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1. 发明授权

EP4058350B1 A WEAPON SYSTEM 有权
公开(公告)号：EP4058350B1
公开(公告)日：2024-06-05
申请号：EP20804638.3
申请日：2020-11-05
IPC分类号： B64C13/16 , B64D7/00 , F41H13/00 , G05D1/00 , F41H7/00
CPC分类号： F41H13/0043 , F41H13/005 , B64D7/00 , B64C13/16 , G05D1/0094 , F41H7/00

2. 发明授权

EP2898286B1 ARMOR SYSTEM 有权
标题翻译： ARMOR系统
公开(公告)号：EP2898286B1
公开(公告)日：2018-01-10
申请号：EP13785929.4
申请日：2013-09-23
申请人： Edan Administration Services (Ireland) Limited
发明人： COHEN, Hananya , COHEN, Edwin
IPC分类号： F41H5/04
CPC分类号： F41H5/0428 , B63B3/10 , B64D7/00 , F41H1/02 , F41H5/0421 , F41H5/0492 , F41H5/24 , F41H7/02
摘要： An armor system pellet is provided. The pellet includes a pellet body attached to four projections for interlocking adjacent pellets when arranged in an array. The pellet is configured such that the width of a first pair of co-linear projections is less than a width of a second pair of co-linear projections.

3. 发明公开

EP3120104A4 ARMORED WINDOW 审中-公开
公开(公告)号：EP3120104A4
公开(公告)日：2017-11-15
申请号：EP14886313
申请日：2014-03-18
申请人： SIKORSKY AIRCRAFT CORP
发明人： HALLQUIST CRAIG
IPC分类号： F41H5/26 , B64C1/14 , F41H5/04
CPC分类号： B64C1/1484 , B64C1/1492 , B64D7/00 , F41H5/0407 , F41H5/263

4. 发明授权

EP2382125B1 AN ARRANGEMENT AT AN AIRCRAFT OF A DISPENSER UNIT FOR COUNTERMEASURES 有权
标题翻译：对付分配器单元的飞机上的安排对策
公开(公告)号：EP2382125B1
公开(公告)日：2017-07-19
申请号：EP09838487.8
申请日：2009-01-16
申请人： Saab AB
发明人： MELIN, Robert
IPC分类号： B64D1/02 , F41H11/02 , B64D7/00 , F42B5/15 , F41A23/20
CPC分类号： B64D1/02 , B64D7/00 , F41A23/20 , F42B5/15

5. 发明公开

EP3120104A1 ARMORED WINDOW 审中-公开
标题翻译： GEPANZERTES FENSTER
公开(公告)号：EP3120104A1
公开(公告)日：2017-01-25
申请号：EP14886313.7
申请日：2014-03-18
申请人： Sikorsky Aircraft Corporation
发明人： HALLQUIST, Craig
IPC分类号： F41H5/26 , B64C1/14
CPC分类号： B64C1/1484 , B64C1/1492 , B64D7/00 , F41H5/0407 , F41H5/263
摘要： A rotary wing aircraft is provided including an airframe having a nose section located at a forward end. A window assembly is coupled to the nose section. The window assembly includes a frame and a transparent armored window. The frame has a large opening and a lip extends from a portion of the frame adjacent the large opening. The transparent armored window is formed from a plurality of layers and has a shape generally complementary to the large opening. When the transparent armored window is received within the large opening of the frame, a portion of the transparent armored window is attached to a portion of the lip.
摘要翻译：提供了一种旋翼机，其包括具有位于前端的鼻部的机身。窗组件联接到鼻部。窗组件包括框架和透明装甲窗。框架具有大的开口，并且唇缘从邻近大开口的框架的一部分延伸。透明铠装窗由多层形成，具有与大开口大致互补的形状。当透明铠装窗口被容纳在框架的大开口内时，透明铠装窗口的一部分附接到唇部的一部分。

6. 发明公开

EP3102486A1 RECONFIGURABLE PAYLOAD SYSTEMS (RPS) FOR AIRCRAFT 审中-公开
标题翻译：可重构有效载荷系统 - 飞机
公开(公告)号：EP3102486A1
公开(公告)日：2016-12-14
申请号：EP15740812.1
申请日：2015-01-23
申请人： L-3 Communications Integrated Systems L.P.
发明人： HODGE, Ben D. , TROUP, Timothy W. , CROPPER, Richard D. , STOKES, Brandy D.
IPC分类号： B64C7/00 , B64D1/08 , B64D1/12
CPC分类号： B64D9/00 , B64C39/02 , B64C2201/128 , B64C2211/00 , B64D7/00
摘要： Reconfigurable payload systems (RPS) and methods of configuring and using the same with operational load envelopes are disclosed that may be employed to enable external aircraft payloads to be rapidly interchanged or swapped out together with associated internal equipment within a given aircraft so as to modify or change payload capability of the aircraft, e.g., to meet a particular mission and/or to enable use of future payload types as they are developed. The RPS and associated methods may be implemented to allow multiple different payload systems to be swapped in and out on a given aircraft as required based on needs for a given mission.

7. 发明公开

EP3085054A1 AUSSENLAST FÜR EIN LUFTFAHRZEUG MIT UNIVERSELLER ANSTEUERSCHNITTSTELLE 有权
标题翻译：外部持续符合通用驱动器接口飞机
公开(公告)号：EP3085054A1
公开(公告)日：2016-10-26
申请号：EP14837098.4
申请日：2014-12-06
申请人： Airbus Defence and Space GmbH
发明人： KUTKA, Joachim
IPC分类号： H04L29/06
CPC分类号： H04L69/08 , B64D7/00 , B64D9/00 , H04L67/12
摘要： The invention relates to an external load (100) for an aircraft (200) comprising a first control unit (120), which is designed to be coupled to the aircraft and to exchange control data with the aircraft by means of a first specified input signal protocol (119), and a first payload space (160A) for accommodating a first payload (150A). The first payload is realized as a first function module for performing a function, and the performance of the function is initiated by the aircraft by transferring control data to the first control unit (120). The first control unit is designed to output control data according to a first specified output signal protocol (121). The external load (100) has a second control unit (130), which is arranged in such a way that the control data according to the first specified output signal protocol (121) serve as input signals for the second control unit (130). The second control unit (130) is designed to convert the input signals (121) received by the second control unit into a second output signal protocol (133) in accordance with a first conversion protocol and to adapt said input signals to a control protocol of the first function module.

8. 发明授权

EP2094920B1 A BARRIER 有权
标题翻译：屏障
公开(公告)号：EP2094920B1
公开(公告)日：2016-09-28
申请号：EP07848562.0
申请日：2007-12-17
申请人： THE SECRETARY OF STATE FOR DEFENCE
发明人： BARNES, Ian , THOMAS, Bryn
IPC分类号： B64D7/00 , F42B39/24 , F42D5/045 , E04H9/04
CPC分类号： B64D7/00 , E04H9/04 , F42B39/24 , F42D5/045

9. 发明公开

EP2421754A4 CLOSABLE COUNTER-MEASURE COMPARTMENTS FOR A DISPENSER UNIT 有权
标题翻译：关闭措施，防止呼吁，要求KILL UNIT
公开(公告)号：EP2421754A4
公开(公告)日：2015-06-03
申请号：EP09843741
申请日：2009-04-23
申请人： SAAB AB
发明人： ZÄTTERQVIST CHRISTER
IPC分类号： B64D1/02 , B64D7/00 , F41F3/065 , F41H11/02 , F41J2/02 , F42B12/70
CPC分类号： B64D7/00 , F41F3/065 , F41J2/02 , F42B12/70

10. 发明公开

EP2297592A4 SENSOR FOR AIRBORNE SHOOTER LOCALIZATION SYSTEM 有权
标题翻译：传感器FÜREIN系统ZUR LOKALISIERUNG VONSCHÜTZENIN DER LUFT
公开(公告)号：EP2297592A4
公开(公告)日：2015-06-03
申请号：EP09746937
申请日：2009-05-12
申请人： RAYTHEON BBN TECHNOLOGIES CORP
发明人： BARGER JAMES E , STANLEY JOHN
IPC分类号： G01S3/808 , B64C27/04 , B64D7/00 , F41H11/00 , F41H13/00 , G01H11/00 , G01H11/06 , G01S3/86 , G10K11/00
CPC分类号： B64D7/00 , B64C27/04 , F41H11/00 , F41H13/00 , G01H11/06 , G01S3/808 , G01S3/86 , G10K11/002 , G10K11/004 , H04R2410/00
摘要： A sensor assembly suitable for use in an airborne shooter localization system. The sensor assembly has a pressure sensor subassembly with a pressure transducer positioned to detect pressure variations associated with a shock wave from a passing projectile or the muzzle blast following the shock wave. To substantially increase the signal to noise ratio for measurements of the shock wave, the pressure sensor subassembly attenuates pressure fluctuations triggered by turbulent airflow over the surface of the subassembly more than it attenuates the shock wave. This preferential attenuation is provided by separating the pressure transducer from the surface of the sensor assembly by a cavity large enough that the pressure fluctuations are substantially attenuated as they propagate across the cavity. Additionally, features of a housing that holds the pressure sensor subassembly facilitate use on an aircraft. Those features include flexibility that allows the sensor assembly to conform to curved surfaces, a skin that provides resistance to environmental conditions and allows the sensor assembly to be attached with an adhesive, and a body region that provides high vibrational impedance to prevent low frequency mechanical vibrations from being coupled to the pressure transducer.
摘要翻译：适用于机载射手定位系统的传感器组件。传感器组件具有压力传感器子组件，压力传感器定位成用于检测与冲击波之后的经过的射弹或枪口爆炸的冲击波相关联的压力变化。为了大大增加用于冲击波测量的信噪比，压力传感器子组件衰减了比组件表面上的湍流气流触发的压力波动更多的是衰减冲击波。通过将压力传感器与传感器组件的表面分开一个足够大的空腔，使压力波动在其穿过空腔传播时基本上衰减而提供这种优先衰减。此外，保持压力传感器子组件的壳体的特征便于在飞机上使用。这些特征包括灵活性，其允许传感器组件符合弯曲表面，提供对环境条件的抵抗力并允许传感器组件用粘合剂附着的皮肤，以及提供高振动阻抗以防止低频机械振动的身体区域从耦合到压力传感器。

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