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1. 发明授权

US07989744B2 Methods and apparatus for transferring a fluid 有权
标题翻译：用于转移流体的方法和装置
公开(公告)号：US07989744B2
公开(公告)日：2011-08-02
申请号：US12024532
申请日：2008-02-01
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Michael D. Do
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Michael D. Do
IPC分类号： B64G1/24 , F42B15/01 , F42B15/00
CPC分类号： F42B15/01
摘要： Methods and apparatus for a missile having an external system operate in conjunction with an airframe and a fluid transfer system. The airframe includes an interior surface defining a substantially enclosed internal chamber. The fluid transfer system selectively connects the internal chamber to the external system, for example to provide pressurant or coolant to the external system.
摘要翻译：具有外部系统的导弹的方法和装置与机身和流体传输系统一起操作。机身包括限定基本封闭的内部腔室的内表面。流体传输系统选择性地将内部室连接到外部系统，例如以向外部系统提供加压或冷却剂。

2. 发明申请

US20090194632A1 METHODS AND APPARATUS FOR TRANSFERRING A FLUID 有权
标题翻译：用于传输流体的方法和装置
公开(公告)号：US20090194632A1
公开(公告)日：2009-08-06
申请号：US12024532
申请日：2008-02-01
申请人： ANDREW B. FACCIANO , Robert T. Moore , Gregg J. Hlavacek , Michael D. Do
发明人： ANDREW B. FACCIANO , Robert T. Moore , Gregg J. Hlavacek , Michael D. Do
IPC分类号： F42B15/00 , F42B15/01 , G01F11/00
CPC分类号： F42B15/01
摘要： Methods and apparatus for a missile having an external system operate in conjunction with an airframe and a fluid transfer system. The airframe includes an interior surface defining a substantially enclosed internal chamber. The fluid transfer system selectively connects the internal chamber to the external system, for example to provide pressurant or coolant to the external system.
摘要翻译：具有外部系统的导弹的方法和装置与机身和流体传输系统一起操作。机身包括限定基本封闭的内部腔室的内表面。流体传输系统选择性地将内部室连接到外部系统，例如以向外部系统提供加压或冷却剂。

3. 发明授权

US08049148B2 Missile airframe and structure comprising piezoelectric fibers and method for active structural response control 有权
标题翻译：导弹机体和包括压电纤维的结构和主动结构响应控制方法
公开(公告)号：US08049148B2
公开(公告)日：2011-11-01
申请号：US12823683
申请日：2010-06-25
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
IPC分类号： F42B15/01 , H02N2/00 , F42B15/00
CPC分类号： H01L41/08 , F42B10/00 , F42B15/10 , H01L41/04
摘要： Embodiments of a missile, an airframe and a structure comprising piezoelectric fibers and a method for active structural response control are generally described herein. In some embodiments, a housing structure includes a composite material containing a plurality of piezoelectric fibers adapted to generate an electrical signal in response to a deformation in the structure and to deform the structure to provide low frequency stiffness and strength performance while attenuating high frequency vibrations.
摘要翻译：导弹，机身和包括压电纤维的结构的实施例和用于主动结构响应控制的方法一般在本文中描述。在一些实施例中，壳体结构包括复合材料，其包含多个压电纤维，其适于响应于结构中的变形而产生电信号，并且使结构变形以提供低频刚度和强度性能，同时衰减高频振动。

4. 发明授权

US07509903B2 Separable structure material 有权
标题翻译：可分离的结构材料
公开(公告)号：US07509903B2
公开(公告)日：2009-03-31
申请号：US11190297
申请日：2005-07-27
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
IPC分类号： B64G1/64
CPC分类号： F42B15/38 , Y10T428/15
摘要： A separable structure includes composite material that is separated or severed by a reactive pyrotechnic material. According to one embodiment, the structure includes a pair of composite laminate structural portions, each including multiple layers of composite material. The portions each extend into an overlap region, within which the composite layers of the two structural portions may be alternately placed, overlapping one another. A reactive material is also placed within this overlap region, for instance being in layers between pairs of the composite material layers. The reactive material may be ignited to cause destruction of the pyrotechnic material, and a matrix or resin material of the composite materials layers in the overlap region. This causes the structure to sever or separate along a line of separation within the overlap region. The separation may occur without need to sever fibers of the composite material.
摘要翻译：可分离结构包括由反应性烟火材料分离或切断的复合材料。根据一个实施例，该结构包括一对复合层压结构部分，每个复合层压结构部分包括多层复合材料。这些部分各自延伸到重叠区域中，两个结构部分的复合层可以交替放置在该重叠区域内，彼此重叠。反应性材料也被放置在该重叠区域内，例如在复合材料层对之间的层中。可以点燃反应性材料以引起烟火材料的破坏，并且重叠区域中的复合材料层的基质或树脂材料层。这导致结构沿着重叠区域内的分离线断开或分离。可能发生分离而不需要切断复合材料的纤维。

5. 发明申请

US20100264251A1 MISSILE AIRFRAME AND STRUCTURE COMPRISING PIEZOELECTRIC FIBERS AND METHOD FOR ACTIVE STRUCTURAL RESPONSE CONTROL 有权
标题翻译：包含压电纤维的空气弹性体结构和主动结构响应控制方法
公开(公告)号：US20100264251A1
公开(公告)日：2010-10-21
申请号：US12823683
申请日：2010-06-25
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
IPC分类号： F42B15/01 , F42B15/00 , H01L41/053 , H01L41/09
CPC分类号： H01L41/08 , F42B10/00 , F42B15/10 , H01L41/04
摘要： Embodiments of a missile, an airframe and a structure comprising piezoelectric fibers and a method for active structural response control are generally described herein. In some embodiments, a housing structure includes a composite material containing a plurality of piezoelectric fibers adapted to generate an electrical signal in response to a deformation in the structure and to deform the structure in response to an electrical signal applied thereto. A control circuit receives the sensed signal from the fibers and generates an excitation signal that is applied to the fibers to increase the stiffness or compliance of the fibers at predetermined frequencies. In an illustrative embodiment, the control signal is adapted to provide low frequency stiffness and strength performance while attenuating high frequency vibrations to protect electronics housed within the structure.
摘要翻译：导弹，机身和包括压电纤维的结构的实施例和用于主动结构响应控制的方法一般在本文中描述。在一些实施例中，壳体结构包括复合材料，其包含多个压电纤维，其适于响应于结构中的变形而产生电信号，并且响应于施加到其上的电信号使结构变形。控制电路从光纤接收感测到的信号，并产生施加到光纤的激励信号，以增加光纤在预定频率下的刚度或顺应性。在说明性实施例中，控制信号适于提供低频刚度和强度性能，同时衰减高频振动以保护容纳在结构内的电子元件。

6. 发明申请

US20090071320A1 SEPARABLE STRUCTURE MATERIAL METHOD 有权
标题翻译：可分离结构材料方法
公开(公告)号：US20090071320A1
公开(公告)日：2009-03-19
申请号：US12274660
申请日：2008-11-20
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
IPC分类号： F42D3/00
CPC分类号： F42B15/38 , Y10T428/15
摘要： A separable structure includes composite material that is separated or severed by a reactive pyrotechnic material. According to one embodiment, the structure includes a pair of composite laminate structural portions, each including multiple layers of composite material. The portions each extend into an overlap region, within which the composite layers of the two structural portions may be alternately placed, overlapping one another. A reactive material is also placed within this overlap region, for instance being in layers between pairs of the composite material layers. The reactive material may be ignited to cause destruction of the pyrotechnic material, and a matrix or resin material of the composite materials layers in the overlap region. This causes the structure to sever or separate along a line of separation within the overlap region. The separation may occur without need to sever fibers of the composite material.
摘要翻译：可分离结构包括由反应性烟火材料分离或切断的复合材料。根据一个实施例，该结构包括一对复合层压结构部分，每个复合层压结构部分包括多层复合材料。这些部分各自延伸到重叠区域中，两个结构部分的复合层可以交替放置在该重叠区域内，彼此重叠。反应性材料也被放置在该重叠区域内，例如在复合材料层对之间的层中。可以点燃反应性材料以引起烟火材料的破坏，并且重叠区域中的复合材料层的基质或树脂材料层。这导致结构沿着重叠区域内的分离线断开或分离。可能发生分离而不需要切断复合材料的纤维。

7. 发明授权

US07819048B2 Separable structure material method 有权
标题翻译：可分离结构材料法
公开(公告)号：US07819048B2
公开(公告)日：2010-10-26
申请号：US12274660
申请日：2008-11-20
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek
IPC分类号： B64G1/64
CPC分类号： F42B15/38 , Y10T428/15
摘要： A separable structure includes composite material that is separated or severed by a reactive pyrotechnic material. According to one embodiment, the structure includes a pair of composite laminate structural portions, each including multiple layers of composite material. The portions each extend into an overlap region, within which the composite layers of the two structural portions may be alternately placed, overlapping one another. A reactive material is also placed within this overlap region, for instance being in layers between pairs of the composite material layers. The reactive material may be ignited to cause destruction of the pyrotechnic material, and a matrix or resin material of the composite materials layers in the overlap region. This causes the structure to sever or separate along a line of separation within the overlap region. The separation may occur without need to sever fibers of the composite material.
摘要翻译：可分离结构包括由反应性烟火材料分离或切断的复合材料。根据一个实施例，该结构包括一对复合层压结构部分，每个复合层压结构部分包括多层复合材料。这些部分各自延伸到重叠区域中，两个结构部分的复合层可以交替放置在该重叠区域内，彼此重叠。反应性材料也被放置在该重叠区域内，例如在复合材料层对之间的层中。可以点燃反应性材料以引起烟火材料的破坏，并且重叠区域中的复合材料层的基质或树脂材料层。这导致结构沿着重叠区域内的分离线断开或分离。可能发生分离而不需要切断复合材料的纤维。

8. 发明授权

US07767944B2 Piezoelectric fiber, active damped, composite electronic housings 有权
标题翻译：压电纤维，主动阻尼，复合电子外壳
公开(公告)号：US07767944B2
公开(公告)日：2010-08-03
申请号：US11715034
申请日：2007-03-07
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
IPC分类号： F41G7/00 , F42B15/10
CPC分类号： H01L41/08 , F42B10/00 , F42B15/10 , H01L41/04
摘要： A vibration controlled housing. The novel housing includes a housing structure and a mechanism for receiving a control signal and in accordance therewith electronically tuning a structural response of the structure. In an illustrative embodiment, the housing structure includes a composite material containing a plurality of piezoelectric fibers adapted to generate an electrical signal in response to a deformation in the structure and to deform the structure in response to an electrical signal applied thereto. A control circuit receives the sensed signal from the fibers and generates an excitation signal that is applied to the fibers to increase the stiffness or compliance of the fibers at predetermined frequencies. In an illustrative embodiment, the control signal is adapted to provide low frequency stiffness and strength performance while attenuating high frequency vibrations to protect electronics housed within the structure.
摘要翻译：振动控制的外壳。新颖的壳体包括壳体结构和用于接收控制信号并根据其电子调谐结构的结构响应的机构。在说明性实施例中，壳体结构包括复合材料，其包含多个压电纤维，其适于响应于结构中的变形而产生电信号，并且响应于施加到其上的电信号使结构变形。控制电路从光纤接收感测到的信号，并产生施加到光纤的激励信号，以增加光纤在预定频率下的刚度或顺应性。在说明性实施例中，控制信号适于提供低频刚度和强度性能，同时衰减高频振动以保护容纳在结构内的电子元件。

9. 发明授权

US07681834B2 Composite missile nose cone 有权
标题翻译：复合导弹鼻锥
公开(公告)号：US07681834B2
公开(公告)日：2010-03-23
申请号：US11395794
申请日：2006-03-31
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
IPC分类号： B64C1/00
CPC分类号： F42B10/46 , H01Q1/281 , H01Q1/42 , H01Q21/065
摘要： A missile includes a radome-seeker airframe assembly that has a single-piece composite material forebody. The forebody is made of a high-temperature composite material that can withstand heat with little or no ablation. The forebody has a front part with an ogive shape and an aft part that has a cylindrical shape. The front part acts as a radome for a seeker located within the forebody. Patch antennas are attached to an inside surface of the cylindrical aft part. The aft part acts as a radome for the patch antennas, allowing signals to be sent and received by the patch antennas without a need for cutouts. A single seal may be used to seal the guidance system and seeker within the forebody, allowing the equipment to be hermetically sealed within the forebody.
摘要翻译：导弹包括具有单件复合材料前身的天线探头机身机身组件。前体由高温复合材料制成，能够耐受很少或无消融的热量。前身具有具有圆柱形状的前部，其具有凹凸形状和后部。前部作为位于前体内的寻求者的天线罩。贴片天线连接到圆筒形后部的内表面。尾部作为贴片天线的天线罩，允许由贴片天线发送和接收信号，而不需要切口。可以使用单个密封件来密封前体内的引导系统和探测器，从而允许设备在前体内气密密封。

10. 发明申请

US20080217465A1 Piezoelectric fiber, active damped, composite electronic housings 有权
标题翻译：压电纤维，主动阻尼，复合电子外壳
公开(公告)号：US20080217465A1
公开(公告)日：2008-09-11
申请号：US11715034
申请日：2007-03-07
申请人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
发明人： Andrew B. Facciano , Robert T. Moore , Gregg J. Hlavacek , Craig D. Seasly
IPC分类号： F41G9/00 , H01L41/08
CPC分类号： H01L41/08 , F42B10/00 , F42B15/10 , H01L41/04
摘要： A vibration controlled housing. The novel housing includes a housing structure and a mechanism for receiving a control signal and in accordance therewith electronically tuning a structural response of the structure. In an illustrative embodiment, the housing structure includes a composite material containing a plurality of piezoelectric fibers adapted to generate an electrical signal in response to a deformation in the structure and to deform the structure in response to an electrical signal applied thereto. A control circuit receives the sensed signal from the fibers and generates an excitation signal that is applied to the fibers to increase the stiffness or compliance of the fibers at predetermined frequencies. In an illustrative embodiment, the control signal is adapted to provide low frequency stiffness and strength performance while attenuating high frequency vibrations to protect electronics housed within the structure.
摘要翻译：振动控制的外壳。新颖的壳体包括壳体结构和用于接收控制信号并根据其电子调谐结构的结构响应的机构。在说明性实施例中，壳体结构包括复合材料，其包含多个压电纤维，其适于响应于结构中的变形而产生电信号，并且响应于施加到其上的电信号使结构变形。控制电路从光纤接收感测到的信号，并产生施加到光纤的激励信号，以增加光纤在预定频率下的刚度或顺应性。在说明性实施例中，控制信号适于提供低频刚度和强度性能，同时衰减高频振动以保护容纳在结构内的电子元件。

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