首页> 外国专利> FUEL SYSTEM FOR MILITARY TRAINER AIRCRAFT WITH DIHEDRAL WING TANKS WITH AUTO LEVEL BALANCING AND SUPPLY TANK PRESSURISATION

FUEL SYSTEM FOR MILITARY TRAINER AIRCRAFT WITH DIHEDRAL WING TANKS WITH AUTO LEVEL BALANCING AND SUPPLY TANK PRESSURISATION

机译:具有自动平衡和供气罐加压功能的双翼油箱的军用飞机的燃油系统

摘要

Effective fuel system is invented to have reduced number of components and piping by introducing innovative components and ideas to reduce cost and weight of the system without sacrificing any of the operational and maintenance performances and emergency redundancies in meeting requirements for military trainer aircrafts with dihedral wing tanks. Continuous fuel feed at required pressure is ensured to the engine from the fuel system at all maneuovers including inverted flying. In addition, system is featured with single point refueling, automatic wing tank imbalance correction, simplified venting.
机译:通过引入创新的组件和思想来减少系统的成本和重量,而又不牺牲任何运行和维护性能以及紧急裁员来满足带有二面翼坦克的军用教练机的需求,发明了有效的燃油系统,从而减少了组件和管道的数量。在包括反向飞行在内的所有机动过程中,都确保从燃油系统以所需压力连续向发动机供油。此外,该系统具有单点加油,自动翼舱失衡校正,简化排气的功能。

著录项

  • 公开/公告号IN2013CH01956A

    专利类型

  • 公开/公告日2016-06-03

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN1956/CHE/2013

  • 发明设计人 M JAYACHANDRAN;P RAMESH;AREKH SHARMA;

    申请日2013-05-01

  • 分类号G09B19/16;

  • 国家 IN

  • 入库时间 2022-08-21 14:25:43

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