Abstract PURPOSE: An injector head of a liquid propellant rocket combustor is provided to prevent oxidizer and fuel from being leaked and mixed inside the injector head by separately including an oxidizer injector and a fuel injection nozzle. CONSTITUTION: An injector head of a liquid propellant rocket combustor comprises an injection plate(110), a partition plate(120), a fuel injection nozzle(130), and an oxidizer injector(140). The injection plate constitutes the upper side of the combustion chamber and has through-holes(111). The partition plate is apart from the upper part of the injection plate to form a space between the partition plate and the injection plate. The fuel injection nozzle injects fuel supplied from a fuel supply manifold to the combustion chamber. The upper side of the fuel injection nozzle is coupled with the lower side of the partition plate and the lower side of the fuel injection nozzle is inserted into the through-hole. The oxidizer injector injects oxidizer supplied from an oxidizer supply manifold.
AbstractList PURPOSE: An injector head of a liquid propellant rocket combustor is provided to prevent oxidizer and fuel from being leaked and mixed inside the injector head by separately including an oxidizer injector and a fuel injection nozzle. CONSTITUTION: An injector head of a liquid propellant rocket combustor comprises an injection plate(110), a partition plate(120), a fuel injection nozzle(130), and an oxidizer injector(140). The injection plate constitutes the upper side of the combustion chamber and has through-holes(111). The partition plate is apart from the upper part of the injection plate to form a space between the partition plate and the injection plate. The fuel injection nozzle injects fuel supplied from a fuel supply manifold to the combustion chamber. The upper side of the fuel injection nozzle is coupled with the lower side of the partition plate and the lower side of the fuel injection nozzle is inserted into the through-hole. The oxidizer injector injects oxidizer supplied from an oxidizer supply manifold.
Author CHOI, HWAN SEOK
SEO, SEONG HYEON
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Snippet PURPOSE: An injector head of a liquid propellant rocket combustor is provided to prevent oxidizer and fuel from being leaked and mixed inside the injector head...
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SubjectTerms AIR SUPPLY
BLASTING
COMBUSTION APPARATUS
COMBUSTION ENGINES
COMBUSTION PROCESSES
DRAUGHT-INDUCING
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION
SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
WEAPONS
Title LIQUID ROCKET ENGINE INJECTOR HEAD
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