公开(公告)号：WO2010143179A1

公开(公告)日：2010-12-16

申请号：PCT/IL2010/000435

申请日：2010-06-02

Applicant: ELTA SYSTEMS LTD. ,  PRATZOVNICK, Arie ,  RON, Shmuel

Inventor： PRATZOVNICK, Arie ,  RON, Shmuel

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/127

Abstract: A sensor/emitter arrangement (M1-M3) is integrated into the fuselage (120) structure of a specially designed air vehicle (100), in which the air vehicle is configured for optimizing operation of the sensor/emitter arrangement (M1-M3) with respect to at least azimuthal lines of sight radiating along a azimuthal reference plane of the air vehicle (100). The azimuthal reference plane intersects the air vehicle fuselage (120). In at least some embodiments, the fuselage (120) is formed with a plurality of oblate cross-sections that facilitate maximizing the room available for a sensor/emitter array (172, 174, 176) that is elongated along an elongate axis that may be aligned with the azimuthal reference plane. In at least some embodiments one or more such elongate axes may be inclines to the longitudinal (roll) axis and the pitch axis of the air vehicle (100). In at least some embodiments, the air vehicle may have a blunt aft end incorporating an elongate aft-facing sensor/emitter array (172, 174, 176).

Abstract translation: 传感器/发射器装置（M1-M3）集成在专门设计的空中飞行器（100）的机身（120）结构中，其中，空中飞行器配置成优化传感器/发射器装置（M1-M3）的操作， 相对于沿着所述空中交通工具（100）的方位角参考平面辐射的至少方位视线。 方位角参考平面与机动车辆机身（120）相交。 在至少一些实施例中，机身（120）形成有多个扁平横截面，其有助于最大化可用于沿着细长轴线延伸的传感器/发射器阵列（172,174,176）的房间，该细长轴线可以是 与方位角参考平面对齐。 在至少一些实施例中，一个或多个这样的细长轴线可以倾斜到空中车辆（100）的纵向（滚动）轴线和俯仰轴线。 在至少一些实施例中，空中交通工具可以具有并入一个延伸的面向后面的传感器/发射器阵列（172,174,176）的平头后端。

公开(公告)号：EP2440456A1

公开(公告)日：2012-04-18

申请号：EP10728388.9

申请日：2010-06-02

Applicant: Elta Systems Ltd.

Inventor： PRATZOVNICK, Arie ,  RON, Shmuel

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/127

Abstract: A sensor/emitter arrangement (M1-M3) is integrated into the fuselage (120) structure of a specially designed air vehicle (100), in which the air vehicle is configured for optimizing operation of the sensor/emitter arrangement (M1-M3) with respect to at least azimuthal lines of sight radiating along a azimuthal reference plane of the air vehicle (100). The azimuthal reference plane intersects the air vehicle fuselage (120). In at least some embodiments, the fuselage (120) is formed with a plurality of oblate cross-sections that facilitate maximizing the room available for a sensor/emitter array (172, 174, 176) that is elongated along an elongate axis that may be aligned with the azimuthal reference plane. In at least some embodiments one or more such elongate axes may be inclines to the longitudinal (roll) axis and the pitch axis of the air vehicle (100). In at least some embodiments, the air vehicle may have a blunt aft end incorporating an elongate aft-facing sensor/emitter array (172, 174, 176).

Abstract translation: 传感器/发射器装置（M1-M3）被集成到专门设计的飞行器（100）的机身（120）结构中，其中飞行器被配置用于优化传感器/发射器装置（M1-M3） 至少相对于沿航空器（100）的方位参考平面辐射的方位角视线。 方位参考平面与飞行器机身（120）相交。 在至少一些实施例中，机身（120）形成有多个扁平横截面，这有助于最大化可用于传感器/发射器阵列（172,174,176）的空间，该传感器/发射器阵列沿着细长轴线伸长，该细长轴线可以是 与方位参考平面对齐。 在至少一些实施例中，一个或多个这种细长轴线可以倾斜至飞行器（100）的纵向（滚动）轴线和俯仰轴线。 在至少一些实施例中，飞行器可以具有包含细长的面向后方的传感器/发射器阵列（172,174,176）的钝后端。