Injector assembly for liquid fueled rocket engines Patent

机译：用于液体燃料火箭发动机的喷射器组件专利

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摘要

Propellant injection assembly having individually removable and replaceable nozzles for liquid fueled rocket engines

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作者
Escher, W. J. D.;
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年度 1966
页码 1-6
总页数 6
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FUEL INJECTION; LIQUID INJECTION; NOZZLE DESIGN; COMBUSTION CHAMBERS; LIQUID ROCKET PROPELLANTS;

机译：燃油喷射;液体注射;喷嘴设计;燃烧室;液体火箭推进剂;

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专利

1. Extreme fuel-rich combustion characteristics of RBCC embedded rocket engine with gas-liquid shear coaxial injectors in continuously varying mixture ratios [J] . Qinglian Li, Peng Cheng, Zhongtao Kang, Proceedings of the Institution of Mechanical Engineers . 2015,第g4期

机译：RBCC嵌入式火箭发动机的气-液剪切同轴喷射器在连续变化的混合比下具有极高的富燃料燃烧特性
2. Study on Breakup Length of Liquid Jet by Liquid-Gas Coaxial Injector: Evaluation of Atomization Characteristics of Rocket Engine Injectors [J] . Nobuyuki Yatsuyanagi Transactions of the Japan society for aeronautical and space sciences . 2006,第165期

机译：液-气同轴喷射器对液体射流破裂长度的研究：火箭发动机喷射器的雾化特性评估
3. Numerical study on the combustion characteristics of a fuel-centered pintle injector for methane rocket engines [J] . Son Min, Radhakrishnan Kanmaniraja, Yoon Youngbin, Acta astronautica . 2017,第JUNa期

机译：甲烷火箭发动机燃料中心枢轴喷油器燃烧特性的数值研究
4. Effect of engine and fuel variables on liquid fuel transport into the cylinder in port-injected SI engines [C] . Robert Meyer, John B. Heywood SAE International Congress and Exposition . 2000

机译：发动机和燃料变量对液体燃料输送到端口注射的SI发动机汽缸中的影响
5. Effects of fuel rail design and fuel injector durability on the starting performance of a liquid LPG fuelled PFI engine. [D] . Hoag, Matthew Warner. 2001

机译：燃料导轨设计和喷油器耐用性对液化石油气为燃料的PFI发动机的启动性能的影响。
6. THE SIGNIFICANT STRUCTURE THEORY APPLIED TO SOME LIQUID ROCKET FUELS [O] . T. Richard Schmidt, Mu Shik Jhon, Henry Eyring 2015

机译：重要结构理论应用于某些液体火箭燃料
7. Study on Breakup Length of Liquid Jet by Liquid-Gas Coaxial Injector —Evaluation of Atomization Characteristics of Rocket Engine Injectors— [O] . Nobuyuki YATSUYANAGI 2006

机译：液 - 气同轴注射器液体射流分解长度的研究 - 火箭发动机喷射器雾化特性 -

Injector assembly for liquid fueled rocket engines Patent

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