T T-SHAPED APPARATUS INJECTING FUEL AND ENGINE MODULE COMPRISING THE SAME

A T-type fuel injection device according to an embodiment comprises: a main body disposed inside an engine, and having lower and upper parts formed in a T shape; an internal flow path through which fuel is supplied inside the main body; and an injection hole communicating with the internal flow path...

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Bibliographische Detailangaben
Hauptverfasser:	LIM CHANG WON, JIN SANG WOOK
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A T-type fuel injection device according to an embodiment comprises: a main body disposed inside an engine, and having lower and upper parts formed in a T shape; an internal flow path through which fuel is supplied inside the main body; and an injection hole communicating with the internal flow path and formed through the main body, wherein the injection holes may be formed in plural numbers and disposed at the upper and lower parts of the main body. According to one embodiment, the T-type fuel injection device that can increase the penetration distance of fuel while minimizing flow resistance can be provided. 일 실시 예에 따른 T형 연료 분사 장치는 엔진 내부에 배치되고, 하부 및 상부가 T 형상으로 형성되는 본체; 상기 본체의 내부에서 연료가 공급되는 경로가 되는 내부 유로; 및 상기 내부 유로에 연통하고, 상기 본체를 관통하여 형성되는 분사공을 포함하고, 상기 분사공은, 복수 개로 형성되고, 상기 본체의 상부 및 하부에 배치될 수 있다.