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1. 发明授权

US09851185B2 Target 有权
公开(公告)号：US09851185B2
公开(公告)日：2017-12-26
申请号：US15335883
申请日：2016-10-27
申请人： COMINEL S.R.L.
发明人： Devis Bartolini
IPC分类号： F41J9/16 , F41J9/08 , F41J5/24
CPC分类号： F41J9/08 , F41J5/24 , F41J5/26 , F41J9/16
摘要： Target for helice target shooting comprising a helical body and a center piece that are snap-coupled together; the helical body comprising a cylindrical annular portion that extends according to a central axis (A) and is provided, peripherally, of at least one pair of mushroom-shaped projections so configured as to couple with the center piece in correspondence of respective peripheral seats; the annular portion having crack nucleation means suitable to facilitate the fracture, in use, by at least one shot.

2. 发明申请

US20170343325A1 METHOD FOR PERFORMING EXO-ATMOSPHERIC MISSILE'S INTERCEPTION TRIAL 审中-公开
公开(公告)号：US20170343325A1
公开(公告)日：2017-11-30
申请号：US15130526
申请日：2016-04-15
申请人： ISRAEL AEROSPACE INDUSTRIES LTD.
发明人： Jacob ROVINSKY , Yoav TOURGEMAN
IPC分类号： F41J2/00 , F41J2/02 , F41J9/08 , F41G7/00 , F42B8/24 , F42B8/12
CPC分类号： F41J2/00 , F41G7/003 , F41G7/004 , F41G7/006 , F41J2/02 , F41J9/08 , F42B8/12 , F42B8/24 , F42B10/60 , F42B10/62
摘要： An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet.

3. 发明授权

US09671876B2 Perspective tracking system 有权
公开(公告)号：US09671876B2
公开(公告)日：2017-06-06
申请号：US14707672
申请日：2015-05-08
申请人： Raydon Corporation
发明人： David Page
IPC分类号： F41A33/00 , F41G3/26 , F41J9/00 , F41J5/02 , G06K9/78 , G09B9/00 , G09B19/00 , G06F3/0346 , F41J9/08 , G01B11/14 , G09B9/08 , G09B9/04 , G09B9/30 , G06T7/80 , G01B21/04 , G06T7/73 , G06K9/32 , G01S5/16 , G06F17/30
CPC分类号： G06F3/0346 , F41A33/00 , F41G3/26 , F41G3/2605 , F41G3/2661 , F41J5/02 , F41J9/00 , F41J9/08 , G01B11/14 , G01B21/042 , G01S5/163 , G06F17/30825 , G06F17/30831 , G06K9/3216 , G06K9/78 , G06T7/74 , G06T7/80 , G06T2207/10016 , G06T2207/30204 , G09B9/00 , G09B9/003 , G09B9/006 , G09B9/04 , G09B9/08 , G09B9/301 , G09B9/307 , G09B19/00
摘要： Resolution of perspective in three dimensions is necessary for intermeshing real players into simulated environments during virtual training exercises. With the advent of high resolution image sensors the ability to sense position and orientation using image capture devices is possible. The combination of small sized sensors and image recognition tracking algorithms allows the tracking element to be placed directly on the device whose perspective is desired. This provides a solution to determining perspective as it provides a direct measurement from the center axis of the observer. This invention employs a perspective tracking device to determine a point-of-gaze or a point-of-aim in a three-dimensional space to a high degree of accuracy. Point-of-gaze may be used to determine views for head mounted displays and aim-points for weapons. The invention may operate in an unconstrained space allowing simulation participants to operate in a larger, open environment. Areas of interest in the environment are bounded by area of interest markers which identify the region and its physical constraints.

4. 发明申请

US20160169636A1 Simulation of Missile Signatures 审中-公开
标题翻译：导弹签名模拟
公开(公告)号：US20160169636A1
公开(公告)日：2016-06-16
申请号：US15049681
申请日：2016-02-22
申请人： Sensor Electronic Technology, Inc.
发明人： Remigijus Gaska , Alexander Dobrinsky , Maxim S. Shatalov , Michael Shur
IPC分类号： F41J2/02 , F41J9/00
CPC分类号： F41J2/02 , F41G7/002 , F41H11/02 , F41J2/00 , F41J9/00 , F41J9/08
摘要： An emitting structure for simulating an irradiance signature of a missile is provided. The emitting structure includes one or more radiation sources, each of which includes at least one ultraviolet radiation source and at least one infrared radiation source. The emitting structure also includes a spherical shell and a mechanism for positioning the radiation source(s) along a three dimensional boundary of the spherical shell. The emitting structure can locate and operate one of the radiation sources to simulate the irradiance signature of the missile.
摘要翻译：提供了用于模拟导弹的辐照度特征的发射结构。发射结构包括一个或多个辐射源，每个辐射源包括至少一个紫外辐射源和至少一个红外辐射源。发射结构还包括球壳和用于沿着球壳的三维边界定位辐射源的机构。发射结构可以定位和操作其中一个辐射源，以模拟导弹的辐照度特征。

5. 发明授权

US07007290B2 Flexible airfoil ring for safely flying CDs and DVDs 失效
标题翻译：灵活的翼型环，用于安全地放置CD和DVD
公开(公告)号：US07007290B2
公开(公告)日：2006-02-28
申请号：US10700841
申请日：2003-11-03
申请人： Cynthia H. Wilcoxson , Don G. Harland
发明人： Cynthia H. Wilcoxson , Don G. Harland
IPC分类号： G11B23/03
CPC分类号： F41J9/08 , A63H33/18 , F41J1/01 , G11B7/24097 , G11B33/0422
摘要： An annular protective ring attachment designed to grip the outer peripheral edge of all compact discs (CDs) and digital video discs (DVDs) which, when used in combination with said CD or DVD, creates an airfoil. The airfoil ring consists of an inner periphery, which is molded to form a top lip (3) and bottom lip (4), and between these lips, a gripping mouth (6), which securely holds the CD or DVD (7,76) inside the aperture of the airfoil ring. The body of the airfoil ring is curved in such a way as to create an airfoil adequate to enable the airfoil ring with inserted CD or DVD to be safely tossed into the air and to exhibit controllability in flight. The airfoil ring is constructed of a soft, flexible plastic material, and uses a hinge groove (5) on the top side of the airfoil skirt (1) and a hinge groove reaction area (9) on the underside of the airfoil skirt (1) to dissipate the contact force upon impact and create a cushioning effect so as to avoid resultant injury or damage when tossed into the air. A locking groove (8) inside the gripping mouth area (6) traps the sharp edge of the CD or DVD (7), preventing it from dislodging upon impact and causing injury.
摘要翻译：设计用于夹持所有光盘（CD）和数字视频光盘（DVD）的外围边缘的环形保护环附件，当与所述CD或DVD结合使用时，产生一个翼型件。翼型环由内周构成，其内模被形成以形成上唇（3）和底唇（4），并且在这些唇之间，夹紧口（6）牢固地保持CD或DVD（7,76 ）在翼型环的孔内。机翼环的主体以这样的方式弯曲，以便产生足以使具有插入的CD或DVD的翼型环能够安全地扔进空气中并且在飞行中展现可控性的翼型件。翼型环由柔软的柔性塑料材料构成，并且使用翼型裙部（1）的顶侧上的铰链槽（5）和翼型裙部（1）的下侧上的铰链槽反作用区域（9））在冲击时消除接触力，并产生缓冲作用，以避免在扔入空气时造成伤害或损坏。夹持口区域（6）内的锁定槽（8）捕获CD或DVD（7）的锋利边缘，防止其在撞击时被移除并造成伤害。

6. 发明授权

US06888152B2 IR source, method and apparatus 有权
标题翻译：红外光源，方法和装置
公开(公告)号：US06888152B2
公开(公告)日：2005-05-03
申请号：US10331792
申请日：2002-12-30
申请人： Theodore R. Strickland
发明人： Theodore R. Strickland
IPC分类号： F41J2/02 , F41J9/08 , G21G60/299
CPC分类号： F41J9/08 , F41J2/02
摘要： The invention is an apparatus for producing an IR (infra-red) signature. In the method, the apparatus is mounted on a target to give the target an infra-red signature whereby the target can be acquired by an appropriate weapon sensor.
摘要翻译：本发明是用于产生IR（红外）签名的装置。在该方法中，该装置安装在目标上以向目标提供红外签名，由此目标可由适当的武器传感器获取。

7. 发明申请

US20040075028A1 Kit of parts and a method for converting between a glider and a kite 审中-公开
标题翻译：零件套件和滑翔机和风筝之间转换的方法
公开(公告)号：US20040075028A1
公开(公告)日：2004-04-22
申请号：US10462777
申请日：2003-06-17
发明人： Jung-Yuan Wang
IPC分类号： F41J009/08 , A63H027/08 , B64C031/06
CPC分类号： A63H27/02 , A63H27/08 , F41J9/08 , F42B10/00
摘要： A kit of parts and a method for converting between a glider and a kite. The kit of parts includes a body, a kite wing and a glider wing. The kite wing is removably connectable to the body so that the body and the kite wing can be connected to a kite string and flown as a kite. The glider wing is removably connectable to the body so that the body and the glider wing can be flown as a glider.
摘要翻译：一套零件和一种在滑翔机和风筝之间转换的方法。零件套件包括一个身体，一个风筝翼和一个滑翔机翼。风筝翼可拆卸地连接到身体，使得身体和风筝翼可以连接到风筝绳上，并作为风筝飞行。滑翔机翼可拆卸地连接到身体，使身体和滑翔机翼可以作为滑翔机飞行。

8. 发明申请

US20030141463A1 IR source, method and apparatus 有权
公开(公告)号：US20030141463A1
公开(公告)日：2003-07-31
申请号：US10331792
申请日：2002-12-30
申请人： Precision Combustion, Inc.
发明人： Theodore R. Strickland
IPC分类号： G21G004/00
CPC分类号： F41J9/08 , F41J2/02
摘要： The invention is an apparatus for producing an IR (infra-red) signature. In the method, the apparatus is mounted on a target to give the target an infra-red signature whereby the target can be acquired by an appropriate weapon sensor.

9. 发明授权

US06600165B1 Self-propelled infrared emission aerial target 失效
标题翻译：自走红外发射空中目标
公开(公告)号：US06600165B1
公开(公告)日：2003-07-29
申请号：US09330133
申请日：1999-06-11
申请人： Pascal Doe , Herve Guidetti , Gilles Thavot , Eric Rantet
发明人： Pascal Doe , Herve Guidetti , Gilles Thavot , Eric Rantet
IPC分类号： G01J100
CPC分类号： F41J9/08
摘要： A self-propelled infrared emission aerial target has an aircraft- or a missile-shaped body and a nose, wings and/or control surfaces, a system for feeding fuel and oxidizer to a combustion chamber in which combustion gases are produced and for supplying the combustion gases to a propulsion nozzle, and an infrared radiation emitter. The target has at least one conduit connecting the combustion chamber or propulsion nozzle of the propulsion system to a nose, wing and/or control surface of the target, or to an outside element attached thereto.
摘要翻译：自推进红外发射空中目标具有飞机或导弹形体以及鼻翼，翼和/或控制表面，用于将燃料和氧化剂供给到其中产生燃烧气体的燃烧室的系统，燃烧气体到推进喷嘴和红外辐射发射器。目标具有将推进系统的燃烧室或推进喷嘴连接到靶的鼻，翼和/或控制表面或连接到其上的外部元件的至少一个导管。

10. 发明授权

US3774871A External slurry injection for infrared enhancement of exhaust plume 失效
公开(公告)号：US3774871A
公开(公告)日：1973-11-27
申请号：US3774871D
申请日：1970-04-30
申请人： US AIR FORCE
发明人： SEMMES I , SIMPSON C
IPC分类号： F41J2/02 , F41J9/08 , B64D1/18
CPC分类号： F41J9/08 , F41J2/02
摘要： A means for enhancing the infrared content of the exhaust plume of a rocket-powered target vehicle by controllably atomizing and injecting an enriching slurry into the main exhaust flow thereby producing an output which realistically simulates the radiant intensity pattern produced by an afterburning aircraft.

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