The invention discloses a turboprop engine power device for a single-engine double-wing aircraft. The turboprop engine power device comprises an engine fairing, a turboprop engine is fixedly connectedto the inner wall of a front port of the engine fairing, and an engine firewall is fixedly connected to the inner wall of the front port of the engine fairing. An engine installation frame is installed at the end, located in the engine fairing, of the turboprop engine, a five-blade propeller is installed at the end, located outside the engine fairing, of the turboprop engine, the exterior of theengine installation frame penetrates through an engine firewall, and an installation base is installed at the tail of the engine installation frame. The invention relates to the technical field of aviation. The invention solves the problems that the piston engine adopted by Y5/Y5B series aircrafts is high in oil consumption, the supply guarantee of aviation gasoline is also the problem of aviationoperation of various airlines, and the aviation gasoline is increasingly scarce and difficult to purchase due to many factors such as high production difficulty, high manufacturing cost, serious atmospheric pollution and the like, and great inconvenience is brought to a piston type aviation gasoline engine user.
本发明公开了一种用于单发双翼飞机的涡桨发动机动力装置,包括有发动机整流罩,发动机整流罩前部端口处的内壁固定连接有涡桨发动机,以及内壁固定连接有发动机防火墙,涡桨发动机位于发动机整流罩内部的一端安装有发动机安装架,以及位于发动机整流罩外部的一端安装有五叶螺旋桨,发动机安装架的外部穿过发动机防火墙,且尾部安装有安装基座,本发明涉及航空技术领域。本发明,解决了Y5/Y5B系列飞机采用的活塞发动机,不仅油耗高,而且航空汽油的供应保障也是各航空公司航空作业的难题,又因航空汽油本身生产难度大、制造成本高、对大气污染严重等诸多因素,导致航空汽油日益紧缺,燃油采购困难,给活塞类航空汽油发动机用户造成极大的不便的问题。
Turboprop engine power device for single-engine double-wing aircraft
一种用于单发双翼飞机的涡桨发动机动力装置
2021-02-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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