid Jet Engine for High Altitude Reconnaissance Flight [C] . C. Hamilton, P. King, M. Franke Aerospace Sciences Meeting and Exhibit . 2003

机译：用于高空侦察飞行的混合动力喷气发动机中的核能源
5. Control of a helicopter engine in low-altitude flight. [D] . Jaw, Link Ching. 1991

机译：在低空飞行中控制直升机引擎。
6. A comparison of the delivery of inhaled drugs by jet nebulizer and vibrating mesh nebulizer using dual-source dual-energy computed tomography in rabbits: a preliminary [O] . Qixing Wang, Yuhao Liu, Zhengfang Zhu, 2020

机译：利用双源双能计算断层扫描的喷射雾化器和振动网雾化器递送吸入药物的比较：初步
7. Analysis of the Impact of Changes in Flight Speed and Altitude on Emission Indexes of Pollutants in Jet Engine Exhausts [O] . Małgorzata Pawlak, Michał Kuźniar 2019

机译：喷气发动机排放污染物排放指标对飞行速度和海拔高度影响的影响
8. Design Study of Triggered Isomer Heat Exchanger-Combustion Hybrid Jet Engine for High Altitude Flight. [R] . Hamilton, C. E. 2002

机译：高空飞行触发异构体换热器 - 燃烧混合式喷气发动机的设计研究。

Isomer Energy Source in Hybrid Jet Engines for High Altitude Reconnaissance Flight

摘要

著录项

相似文献

相关主题

期刊订阅