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1. 发明申请

WO2016157077A2 A VEHICLE AND METHOD FOR DETECTING AND NEUTRALIZING AN INCENDIARY OBJECT 审中-公开
标题翻译：用于检测和中和故障对象的车辆和方法
公开(公告)号：WO2016157077A2
公开(公告)日：2016-10-06
申请号：PCT/IB2016/051766
申请日：2016-03-29
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： BABU, Natesan , RAJASEKARAN, Alexander , RAMESH, Swarna , PERUMAL THIRUNAVUKKARASU, Lakshmi Prathibha
CPC分类号： F41H11/134 , F41H11/136 , F41H11/16
摘要： A vehicle for detecting and neutralizing an incendiary object comprises a detecting device configured to mount at fore-end of the vehicle is disclosed. The detecting device comprises: one or more platforms configured to be mounted at the fore end of the vehicle. The one or more platforms are located proximal to the ground surface such that they hover over the ground surface at a predetermined distance. A plurality of sensors wherein each of the plurality of sensors mounted on the at least one of the one or more platforms for capturing information related to the incendiary object. A neutralizing device interfaced with the detecting device, wherein the neutralizing device comprises: a neutralizing arm member which actuates in one or more directions for handling and neutralizing the incendiary object based on the information related to the incendiary object. An annihilator device equipped with the neutralizing device to annihilate the incendiary object.
摘要翻译：用于检测和中和燃烧物体的车辆包括被配置为安装在车辆前端的检测装置。检测装置包括：一个或多个平台，被配置为安装在车辆的前端。一个或多个平台位于地面附近，使得它们以预定距离悬停在地面上。多个传感器，其中安装在一个或多个平台中的至少一个平台上的多个传感器中的每一个用于捕获与燃烧物体有关的信息。一种与所述检测装置接口的中和装置，其中所述中和装置包括：中和臂构件，其基于与所述燃烧物体相关的信息，在一个或多个方向上致动以处理和中和所述燃烧物体。装备有中和装置以消灭燃烧物体的歼灭机器。

2. 发明申请

WO2018073701A1 SINGLE LAYER SHARED APERTURE DUAL BAND ANTENNA 审中-公开
标题翻译：单层共享光孔双波段天线
公开(公告)号：WO2018073701A1
公开(公告)日：2018-04-26
申请号：PCT/IB2017/056308
申请日：2017-10-12
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： JAIN, Sachin , REDDY G, Siva Rami , RATNA, Pummy , VERMA, Usha P.
IPC分类号： H01Q5/00 , H01Q13/08
摘要： Embodiment of the present disclosure relates to a shared aperture antenna for continuous transmission of signal to ground station at two different spot frequencies. The antenna provides a broad side radiation pattern for frequency range of S band and squinted radiation pattern for frequency range of Ka band. The dual band microstrip antenna is configured on a single layer substrate, having a rectangular slot at small offset from the center on low frequency radiating patch. The positioning of radiating patch and length of high impedance microstrip feed are adjusted to fit into the slot and to get desired squint at high frequency. Two separate coaxial feeds are provided to excite the antenna independently. Third feed fulfil the termination needed by travelling wave array which increases the impedance bandwidth of antenna. A radome is provided to protect the radiating element from environment.
摘要翻译：本公开的实施例涉及用于在两个不同的点频率下连续地传输信号到地面站的共享孔径天线。天线为Ka波段的频率范围提供了S波段频率范围的宽侧辐射方向图和斜视辐射方向图。双频带微带天线配置在单层衬底上，在低频辐射贴片上有一个偏离中心偏离小的矩形槽。调整辐射贴片的位置和高阻抗微带馈送的长度，使其适合插槽并获得所需的高频斜视。提供两个独立的同轴馈电以独立激发天线。第三馈电完成行波阵列所需的终端，增加天线的阻抗带宽。天线罩用于保护辐射元件不受环境影响。

3. 发明申请

WO2016156935A1 MANDREL ASSEMBLY AND METHOD OF MANUFACTURING SOLID ROCKET PROPELLANT GRAIN USING THE SAME 审中-公开
标题翻译： MANDREL ASSEMBLY AND METHOD OF MANUFACTURING SOLID ROCKET PROPELLANT GRAIN WITH THE SAME
公开(公告)号：WO2016156935A1
公开(公告)日：2016-10-06
申请号：PCT/IB2015/055086
申请日：2015-07-06
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： KRISHNAN, Anish, Bala
IPC分类号： F02K9/24
CPC分类号： F02K9/24 , B65B3/022 , F02K9/10 , F02K9/343 , F05D2230/21
摘要： The present disclosure relates to a dismantleable mandrel assembly and a method of molding solid propellant grains with deep fin cavities whose major transverse dimensions are larger than casing opening dimensions in a monolithic rocket motor. The mandrel assembly comprises a base mandrel, a core mandrel insertable into the base mandrel and a plurality of fin molds attachable onto the base mandrel in a circular pattern about the motor axis. The plurality of longitudinal fin cavities is configured with forward swept leading and trailing edges. The manufacturing technique involves assembling and disassembling the mandrel components before propellant casting and after propellant curing respectively in a specific sequence. With minimum number of components and critical joints the method assures reduced quantum of explosive hazard in propellant grain manufacturing for high performance solid rocket motors.
摘要翻译：本公开涉及一种可拆卸的心轴组件以及一种具有深翅片腔的固体推进剂颗粒的方法，其主横向尺寸大于整体式火箭发动机中的壳体开口尺寸。心轴组件包括基部心轴，可插入到基座心轴中的芯心轴和以围绕电动机轴线的圆形图案可附接到基座心轴上的多个翅片模具。多个纵向翅片腔被配置有前扫掠的前缘和后缘。制造技术包括在推进剂流延之前和推进剂固化后分别以特定顺序组装和拆卸心轴组件。使用最少数量的部件和关键接头，该方法可确保在高性能固体火箭发动机的推进剂颗粒制造中减少爆炸危险的数量。

4. 发明申请

WO2011064707A3 FIBER REINFORCED POLYMERIC COMPOSITES WITH TAILORABLE ELECTRICAL RESISTIVITIES AND PROCESS FOR PREPARING THE SAME 审中-公开
公开(公告)号：WO2011064707A3
公开(公告)日：2011-06-03
申请号：PCT/IB2010/055323
申请日：2010-11-22
申请人： THE DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO) , DASGUPTA, Samudra , KUMAR, Madishetty, Narayana, Rao, Jagdish , SANKARAN, Sundaram
发明人： DASGUPTA, Samudra , KUMAR, Madishetty, Narayana, Rao, Jagdish , SANKARAN, Sundaram
IPC分类号： B29C70/88 , B29C70/02
摘要： The present invention relates to polymer composite materials, more particularly relates to composite materials with tailor made surface electrical resistivities in the range of 10 9 to 10 -1 Ω/sq. and process of making the same. The process for preparing Fibre Reinforced Polymeric (FRP) Composite, said process comprising acts of homogeneously mixing 1- 30% by weight of different electrically conducting fillers in matrix resin system to obtain resin mix; wetting dry preforms using the resin mix; compacting the wetted preforms to obtain green composite; curing the green composite; and post-curing the cured composite to prepare the FRP Composite.

5. 发明申请

WO2016075571A1 A BI-STABLE MAGNETIC ACTUATOR 审中-公开
标题翻译：双稳态磁力执行器
公开(公告)号：WO2016075571A1
公开(公告)日：2016-05-19
申请号：PCT/IB2015/058069
申请日：2015-10-20
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： GOLLAPUDI, Sreedhar Babu , MARIMANUKUPPAM, Rajamani Bhaskar , CHETLAPALLI, Satyanarayana Raju
IPC分类号： H01F7/16
CPC分类号： H01F7/1646 , H01F2007/1669
摘要： Embodiment of the present disclosure provides a bistable actuator comprising two magnets (7) interconnected through a central rod (5), which acts as a plunger connecting the at least two magnets and moves the at least two magnets as a single body. The surfaces of the two magnets facing each other have same polarity. Also, the bistable actuator comprises at least one soft magnet (6) configured around the central rod (5) between the two magnets (7). The at least one soft magnet (6) is of bobbin shape. Further, the bistable actuator comprises a copper coil (11), wound around the at least one bobbin shaped soft magnet, the copper coil magnetizes the at least one soft magnet to a polarity based on an applied electric pulse. The at least one soft magnet (6) is attracted to one of the two magnets (7) based on the applied electric pulse, which is instantaneous.
摘要翻译：本公开的实施例提供了一种双稳态致动器，其包括通过中心杆（5）互连的两个磁体（7），其作为连接至少两个磁体的柱塞，并将至少两个磁体作为单个主体移动。两个磁体彼此面对的表面具有相同的极性。此外，双稳态致动器包括围绕中心杆（5）围绕两个磁体（7）构成的至少一个软磁体（6）。所述至少一个软磁体（6）为筒状。此外，双稳态致动器包括缠绕在至少一个线圈形软磁体上的铜线圈（11），铜线圈基于所施加的电脉冲将至少一个软磁体磁化至极性。基于所施加的瞬时的电脉冲，至少一个软磁体（6）被吸引到两个磁体（7）中的一个。

6. 发明申请

WO2016128804A1 PROPELLANT GRAIN FOR A SOLID ROCKET MOTOR 审中-公开
标题翻译：用于固体摇臂电机的推土机
公开(公告)号：WO2016128804A1
公开(公告)日：2016-08-18
申请号：PCT/IB2015/055027
申请日：2015-07-03
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： KRISHNAN, Anish, Bala , MANICKAVASAGAM, Marudhanayagam , GNANASEKARAN, Venkataswamy
IPC分类号： F02K9/28
CPC分类号： F02K9/10 , F02K9/18 , F02K9/346 , F05D2220/80
摘要： The present disclosure relates to propellant grain configuration in solid rocket motors. In one embodiment, the propellant grain is a case-bonded, forward- swept, deep finocyl grain offering significant flexibility in tailoring burn surface area regression profiles to meet different performance requirements even while allowing for high propellant volumetric loading densities. The grain comprises of two or more longitudinal fin cavities with forward swept leading edges, circular-patterned about an axial cavity.
摘要翻译：本公开涉及固体火箭发动机中的推进剂颗粒构造。在一个实施方案中，推进剂颗粒是壳结合的，向前扫掠的深的finocyl颗粒，在定制燃烧表面积回归分布方面提供显着的灵活性，以满足不同的性能要求，甚至在允许高推进剂体积负荷密度的情况下。颗粒包括两个或更多个纵向翅片腔，其具有向前扫掠的前缘，围绕轴向腔呈圆形图案化。

7. 发明申请

WO2015015429A1 A BLACK BOX RECORDER WITH SATELLITE TRANSMITTER (BSAT) FOR UNDERWATER VEHICLES 审中-公开
标题翻译：带卫星发射机（BSAT）的黑匣子记录仪用于水下车辆
公开(公告)号：WO2015015429A1
公开(公告)日：2015-02-05
申请号：PCT/IB2014/063538
申请日：2014-07-30
申请人： THE DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO)
发明人： ABRAHAM, Varughese , NIRMALA, Mailapalli , PARVATHANENI SHIVA, Prasad , SANJAY, Attara , DEBASISH, Chakraborti
IPC分类号： H05K5/02 , G07C5/00 , B63G8/00 , B63G8/41
CPC分类号： G07C5/008 , B63C2009/0017 , B63G8/40 , B63G8/41 , G01S19/03 , G07C5/085 , H05K5/0213
摘要： Embodiments of the present disclosure disclose a Black box with Satellite Transmitter (BSAT) for underwater vehicles. The BSAT provides a mission data backup of sunken under water vehicles and it is akin to a black box recorder of aircrafts. The BSAT comprising a sealed enclosure to receive and transmit IR and electromagnetic signals, a Global Positioning System (GPS) with an antenna to provide GPS parameters of the BSAT, a transmit antenna to transmit the GPS parameters and parameters associated with the underwater vehicle, an ejection mechanism to eject the BSAT from the underwater vehicle on detecting a pre-defined condition, by an electronic controller. The electronic controller to perform at least one of sending control signals, communicating using IR transceiver, acquire and store underwater vehicle parameters, identifying an ejection instant, acquiring and storing data GPS parameters, scheduling data transmission through a satellite after ejection of the BSAT from the underwater vehicle.
摘要翻译：本公开的实施例公开了一种用于水下航行器的具有卫星发射机（BSAT）的黑盒。 BSAT提供了在水下车辆下沉的任务数据备份，它类似于黑匣子的飞机记录器。 BSAT包括用于接收和发送IR和电磁信号的密封外壳，具有天线的全球定位系统（GPS）以提供BSAT的GPS参数，用于发送GPS参数和与水下飞行器相关联的参数的发射天线，弹出机构，通过电子控制器检测到预先定义的状况，从水下航行器弹出BSAT。所述电子控制器执行发送控制信号，使用IR收发器进行通信，获取和存储水下车辆参数，识别弹出时刻，获取和存储数据GPS参数中的至少一个，在从所述BSAT弹出所述BSAT之后调度通过卫星的数据传输水下航行器。

8. 发明申请

WO2012104865A1 N, N- DIALKYL -MORPHOLIN- 4 - CARBOXAMIDE COMPOUNDS AS INSECT REPELLING AGENTS AND A PROCESS FOR THEIR PREPARATION 审中-公开
标题翻译： N，N-二烷基 - 吗啉-4-羧酰胺化合物作为外源代谢剂及其制备方法
公开(公告)号：WO2012104865A1
公开(公告)日：2012-08-09
申请号：PCT/IN2012/000003
申请日：2012-01-03
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION (DRDO) , AMBATI, Narasimha Rao , KUMAR, Geneshan , BRAHMA, Dutt Parashar , MULLIDHAR, Jaywantrao Mendki , SACHIN, Narayanrao Tikar , AMAR, Pal Singh , ANSHOO, Gautam , RAJAGOPALAN, Vijayyaraghavan
发明人： AMBATI, Narasimha Rao , KUMAR, Geneshan , BRAHMA, Dutt Parashar , MULLIDHAR, Jaywantrao Mendki , SACHIN, Narayanrao Tikar , AMAR, Pal Singh , ANSHOO, Gautam , RAJAGOPALAN, Vijayyaraghavan
IPC分类号： A01N43/84 , C07D265/30
CPC分类号： C07D295/215 , A01N47/38
摘要： "An insect repelling compound and a process for preparation thereof. The present invention discloses a compound of formula I and a process for preparation thereof. The compound exhibits insect repellent properties. The invention also discloses pharmaceutical composition comprising the said compound. — N R O R Formula I which R is (CH 2 )n CH 3 , or a pharmaceutically acceptable salts thereof, wherein
摘要翻译：本发明公开了一种式I化合物及其制备方法，该化合物具有驱虫性，本发明还公开了包含所述化合物的药物组合物，NROR式I 其中R是（CH 2）n CH 3，或其药学上可接受的盐，其中

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