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1. 发明公开

EP1902323A4 TUNING FORK GYROSCOPES, ACCELEROMETERS, AND OTHER SENSORS WITH IMPROVED SCALE FACTOR 审中-公开
标题翻译： STIMMGABEL GYRO，具有完善的比例因子加速计和其他传感器
公开(公告)号：EP1902323A4
公开(公告)日：2011-11-02
申请号：EP06784891
申请日：2006-06-14
申请人： DRAPER LAB CHARLES S
发明人： WEINBERG MARC S , BERNSTEIN JONATHAN , BORENSTEIN JEFFREY T , ELLIOTT RICHARD , KIRKOS GREGORY , KOUREPENIS ANTHONY S
IPC分类号： G01P9/04 , G01P15/125
CPC分类号： G01C19/5733 , G01P15/125

2. 发明申请

WO2006138392A2 TUNING FORK GYROSCOPES, ACCELEROMETERS, AND OTHER SENSORS WITH IMPROVED SCALE FACTOR 审中-公开
标题翻译：调谐陀螺仪，加速度计和其他传感器具有改进的尺度因子
公开(公告)号：WO2006138392A2
公开(公告)日：2006-12-28
申请号：PCT/US2006023189
申请日：2006-06-14
申请人： DRAPER LAB CHARLES S , WEINBERG MARC S , BERNSTEIN JONATHAN , BORENSTEIN JEFFREY T , ELLIOTT RICHARD , KIRKOS GREGORY , KOUREPENIS ANTHONY S
发明人： WEINBERG MARC S , BERNSTEIN JONATHAN , BORENSTEIN JEFFREY T , ELLIOTT RICHARD , KIRKOS GREGORY , KOUREPENIS ANTHONY S
IPC分类号： G01P15/08
CPC分类号： G01C19/5733 , G01P15/125
摘要： A tuning fork gyroscope design where at least one proof mass is supported above a substrate. At least one drive electrode is also supported above the substrate adjacent the proof mass. Typically, the proof mass and the drive electrode include interleaved electrode fingers. A sense plate or shield electrode on the substrate beneath the proof mass extends completely under the extent of the electrode fingers of proof mass.
摘要翻译：音叉陀螺仪设计，其中至少一个检测质量被支撑在基板上方。至少一个驱动电极也被支撑在与基体相邻的衬底上。通常，检测质量块和驱动电极包括交错的电极指。在证明物质下方的基底上的感应板或屏蔽电极在证明质量的电极指的范围内完全延伸。

3. 发明申请

WO0232762A3 ARTILLERY LAUNCHED FLYER ASSEMBLY 审中-公开
标题翻译： ARTILLERY推出飞行器总成
公开(公告)号：WO0232762A3
公开(公告)日：2004-01-08
申请号：PCT/US0131631
申请日：2001-10-11
申请人： DRAPER LAB CHARLES S
发明人： MARTORANA RICHARD T , ANDERSON JAMIE , SPEARING SIMON MARK , KESSLER SETH , APPLEBY BRENT , BERGMANN EDWARD , GEORGE SEAN , JACOBSON STEVEN , FLYER DONALD , DRELA MARK , KIRKOS GREGORY , MCFARLAND WILLIAM JR
IPC分类号： B64C39/02 , F42B15/10 , B64C3/56
CPC分类号： F42B15/105 , B64C39/024 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/185 , B64C2201/201
摘要： A flyer assembly (10) is adapted for launching with, transit in, and deployment from an artillery shell (22). The flyer assembly (10) includes a jettisonable shroud (12) and a flyer (14). The flyer (14) is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer (14) is positionable within the shroud (12) with the flyer axis parallel to the shroud axis and the shell axis. The flyer (14) includes a body member disposed about the flyer axis, and a foldable wing assembly (20) mounted to the body member. THe wing assembly (20) is characterized by a plurality of nested wing segments (32) when the flyer is in the first state. THe wing assembly (20) is configurable in an unfolded state characterized by a substantially uninterrupted aerodynamic surface when the flyer is in the second state. The flyer assembly (10) is launched from an artillery cannon, and can thus reach a target quickly, without expending energy stored with theflyer. During launch, the flwyer is coupled to the shroud so as to maintain a portion of the flyer in tension during an acceleration of the flyer along eht flyer axis.
摘要翻译：传单组件（10）适用于从炮弹（22）发射，转运和展开。传单组件（10）包括可喷射的护罩（12）和传单（14）。飞翼（14）适于在处于第一状态时承受沿飞行器轴线的发射加速力，并且在处于第二状态时实现空气动力学飞行。当处于第一状态时，传单（14）可定位在护罩（12）内，飞翼轴线平行于护罩轴线和外壳轴线。传单（14）包括围绕飞行器轴线设置的主体构件和安装到主体构件的可折叠翼组件（20）。当翼片处于第一状态时，翼组件（20）的特征在于多个嵌套翼段（32）。翼组件（20）可配置成展开状态，其特征在于当传单处于第二状态时基本上不间断的空气动力学表面。飞行器组件（10）从炮兵炮发射，并且因此能够快速地达到目标，而不会消耗与飞行器一起存储的能量。在发射过程中，飞镖耦合到护罩上，以便在飞行器沿着飞行器轴线的加速期间将传单的一部分保持在张紧状态。

4. 发明申请

WO0232762A9 FLYER ASSEMBLY 审中-公开
标题翻译：飞机装配
公开(公告)号：WO0232762A9
公开(公告)日：2003-02-20
申请号：PCT/US0131631
申请日：2001-10-11
申请人： DRAPER LAB CHARLES S
发明人： MARTORANA RICHARD T , ANDERSON JAMIE , SPEARING SIMON MARK , KESSLER SETH , APPLEBY BRENT , BERGMANN EDWARD , GEORGE SEAN , JACOBSON STEVEN , FLYER DONALD , DRELA MARK , KIRKOS GREGORY , MCFARLAND WILLIAM JR
IPC分类号： B64C39/02 , F42B15/10 , B64C
CPC分类号： F42B15/105 , B64C39/024 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/185 , B64C2201/201
摘要： A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state. The wing assembly is configurable in an unfolded state characterized by a substantially uninterrupted aerodynamic surface when the flyer is in the second state. The flyer assembly is adapted to be launched from a ballistic delivery system such as an artillery cannon, and can thus reach a target quickly, without expending system energy stored within the flyer. During launch, the flyer is coupled to the shroud so as to maintain a portion of the flyer in tension during an acceleration of the flyer along the flyer axis resulting from the launch. The flyer assembly is adapted to withstand the high g-load an high temperature environments of a cannon launch, and can tolerate a set-back g load of about 16,000 g.
摘要翻译：飞行器组件适用于从具有沿弹道壳轴线延伸的中心空隙区域的炮弹发射，转移和展开。传单组件包括可喷射的护罩和传单。护罩沿护罩轴线延伸，并且可定位在中心空隙区域内，护罩轴线基本上平行于外壳轴线。飞行器适于在处于第一状态时承受沿飞行器轴的发射加速力，并且在处于第二状态时实现空气动力学飞行。当处于第一状态时，传单可定位在护罩内，飞翼轴线平行于护罩轴线和外壳轴线。传单包括围绕飞翼轴设置的主体部件和安装到主体部件的可折叠翼组件。机翼组件可配置成折叠状态，其特征在于当传单处于第一状态时由多个嵌套翼段组成。机翼组件可配置为展开状态，其特征在于当传单处于第二状态时基本上不间断的空气动力学表面。飞行器组件适于从诸如炮兵炮的弹道传送系统发射，并且因此可以快速到达目标，而不会消耗存储在飞行物内的系统能量。在发射期间，传单联接到护罩上，以便在飞行物沿着由发射引起的飞翼轴的加速期间，使传单的一部分保持张紧。飞行器组件适于承受大炮发射的高温环境的高负载，并且可以承受大约16,000g的安装载荷。

5. 发明专利

AU3038702A Flyer assembly 未知
公开(公告)号：AU3038702A
公开(公告)日：2002-04-29
申请号：AU3038702
申请日：2001-10-11
申请人： DRAPER LAB CHARLES S
发明人： MARTORANA RICHARD T , ANDERSON JAMIE , SPEARING SIMON MARK , KESSLER SETH , APPLEBY BRENT , BERGMANN EDWARD , GEORGE SEAN , JACOBSON STEVEN , FLYER DONALD , DRELA MARK , KIRKOS GREGORY , MCFARLAND WILLIAM
IPC分类号： B64C39/02 , F42B15/10
摘要： A flyer assembly is adapted for launching with, transit in, and deployment from an artillery shell having a central void region extending along a ballistic shell axis. The flyer assembly includes a jettisonable shroud and a flyer. The shroud extends along a shroud axis, and is positionable within the central void region with the shroud axis substantially parallel to the shell axis. The flyer is adapted to withstand a launch acceleration force along a flyer axis when in a first state, and to effect aerodynamic flight when in a second state. When in the first state, the flyer is positionable within the shroud with the flyer axis parallel to the shroud axis and the shell axis. The flyer includes a body member disposed about the flyer axis, and a foldable wing assembly mounted to the body member. The wing assembly is configurable in a folded state characterized by a plurality of nested wing segments when the flyer is in the first state. The wing assembly is configurable in an unfolded state characterized by a substantially uninterrupted aerodynamic surface when the flyer is in the second state. The flyer assembly is adapted to be launched from a ballistic delivery system such as an artillery cannon, and can thus reach a target quickly, without expending system energy stored within the flyer. During launch, the flyer is coupled to the shroud so as to maintain a portion of the flyer in tension during an acceleration of the flyer along the flyer axis resulting from the launch. The flyer assembly is adapted to withstand the high g-load and high temperature environments of a cannon launch, and can tolerate a set-back g load of about 16,000 g.

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