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    NUTRITIONAL FOOD PRODUCTS EMPLOYING GELLED PROTEIN FORMULATIONS
    1.
    发明申请
    NUTRITIONAL FOOD PRODUCTS EMPLOYING GELLED PROTEIN FORMULATIONS 审中-公开
    使用凝胶蛋白制剂的营养食品

    公开(公告)号：WO2007035595A1

    公开(公告)日：2007-03-29

    申请号：PCT/US2006/036219

    申请日：2006-09-18

    Applicant: MARTIN, Robert, W., Jr.

    Inventor： MARTIN, Robert, W., Jr.

    IPC: A23J1/00

    CPC classification number: A23G9/38 ,  A23L33/17 ,  A23L33/185 ,  A23L33/19

    Abstract: This invention relates to nutritional food products having palatable/organoleptic characteristics. The palatable/organoleptic characteristics are obtained in part through use of gelled whey protein, soy protein and egg protein containing formulations. Such nutritional food products include powders, liquids and, especially, frozen foods such as frozen nutrition bars and cones. Methods for making such products are also disclosed.

    Abstract translation: 本发明涉及具有可口/感官特征的营养食品。 可口/感官特征部分通过使用凝胶乳清蛋白，大豆蛋白和含蛋白的制剂获得。 这种营养食品包括粉末，液体，特别是冷冻食品，如冷冻营养棒和锥体。 还公开了制造这种产品的方法。

    METHODS AND APPARATUS FOR DEPLOYING CONTROL SURFACES SEQUENTIALLY
    2.
    发明申请
    METHODS AND APPARATUS FOR DEPLOYING CONTROL SURFACES SEQUENTIALLY 审中-公开
    依次配置控制表面的方法和装置

    公开(公告)号：WO2009067402A1

    公开(公告)日：2009-05-28

    申请号：PCT/US2008/083765

    申请日：2008-11-17

    Applicant: RAYTHEON COMPANY ,  TURNER, Damon, C. ,  MARTIN, Robert, W.

    Inventor： TURNER, Damon, C. ,  MARTIN, Robert, W.

    IPC: F42B10/14

    CPC classification number: F42B10/14 ,  F42B10/64

    Abstract: Methods and apparatus for deploying control surfaces generally comprise a fin deployment system for projectiles. the fin deployment system is used to control the timing of the control surface deployment. In one embodiment, the deployment system comprises a clip that is configured to react the biasing force of one control surface against another in order to maintain the control surfaces in a non-deployed state until at least one control surface is able to overcome the retention force of the clip, thus beginning a chain reaction in which all of the control surfaces deploy sequentially.

    Abstract translation: 用于部署控制表面的方法和装置通常包括用于射弹的翅片展开系统。 翅片部署系统用于控制控制面部署的时序。 在一个实施例中，展开系统包括夹子，该夹子被配置为使一个控制表面的偏置力抵抗另一个控制表面，以便将控制表面维持在非展开状态，直到至少一个控制表面能够克服保持力 从而开始连锁反应，其中所有控制表面顺序地部署。

    DEPLOYMENT SYSTEM FOR AIRBORNE OBJECT COMPRISING A TORSION STOP
    3.
    发明申请
    DEPLOYMENT SYSTEM FOR AIRBORNE OBJECT COMPRISING A TORSION STOP 审中-公开
    包含扭矩停止的AIRBORNE对象的部署系统

    公开(公告)号：WO2011046640A3

    公开(公告)日：2011-06-09

    申请号：PCT/US2010038508

    申请日：2010-06-14

    Applicant: RAYTHEON CO ,  MARTIN ROBERT W

    Inventor： MARTIN ROBERT W

    IPC: F42B10/14

    CPC classification number: F42B10/14

    Abstract: Embodiments of a torsion stop deployment system for utilization onboard an airborne object are provided. In one embodiment, the torsion stop deployment system includes a deployable element hingedly coupled to the airborne object and rotatable from a non-deployed position to a deployed position. The torsion stop deployment system further includes a torsion bar member, which is fixedly coupled to the airborne object and which resiliently resists the rotation of the deployable element to reduce shock to the airborne object during deployment of the deployable element.

    Abstract translation: 提供了一种在机载物体上使用的扭转停止展开系统的实施例。 在一个实施例中，扭转止动部署系统包括铰接地连接到机载物体并可从非展开位置旋转到展开位置的展开元件。 扭转止动部署系统还包括扭杆构件，该扭杆构件固定地联接到机载物体并且弹性地抵抗可展开元件的旋转，以在展开可展开元件的部署期间减少对机载对象的冲击。

    TORSION STOP DEPLOYMENT SYSTEM FOR AIRBORNE OBJECT
    5.
    发明申请
    TORSION STOP DEPLOYMENT SYSTEM FOR AIRBORNE OBJECT 审中-公开
    AIRBORNE对象的扭矩停止部署系统

    公开(公告)号：WO2011046640A2

    公开(公告)日：2011-04-21

    申请号：PCT/US2010/038508

    申请日：2010-06-14

    Applicant: RAYTHEON COMPANY ,  MARTIN, Robert W.

    Inventor： MARTIN, Robert W.

    IPC: F42B10/14

    CPC classification number: F42B10/14

    Abstract: Embodiments of a torsion stop deployment system for utilization onboard an airborne object are provided. In one embodiment, the torsion stop deployment system includes a deployable element hingedly coupled to the airborne object and rotatable from a non-deployed position to a deployed position. The torsion stop deployment system further includes a torsion bar member, which is fixedly coupled to the airborne object and which resiliently resists the rotation of the deployable element to reduce shock to the airborne object during deployment of the deployable element.

    Abstract translation: 提供了一种在机载物体上使用的扭转停止展开系统的实施例。 在一个实施例中，扭转停止展开系统包括铰接地连接到机载物体并且可以从非展开位置旋转到展开位置的展开元件。 扭转停止展开系统还包括扭杆构件，该扭杆构件固定地联接到机载物体并且弹性地抵抗可展开元件的旋转，以在展开可部署元件的过程中减少对机载对象的冲击。

    FERTILIZER OPENER/CLOSER ARRANGEMENT FOR AN AGRICULTURAL MACHINE
    6.
    发明申请
    FERTILIZER OPENER/CLOSER ARRANGEMENT FOR AN AGRICULTURAL MACHINE 审中-公开
    农业机械肥料开关机/封闭机装置

    公开(公告)号：WO2009032829A1

    公开(公告)日：2009-03-12

    申请号：PCT/US2008/075094

    申请日：2008-09-03

    Applicant: DEERE & COMPANY ,  MARTIN, Robert, W. ,  PETERSON, James, R., Jr.

    Inventor： MARTIN, Robert, W. ,  PETERSON, James, R., Jr.

    IPC: A01B49/06

    CPC classification number: A01C5/066 ,  A01C5/064

    Abstract: An agricultural soil trench opening machine includes at least one opener/closer arrangement carried by a tool bar. Each opener/closer arrangement includes an opener disc positioned at an angle relative to a working direction and defining a trench profile. The opener disc has an axis of rotation and leading and trailing edges positioned adjacent one side of the trench profile. A gauge wheel is, generally, adjacent to the trailing edge of and inline with the opener disc. The gauge wheel has a leading edge positioned between opener disc leading and trailing edges. A first closing wheel is positioned on a side of the trench profile opposite to the gauge wheel. The first closing wheel has a leading edge positioned between the axis of rotation and the trailing edge of the opener disc. A second closing wheel is positioned on a same side of the trench profile as the gauge wheel.

    Abstract translation: 农业土壤开沟机包括由工具栏承载的至少一个开启/关闭装置。 每个开启/关闭装置包括一个开启盘，该开启盘相对于工作方向成一定角度并且限定一个沟槽轮廓。 开启盘具有旋转轴线，并且位于与沟槽轮廓的一侧相邻的前缘和后缘。 量规轮通常与开启盘的后缘相邻并且与开启盘一致。 量规轮具有位于开启盘前缘和后缘之间的前缘。 第一闭合轮位于与量规轮相对的沟槽轮廓的一侧。 第一关闭轮具有位于旋转轴线和开启盘的后缘之间的前缘。 第二闭合轮位于与测量轮相同的沟槽轮廓侧。

    COMPACT FUEL INJECTION NOZZLE
    8.
    发明申请
    COMPACT FUEL INJECTION NOZZLE 审中-公开
    紧凑型燃油喷射喷嘴

    公开(公告)号：WO0136811A3

    公开(公告)日：2002-02-21

    申请号：PCT/US0031537

    申请日：2000-11-17

    Applicant: STANADYNE AUTOMOTIVE CORP ,  BRIEN MICHAEL O ,  MARTIN ROBERT W JR

    Inventor： O BRIEN MICHAEL ,  MARTIN ROBERT W JR

    IPC: F02M61/10 ,  F02M61/16 ,  F02M61/18 ,  F02M61/20

    CPC classification number: F02M61/205 ,  F02M61/10 ,  F02M61/161 ,  F02M61/168 ,  F02M61/18

    Abstract: A compact fuel injection nozzle (68 1) includes a unitary nozzle body (70 1), a nozzle cap (72 1), a valve member (82) and a spring sub assembly. The spring sub assembly (140) provides a biasing force against a valve member (82) that includes an integral lift stop. The biasing force holds the nose of the valve member (82) against the valve seat (88) of the nozzle body (70 1) until the fuel pressure inside the injector exceeds a minimum opening pressure. The lift stop (138) provides a stop limit, permitting the valve member (82) to move away from the valve seat (88) a predetermined axial distance. The minimum opening pressure and valve opening axial distance may be calibrated by selection and installation of shims (142).

    Abstract translation: 紧凑型燃料喷射喷嘴（68 1）包括单一喷嘴体（70 1），喷嘴盖（72 1），阀构件（82）和弹簧子组件。 弹簧副组件（140）提供抵抗包括一体式提升挡块的阀构件（82）的偏压力。 偏压力使阀构件（82）的鼻部抵靠喷嘴体（70 1）的阀座（88），直到喷射器内部的燃料压力超过最小开启压力。 提升挡块（138）提供止动限制，允许阀构件（82）以预定的轴向距离离开阀座（88）。 可以通过选择和安装垫片（142）来校准最小开启压力和阀门开启轴向距离。

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