Pintle injector
AssigneeJapan Aerospace Exploration Agency
InventorsKeiichi Hasegawa, Shinichi Moriya
Life of this patent
Estimating the term…
Loading patent…
AssigneeJapan Aerospace Exploration Agency
InventorsKeiichi Hasegawa, Shinichi Moriya
Estimating the term…
To provide a simple structured and low cost pintle injector capable of uniformly atomizing and mixing fuel and oxidizer, and further improving the combustion efficiency of the combustion reaction in the combustion chamber. A pintle injector part having a first propellant channel forms a first injector flow path as a regenerative cooling path along the pintle external wall that projects into a combustion chamber, and high temperature fuel gas is injected from the first pintle injector port. On the other hand, an axial injector part is located upstream of the first pintle injector port, and injects comparatively low temperature liquid or gas fuel from an axial injector port via a third propellant channel and a third injector flow path. Oxidizer is injected from a second pintle injector port via a second propellant channel and a second injector flow path, and is atomized and mixed while being impinged on either by the high temperature fuel gas and the comparatively low temperature liquid or gas fuel. The fuel injected from the first pintle injector port and the fuel injected from the axial injector port may be the same type or a different type of fuel.
A pintle injector, having a pintle injector part which has a propellant channel that transmits fuel or oxidizer propellant and which projects into a combustion chamber for injecting the propellants, wherein
Dependencies are inferred from the claim text.