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1. 发明专利

JP2011237075A Flying object 有权
标题翻译：飞行对象
公开(公告)号：JP2011237075A
公开(公告)日：2011-11-24
申请号：JP2010107370
申请日：2010-05-07
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SUZUKI YASUHITO , FURUYA SHOJIRO , KITANO TAKAHISA
IPC分类号： F42B10/30 , F42B15/00
摘要： PROBLEM TO BE SOLVED: To obtain a flying object which does not increase the whole length and mass and has a simple configuration for obtaining propelling force even when equipped with a sub-propelling means for generating propelling force by jetting combustion gas to the side face direction of a body.SOLUTION: A hollow body 24 contains solid propellant 22 in areas 20A, 20B. The solid propellant 22 is burned by so-called multi-pulse which ignites the solid propellant 22 in the areas 20A, 20B sequentially. A nozzle 26 arranged at the back of the body 24 generates propelling force by jetting combustion gas generated by combustion of the solid propellant 22 to the rear of the body 24. A side thrustor 32 attached to the side face of the body 24 generates propelling force by jetting the combustion gas generated by combustion of the solid propellant 22 in the area 20A ahead of the body 24 to the side face direction of the body 24.
摘要翻译：要解决的问题：为了获得不增加整个长度和质量的飞行物体，并且具有用于获得推进力的简单构造，即使当配备有通过向燃烧气体喷射燃烧气体而产生推进力的副推进装置身体的侧面方向。解决方案：中空体24在区域20A，20B中包含固体推进剂22。固体推进剂22被所谓的多脉冲燃烧，顺序地点燃区域20A，20B中的固体推进剂22。布置在主体24的后部的喷嘴26通过将固体推进剂22的燃烧产生的燃烧气体喷射到主体24的后部而产生推进力。附接到主体24的侧面的侧推进器32产生推进力通过将主体24前方的区域20A中的固体推进剂22的燃烧产生的燃烧气体喷射到主体24的侧面方向。（C）2012年，JPO＆INPIT

2. 发明专利

JP2011237074A Flying body launch system 有权
标题翻译：飞行身体启动系统
公开(公告)号：JP2011237074A
公开(公告)日：2011-11-24
申请号：JP2010107368
申请日：2010-05-07
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KITANO TAKAHISA , FURUYA SHOJIRO , SUZUKI YASUHITO
IPC分类号： F41H11/02 , F41F3/042
摘要： PROBLEM TO BE SOLVED: To provide a flying body launch system allowing improvement of reliability related to control of a plurality of launch units, and allowing efficient operation of launchers and detection devices included in the plurality of launch units.SOLUTION: In this flying object launch system 10, a set including one or more launchers 12 each of which can be loaded with a flying object and launches the flying object, one or more radar devices 14 detecting a target, and a control device 16 controlling the launchers 12 and the radar devices 14 is set as the launch unit 18. The flying object launch system 10 includes the plurality of launch units 18. Each launch unit 18 can communicate with other launch units 18 via a communication network 20. By a main control device selected from the control devices 16 included in the plurality of launch units 18, the launchers 12 and the radar devices 14 included in the other launch units 18 are controlled via the communication network 20, together with the launchers 12 and the radar devices 14 included in the launch unit 18 including the main control device.
摘要翻译：要解决的问题：提供一种能够提高与多个发射单元的控制相关的可靠性的飞行体发射系统，并且允许包括在多个发射单元中的发射器和检测装置的有效操作。解决方案：在该飞行物体发射系统10中，一组包括一个或多个发射器12，每个发射器12可以装载飞行物体并发射飞行物体，一个或多个雷达装置14检测目标，以及一个控制控制发射器12和雷达装置14的装置16被设置为发射单元18.飞行物体发射系统10包括多个发射单元18.每个发射单元18可以经由通信网络20与其他发射单元18通信。通过从包括在多个发射单元18中的控制装置16中选择的主控制装置，通过通信网络20与发射装置12和发射装置12一起控制包括在其它发射装置18中的发射装置12和雷达装置14。包括在包括主控制装置的发射单元18中的雷达装置14。版权所有（C）2012，JPO＆INPIT

3. 发明专利

JP2012202222A Tvc device 有权
标题翻译： TVC设备
公开(公告)号：JP2012202222A
公开(公告)日：2012-10-22
申请号：JP2011064649
申请日：2011-03-23
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SUZUKI YASUHITO , FURUYA SHOJIRO , SERA YOSHIHIRO
IPC分类号： F02K9/90 , F02K1/78 , F42B10/66
摘要： PROBLEM TO BE SOLVED: To provide a TVC device, in which the number of actuators that drive a jet tab can be reduced and the change of a deflection direction of a combustion gas jet flow is suppressed in accordance with a protruding amount of the jet tab into the combustion gas jet flow.SOLUTION: The TVC device includes a jet tab 40 disposed on a rear side of a nozzle 4 in which a combustion gas jet flow blows out, and a drive part. The jet tab 40 includes deflecting parts 41 and 42 disposed to interpose the center axis S4 of the nozzle 4, and coupling parts 45 and 46 coupling the deflecting parts 41 and 42 to each other. The drive part linearly moves the jet tab 40 in such a manner that the deflecting part 41 approaches the center axis S4 and the deflecting part 42 recedes from the center axis S4, and linearly moves the jet tab 40 in such a manner that the deflecting part 42 approaches the center axis S4 and the deflecting part 41 recedes from the center axis S4.
摘要翻译：要解决的问题：提供一种TVC装置，其中可以减少驱动喷射翼片的致动器的数量，并且根据突发量来抑制燃烧气体喷射流的偏转方向的变化喷射片进入燃烧气体射流。解决方案：TVC装置包括设置在燃烧气体喷射流吹出的喷嘴4的后侧的喷射突出部40和驱动部。喷射翼片40包括设置成插入喷嘴4的中心轴线S4的偏转部分41和42以及将偏转部分41和42彼此联接的联接部分45和46。驱动部分使得偏转部分41接近中心轴线S4并且偏转部分42从中心轴线S4退出的方式直线地移动喷射突片40，并且以这样的方式直线地移动喷射突片40，使得偏转部分 42接近中心轴线S4，偏转部分41从中心轴线S4退出。版权所有（C）2013，JPO＆INPIT

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