LIQUID ROCKET ENGINE INJECTOR HEAD
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 combu...
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Main Authors | , |
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Format | Patent |
Language | English Korean |
Published |
25.03.2010
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Subjects | |
Online Access | Get full text |
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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. |
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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 |
Author_xml | – fullname: CHOI, HWAN SEOK – fullname: SEO, SEONG HYEON |
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Notes | Application Number: KR20080090779 |
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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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