首页> 外国专利> INTEGRATION OF DIFFERENT AIRCRAFT UNDERCARRIAGE SYSTEM USING MODULAR DESIGN CONCEPT ON THE IRON BIRD RIG FOR EVALUATION OF ADEQUACY OF HYDRAULIC SYSTEM, INTEGRATED FLIGHT CONTROL SYSTEM

INTEGRATION OF DIFFERENT AIRCRAFT UNDERCARRIAGE SYSTEM USING MODULAR DESIGN CONCEPT ON THE IRON BIRD RIG FOR EVALUATION OF ADEQUACY OF HYDRAULIC SYSTEM, INTEGRATED FLIGHT CONTROL SYSTEM

机译:基于铁鸟架的模块化设计概念的不同飞机底盘系统的集成,以评估液压系统,综合飞行控制系统的适当性

摘要

I.The Innovative idea of having Modular design concept will integrate two different Landing Gears on to the same Iron Bird rig for evaluation of adequacy of Hydraulic system, Integrated Flight Control System & Control Laws for two different variants of a Fly-By- Wire Aircraft. 2. The changeover from one landing gear to another was effortless and quick. 3. The idea and its implementation has resulted in savings amounting to the cost of building another Iron bird without compromising on the technical aspects.
机译:一,采用模块化设计理念的创新理念将两个不同的起落架集成到同一个铁鸟装备上,以评估液压系统,飞控飞机两个不同变体的集成飞行控制系统和控制律。 2.从一个起落架到另一个起落架的转换既轻松又快捷。 3.该构想及其实施导致节省的费用等于建造另一只铁禽的费用,而又不影响技术方面。

著录项

  • 公开/公告号IN2013CH01958A

    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IN1958/CHE/2013

  • 发明设计人 MAHESWARAN E;SANJAY SHARMA;

    申请日2013-05-01

  • 分类号B64C27/06;

  • 国家 IN

  • 入库时间 2022-08-21 14:25:43

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