DEVICE FOR PRODUCING SHAPED HOLES IN ARTICLES SUCH AS GAS TURBINE ENGINE COMPONENTS
    221.
    发明申请
    DEVICE FOR PRODUCING SHAPED HOLES IN ARTICLES SUCH AS GAS TURBINE ENGINE COMPONENTS 审中-公开
    用于在文章中生产形状的孔的装置,例如气体涡轮发动机部件

    公开(公告)号:WO1995017277A1

    公开(公告)日:1995-06-29

    申请号:PCT/US1994014268

    申请日:1994-12-07

    CPC classification number: B23H9/10

    Abstract: A multiple piece electrode for use with an electrical discharge machining device (EDM) includes at least one tooth. The electrode also includes a movable, elongated rod positioned inside each tooth. The movable rod may be secured to the tooth by several means such as a clamp mechanism, an epoxy, or by a securing mechanism attached to the processing equipment. When the electrode is advanced longitudinally into the workpiece, the rod forms a deep, small diameter hole and the tooth forms an enlarged opening at one end of the hole. The rod may be rotated to enhance hole depth capabilities. Additionally, the rod may be hollow, thus allowing a dielectric fluid to pass through the rod.

    Abstract translation: 用于放电加工装置(EDM)的多片电极包括至少一个齿。 电极还包括位于每个牙齿内的可移动的细长杆。 可移动杆可以通过诸如夹紧机构,环氧树脂或通过附接到处理设备的固定机构的几种手段固定到齿上。 当电极纵向前进到工件时,杆形成一个深的,小直径的孔,并且齿在孔的一端形成一个扩大的开口。 杆可以旋转以增强孔深度能力。 此外,杆可以是中空的,从而允许介电流体穿过杆。

    AIRFOIL HAVING COOLABLE LEADING EDGE REGION
    223.
    发明申请
    AIRFOIL HAVING COOLABLE LEADING EDGE REGION 审中-公开
    具有冷却领先边缘地区的飞机

    公开(公告)号:WO1995015430A1

    公开(公告)日:1995-06-08

    申请号:PCT/US1994013839

    申请日:1994-11-30

    CPC classification number: F01D5/186 Y02T50/673 Y02T50/676

    Abstract: A coolable rotor blade (16) having an airfoil section (18) is disclosed. Various construction details are developed which increase the cooling effectiveness under the airfoil section (18) under a variety of operative conditions. In one detailed embodiment, an array of rows of cooling air holes has two staggered rows in the spanwise direction which are spaced spanwisely in the row and chordwisely from row to row in a predetermined manner to ensure adequate cooling to the leading edge region should the aerodynamic leading edge shift.

    Abstract translation: 公开了一种具有翼型部分(18)的可冷却转子叶片(16)。 开发了各种结构细节,其在各种操作条件下增加在翼型部分(18)下的冷却效果。 在一个详细实施例中,排列的冷却空气孔的排列在翼展方向上具有两个交错排,这些行以预定的方式沿行方向逐行地排列并且以逐行排列,以确保如果空气动力学 前沿移位。

    TURBINE SHROUD SEGMENT
    224.
    发明申请
    TURBINE SHROUD SEGMENT 审中-公开
    涡轮SHROUD分段

    公开(公告)号:WO1995013456A1

    公开(公告)日:1995-05-18

    申请号:PCT/US1994008289

    申请日:1994-07-22

    CPC classification number: F01D25/246

    Abstract: A turbine shroud segment includes a center hook (70) along one edge which retains the segment to the turbine structure while permitting thermal distortion of the segment. In a particular embodiment, a segment includes a pair of spaced center hooks (70), a first lateral hook (72), and a second lateral hook (74) disposed oppositely of the first lateral hook. The spaced center hooks retain the segment and prevent radially inward movement of the center region of the segment. The lateral hooks provide supplemental retention while permitting the lateral edges of the segment to move radially outward in response to thermal distortion of the segment.

    Abstract translation: 涡轮机护罩段包括沿着一个边缘的中心钩(70),其将该段保持在涡轮结构上,同时允许该段的热变形。 在一个具体实施例中,一段包括一对间隔开的中心钩(70),第一侧钩(72)和与第一侧钩相对设置的第二侧钩(74)。 间隔开的中心钩保持该段并防止该段的中心区域的径向向内移动。 侧钩提供补充保持,同时允许段的横向边缘响应于段的热失真而径向向外移动。

    INTERLACED CORD CONVEYOR FOR AUTOMATED MATERIAL HANDLING
    225.
    发明申请
    INTERLACED CORD CONVEYOR FOR AUTOMATED MATERIAL HANDLING 审中-公开
    用于自动化材料处理的相互连接的输送机

    公开(公告)号:WO1995010468A1

    公开(公告)日:1995-04-20

    申请号:PCT/US1994010784

    申请日:1994-09-23

    Abstract: A pallet (19) of vertically stacked conveyor sections (15-17) utilizes translating cords (23) which may be juxtaposed between translating cords (22) on a workstation (18). The pallet is disposed on a standard lift table (34) so as to vertically align one of the conveyor sections (16) with the similar cords (22) of a workstation (20). Additional cords (51) may be disposed in alignment with the cords (23) of the conveyor sections (15-17) so as to fill the interstices between the juxtaposed cords (50) of the workstation. Grooved drums (28-31, 54) may be used in place of idler pulleys. A live center (66-68) may ensure proper alignment of a cluth gear (73) so as to drive the conveyor section cords on the pallet through a driven gear (71). The cords may be supported by flat shelves (117-119) having teflon3-coated fiberglass surfaces.

    Abstract translation: 垂直堆叠的输送机部分(15-17)的托盘(19)利用可在工作台(18)上的平移线(22)之间并置的平移线(23)。 托盘被放置在标准的升降台(34)上,以使其中一个输送机部分(16)与工作站(20)的类似的线(22)垂直对齐。 附加绳索(51)可以布置成与输送机部分(15-17)的帘线(23)对准,以便填充工作站的并置的帘线(50)之间的间隙。 可以使用凹槽(28-31,54)代替惰轮。 活动中心(66-68)可以确保冲击齿轮(73)的正确对准,以便通过从动齿轮(71)驱动托盘上的输送机部分绳索。 帘线可以由具有聚四氟乙烯涂覆的玻璃纤维表面的平架(117-119)支撑。

    VARIABLE PRIORITY COCKPIT WARNING AND DISPLAY SYSTEM
    226.
    发明申请
    VARIABLE PRIORITY COCKPIT WARNING AND DISPLAY SYSTEM 审中-公开
    可变优先的警报和显示系统

    公开(公告)号:WO1995009103A1

    公开(公告)日:1995-04-06

    申请号:PCT/US1994010594

    申请日:1994-09-20

    CPC classification number: B64D45/00

    Abstract: An aircraft warning and display system monitors the status of various aircraft equipement (20, 22), and provides cockpit audible and visual messages and indications (52, 53, 59, 67) indicative o f the operational status of the equipment. The operational status of the aircraft is monitored (37, 40), and in response to changes in the operational status of the aircraft for a given equipment status, the priority level of cockpit audible and visual messages and indications are modified to attract the attention of a pilot when pilot action is required. Additionally, information may be displayed (52) to the pilot that indicates specific actions needed to downgrade the priority level of the cockpit messages/indications.

    Abstract translation: 飞机警告和显示系统监控各种飞机设备(20,22)的状态,并提供驾驶员的听觉和视觉信息(52,53,59,67),指示设备的运行状态。 对飞机的运行状态进行监控(37,40),并针对给定设备状态对飞机运行状态的变化做出响应,修改了驾驶舱听觉和视觉信息和指示的优先级,以引起飞行员的注意 飞行员需要采取行动。 此外,信息可以显示(52)到飞行员,指示降低驾驶舱消息/指示的优先级所需的特定动作。

    DIRECTIONALLY SOLIDIFIED EUTECTIC REINFORCING FIBERS
    227.
    发明申请
    DIRECTIONALLY SOLIDIFIED EUTECTIC REINFORCING FIBERS 审中-公开
    方向固化的防腐增强纤维

    公开(公告)号:WO1995004013A1

    公开(公告)日:1995-02-09

    申请号:PCT/US1994007994

    申请日:1994-07-19

    Abstract: Eutectic reinforcing fibers for high temperature composites include eutectic mixtures such as Al2O3-Y2O3, Cr2O3-SiO2, MgO-Y2O3, CaO-NiO, and CaO-MgO. The fibers may be made by several solidification processes. The edge defined film fed growth process (EFG), however, may be especially appropriate. In this process, a seed having a known composition contacts the surface of a eutectic melt in a crucible and forms a molten film. In the present invention, the composition of the seed may be equal to the composition of the eutectic melt. As the seed is pulled upward, the molten film solidifies to form an eutectic fiber. Directional solidification occurs toward the melt.

    Abstract translation: 用于高温复合材料的共晶增强纤维包括共晶混合物如Al2O3-Y2O3,Cr2O3-SiO2,MgO-Y2O3,CaO-NiO和CaO-MgO。 纤维可以通过几种固化方法制成。 然而,边缘定义的膜进料生长过程(EFG)可能是特别合适的。 在该方法中,具有已知组成的种子与坩埚中的共晶熔体的表面接触并形成熔融膜。 在本发明中,种子的组成可以等于共晶熔体的组成。 当种子被向上拉时,熔融薄膜固化形成共晶纤维。 向熔体发生定向凝固。

    SYSTEM FOR AUTOMATIC LOADING OF VEHICLES FOR TRANSPORT
    228.
    发明申请
    SYSTEM FOR AUTOMATIC LOADING OF VEHICLES FOR TRANSPORT 审中-公开
    运输车辆自动装载系统

    公开(公告)号:WO1994023995A1

    公开(公告)日:1994-10-27

    申请号:PCT/US1994004181

    申请日:1994-04-14

    CPC classification number: B64C1/22 B64D9/00

    Abstract: A control system for automatically loading and unloading a vehicle (10) from a cargo compartment comprises a plurality of distance measuring sensors (31, 32, 33, 34) attached to specified locations on the exterior surfaces of the vehicle (54, 56, 57) and the cargo compartment (55). The sensors provide distance signals, indicative of the distance between each sensor and the nearest obstruction, to a microprocessor which compares each of the distance signals to reference signals indicative of the minimum allowable clearance between each specified location and an obstruction. During activation of an automatic loading/unloading switch (70), a winch (39) is activated to move the vehicle into or out of a cargo compartment if each of the distances is greater than the corresponding minimum allowable clearance. If any clearance is less than the minimum allowable clearance while the vehicle is being moved, movement of the vehicle is automatically stopped and the height of the vehicle is adjusted (800-815) until all of the distances are greater than the corresponding minimum allowable clearances, after which the winch is reactivated to continue moving the vehicle. The cycle is repeated until the helicopter is in its final position or the automatic loading/unloading switch is released.

    Abstract translation: 用于从货舱自动装载和卸载车辆(10)的控制系统包括附接到车辆(54,56,57)的外表面上的特定位置的多个距离测量传感器(31,32,33,34) )和货舱(55)。 传感器将指示每个传感器和最近的障碍物之间的距离的距离信号提供给微处理器,该微处理器将每个距离信号与指示每个指定位置与阻塞之间的最小允许间隙的参考信号进行比较。 在启动自动装载/卸载开关(70)期间,如果每个距离大于相应的最小允许间隙,则启动绞盘(39)以将车辆移入或移出货舱。 如果任何间隙小于车辆移动时的最小允许间隙,则自动停止车辆的移动,并调整车辆的高度(800-815),直到所有距离都大于相应的最小允许间隙 之后,绞车被重新启动以继续移动车辆。 重复该循环直到直升机处于其最终位置或释放自动装载/卸载开关。

    FAIL SAFE DRIVE SHAFT SYSTEM
    229.
    发明申请
    FAIL SAFE DRIVE SHAFT SYSTEM 审中-公开
    失效安全驱动轴系统

    公开(公告)号:WO1994018070A2

    公开(公告)日:1994-08-18

    申请号:PCT/US1994000954

    申请日:1994-01-26

    Abstract: A fail safe, segmented drive shaft system includes a segment support assembly (16) comprising a ball bearing (26), for primary rotation, disposed within a journal bearing (28), for secondary rotation, which is disposed within an elastomeric damper (30) that has a vibration probe (34) placed in it for failure detection, and a coupling assembly (18) comprising a flexible diaphragm (66, 67) for primary, flexible coupling between segments and gear teeth (72, 73) which engage for secondary coupling upon failure of the diaphragm (66, 67). The teeth are not concentric with the rotational axis, so vibration indicates failure of the primary flexible coupling.

    Abstract translation: 一个故障安全的,分段的驱动轴系统包括段支撑组件(16),其包括用于初级旋转的滚珠轴承(26),其设置在轴颈轴承(28)内,用于二次旋转,所述轴承轴承布置在弹性阻尼器 ),其具有放置在其中以用于故障检测的振动探测器(34),以及联接组件(18),其包括柔性隔膜(66,67),用于段和齿轮齿(72,73)之间的初级,柔性联接, 隔膜(66,67)故障时的二次联轴器。 齿不与旋转轴同心,所以振动指示主柔性联轴器的故障。

    PRESSURE TOLERANT FUEL TANK PANELS
    230.
    发明申请
    PRESSURE TOLERANT FUEL TANK PANELS 审中-公开
    压力容器燃油面板

    公开(公告)号:WO1994016882A1

    公开(公告)日:1994-08-04

    申请号:PCT/US1993012681

    申请日:1993-12-30

    Abstract: A pressure tolerant composite panel has an inner fiber reinforced layer, an outer fiber reinforced layer and a core disposed therebetween. In one embodiment of the invention, the inner layer (25) has weakening structures (30) incorporated at the peripheral edges thereof, and has an outer layer (26) of a different and lower modulus of elasticity than the inner layer to provide some degree of elongation. When high internal forces are encountered, the weakening structures allow the inner layer to separate, with the outer layers stretching to absorb the forces without failure. Optionally, strengthening straps (28, 29) are positioned about the panel such that it is compartmentalized into discrete sections to contain damage in localized areas. In an alternative embodiment of the invention, the inner core (27) is produced of a crushable material which has a yield strength sufficient to provide structural support under normal operating conditions. When a high pressure is encountered which exceeds the yield limit, the core is crushed to prevent force transmission to the outer layer. Such a composite panel assures survivability of the panel when subjected to impact damage.

    Abstract translation: 耐压复合板具有内纤维增强层,外纤维增强层和设置在其间的芯。 在本发明的一个实施例中,内层(25)具有结合在其外围边缘处的弱化结构(30),并且具有与内层不同的和较低的弹性模量的外层(26),以提供一定的程度 的伸长率。 当遇到高内力时,弱化结构允许内层分离,外层伸展以吸收力而不发生故障。 可选地,加强带(28,29)围绕面板定位,使得其被划分成离散部分以在局部区域中包含损伤。 在本发明的替代实施例中,内芯(27)由可压碎材料制成,其具有足以在正常操作条件下提供结构支撑的屈服强度。 当遇到超过屈服极限的高压时,芯被压碎以防止力传递到外层。 这样的复合板在受到冲击损坏时确保了板的生存性。

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