公开(公告)号：WO1994014154A1

公开(公告)日：1994-06-23

申请号：PCT/US1993011930

申请日：1993-12-08

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  KAPOOR, Mohan, L. ,  MONARCHIE, Dominick, L. ,  REBESCHI, Thomas, J. ,  BUDZILEK, Russell, A.

IPC: G09G03/30

CPC classification number: G09G3/30 ,  G09G2310/027

Abstract: A thin film electroluminescent display panel is driven with either a symmetric or asymmetric drive scheme which includes at least one equalizing voltage pulse per write cycle to remove carriers trapped at the interfaces of dielectric layers and phosphor layer in order to stabilize the charge of each display panel pixel. The present invention reduces the smearing, latent image and pseudo persistence problems caused by carriers being retained and accumulated at the dielectric and phosphor layer interfaces.

Abstract translation: 薄膜电致发光显示面板由对称或非对称驱动方案驱动，每个写周期包括至少一个均衡电压脉冲，以去除俘获在电介质层和磷光体层的界面处的载流子，以便稳定每个显示面板的电荷 像素。 本发明减少了载流子在电介质层和荧光体层界面处被保留和积聚引起的污迹，潜影和伪持久性问题。

公开(公告)号：WO1994013849A1

公开(公告)日：1994-06-23

申请号：PCT/US1993010905

申请日：1993-11-10

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  MILLER, John, A. ,  PAULONIS, Daniel, F. ,  GENEREUX, Paul, D. ,  SAMUELSON, Jeffrey, W. ,  JACKMAN, Laurence, A. ,  VACCARO, Frederick, P. ,  THOMAS, William, M.

IPC: C22F01/10

CPC classification number: C22C19/056 ,  C22F1/10

Abstract: A process for producing a fine grain forged superalloy article having a high yield strength at intermediate temperatures. A preferred starting composition comprises, by weight, 15 % Cr, 13.6 % Co, 4.1 % Mo, 4.6 % Ti, 2.2 % Al, .01 % C, 0.007 % B, 0.07 % Zr, balance Ni. This material is forged at a temperature above the gamma prime solvus and at a true strain of at least .5. Alternately, the material may be forged below the gamma prime solvus temperature with intermediate super solvus anneals. The overaged material is then worked at a temperature below the gamma prime solvus. The resultant fine grain material is then heat treated or can be further isothermally forged prior to heat treatment to produce complex shapes.

Abstract translation: 一种在中间温度下具有高屈服强度的细晶粒锻造超合金制品的制造方法。 优选的起始组合物包含15％Cr，13.6％Co，4.1％Mo，4.6％Ti，2.2％Al，0.01％C，0.007％B，0.07％Zr，余量为Ni。 该材料在高于伽玛质子溶液的温度下锻炼，至少真正的应变为0.5。 或者，可以用中等超固溶退火将材料锻造成低于伽马质子溶质温度。 然后将过时的材料在低于伽玛质子溶液的温度下进行加工。 然后将所得细晶粒材料进行热处理，或者可以在热处理之前进一步等温锻造以产生复杂形状。

公开(公告)号：WO1994013581A1

公开(公告)日：1994-06-23

申请号：PCT/US1993010415

申请日：1993-10-29

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  XIAO, Youming ,  TAN, Beng, Jit ,  SUIB, Steven, Lawrence ,  GALASSO, Francis, S.

IPC: C01B21/06

CPC classification number: C01B21/0726 ,  C01B21/06 ,  C01B21/0765 ,  C01P2002/72

Abstract: A metal nitride powder can be made by heating a reactant powder that includes an oxide or hydroxide of Al, Ti, or Zr to a reaction temperature in a nonreactive atmosphere. The heated reactant powder is contacted with a gaseous reactant mixture comprising a nitrogen source and a carbon source. The molar ratio of nitrogen to carbon in the gaseous reactant mixture is at least about 15. The reactant powder is maintained at the reaction temperature for a sufficient time to convert a portion of it to metal nitride powder.

Abstract translation: 可以通过将包含Al，Ti或Zr的氧化物或氢氧化物的反应物粉末加热至非反应性气氛中的反应温度来制备金属氮化物粉末。 加热的反应物粉末与包含氮源和碳源的气态反应物混合物接触。 气态反应物混合物中氮与碳的摩尔比至少约为15.反应物粉末在反应温度下保持足够的时间以将其一部分转化为金属氮化物粉末。

公开(公告)号：WO1994013530A2

公开(公告)日：1994-06-23

申请号：PCT/US1993011483

申请日：1993-11-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  REINFELDER, William, C. ,  PURSE, Jeffry, C.

IPC: B64C0

CPC classification number: B64C27/46 ,  B64C27/008 ,  Y10S416/50

Abstract: A rotor blade balance weight assembly comprises a weight retention housing (10) having a hollow core (22) and being closed on one end (12). The housing is disposed in an aperture which extends from the upper (52) to the lower (53) airfoil surfaces of the rotor blade (50). The closure end of the housing is contoured to match the airfoil upper surface contour. A stud (70) extends along the central axis of the housing, and washer-like balance weights (72) are received over the stud and secured by a locking nut (75). The open end of the housing is closed by a cover plate (25) that is contoured to match the airfoil lower surface contour, the cover plate being secured to the housing by a nut (78) in locking engagement with the stud. A pair of clips (37) are received within the housing, each clip having a tab suface (40) which extends through slots (42) in the housing, the clips being secured by the locking nut and stud. The cover plate and housing closed end are counter sunk (17, 59, 27) to provide a smooth airfoil surface.

Abstract translation: 转子叶片平衡配重组件包括具有中空芯（22）并且在一端（12）上封闭的重量保持壳体（10）。 壳体设置在从转子叶片（50）的上部（52）到下部（53）翼型表面延伸的孔中。 壳体的封闭端形状与翼型上表面轮廓相匹配。 螺柱（70）沿着壳体的中心轴线延伸，并且垫圈状平衡重（72）被接收在螺柱上并由锁定螺母（75）固定。 壳体的开口端由盖板（25）封闭，盖板（25）的轮廓与机翼下表面轮廓相匹配，盖板通过与螺栓锁定接合的螺母（78）固定到壳体。 一对夹子（37）被容纳在壳体内，每个夹子具有延伸穿过壳体中的狭槽（42）的接头表面（40），夹子通过锁紧螺母和螺栓固定。 盖板和壳体封闭端部是沉没的（17,59,27），以提供平滑的机翼表面。

公开(公告)号：WO1994012775A1

公开(公告)日：1994-06-09

申请号：PCT/US1993011350

申请日：1993-11-22

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  STAHL, Matthew ,  HASTINGS, William, J. ,  KANE, Daniel, E. ,  MURDOCK, James, R. ,  DIERBERGER, James, A.

IPC: F01D11/08

CPC classification number: F01D11/122 ,  F05D2260/201 ,  F05D2260/202

Abstract: An outer air seal assembly (44) cooled by a combination of impingement cooling and film cooling is disclosed. Various construction details are developed which provide impingement of cooling fluid on a radially outer side of an outer air seal assembly (44) and ejection of a film of cooling fluid over a radially inner surface (52) of the outer air seal assembly (44). In a particular embodiment, an outer air seal assembly (44) includes a substrate (54), an apertured cover (56) disposed outward of the substrate (54), and a layer of abradable material (58) extending radially inward of the substrate (54) and defining a flow surface (52). Cooling fluid is directed through the apertures (72), into a cavity (66), and impinges upon the outer surface of the substrate (54). A plurality of film cooling holes (76) extend through the substrate (54) and abradable layer (58) and provide fluid communication between the cavity (66) and flowpath (14). The cooling holes (76) are oriented to eject cooling in a film over the flow surface (52). In another embodiment, the cavity (66) includes a longitudinally extending chamber (112) disposed in an enlarged portion (108) of the air seal (46) to enhance cooling thereof and reduce stresses therewithin.

Abstract translation: 公开了通过冲击冷却和薄膜冷却的组合冷却的外部空气密封组件（44）。 开发了各种结构细节，其提供了在外部空气密封组件（44）的径向外侧上的冷却流体的冲击和在外部空气密封组件（44）的径向内表面（52）上的冷却流体膜的喷射， 。 在特定实施例中，外部空气密封组件（44）包括衬底（54），设置在衬底（54）外侧的有孔盖（56）和沿着衬底的径向向内延伸的可磨损材料层 （54）并限定流动表面（52）。 冷却流体被引导通过孔（72）进入空腔（66），并且撞击在基底（54）的外表面上。 多个膜冷却孔（76）延伸穿过基底（54）和可磨损层（58），并提供空腔（66）和流路（14）之间的流体连通。 冷却孔（76）被定向成喷射在流动表面（52）上的膜中的冷却。 在另一个实施例中，空腔（66）包括设置在空气密封件（46）的扩大部分（108）中的纵向延伸腔室（112），以增强其冷却并降低其中的应力。

公开(公告)号：WO1994012774A1

公开(公告)日：1994-06-09

申请号：PCT/US1993011127

申请日：1993-11-12

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  CHLUS, Wieslaw, A. ,  HOUSTON, David, P.

IPC: F01D05/26

CPC classification number: F01D5/22 ,  Y10S416/50

Abstract: A rotor blade (44) having axially spaced gussets (72, 78) disposed between a root portion (66) and a platform (64) is disclosed. Various construction details are developed which provide a gusset providing both platform support and damper positioning means. In one particular embodiment, a rotor blade assembly (38) includes a plurality of circumferentially spaced rotor blades (44) having dampers (88) disposed between adjacent blades (44), wherein each blade (44) includes an axially spaced pair of gussets (78, 82) extending laterally from the rotor blade (44). The gussets (78, 82) extend from a root portion (66) of the rotor blade (44) to a platform (64) and provide radial support of the platform (64) during rotation of the rotor assembly (38). The gussets (78, 82) include a curved lateral edge which, during rotation of the rotor assembly (38), urges the damper (88) away from the root portion (66) of the blade (44).

Abstract translation: 公开了一种设置在根部（66）和平台（64）之间的具有轴向间隔的角撑板（72,78）的转子叶片（44）。 开发了各种构造细节，其提供提供平台支撑和阻尼器定位装置的角撑板。 在一个特定实施例中，转子叶片组件（38）包括多个周向间隔开的转子叶片（44），其具有设置在相邻叶片（44）之间的阻尼器（88），其中每个叶片（44）包括轴向间隔开的一对角撑板 78）从转子叶片（44）横向延伸。 在转子组件（38）旋转期间，角撑板（78,82）从转子叶片（44）的根部（66）延伸到平台（64）并且提供平台（64）的径向支撑。 角撑板（78,82）包括弯曲的侧边缘，其在转子组件（38）的旋转期间促使阻尼器（88）远离叶片（44）的根部（66）。

公开(公告)号：WO1994012773A1

公开(公告)日：1994-06-09

申请号：PCT/US1993010803

申请日：1993-11-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  CHLUS, Wieslaw, A. ,  GONSOR, Michael ,  HOUSTON, David, P. ,  KUDRA, Paul, D.

IPC: F01D05/26

CPC classification number: F01D5/22 ,  F01D11/006 ,  F05D2260/97 ,  Y10S416/50

Abstract: An integrated damper and windage cover (52) has a windage cover portion (56) cantilevered at the upstream end, free of contact with the blade platform (24, 32). The contact portion (54) is rigid and bears against the underside of the blade platform (24), spanning blade platform clearance (50).

Abstract translation: 集成的阻尼器和风挡盖（52）具有在上游端悬臂的防风罩部分（56），与叶片平台（24,32）无接触。 接触部分（54）是刚性的并且抵靠在叶片平台（24）的下侧，跨越叶片平台间隙（50）。

公开(公告)号：WO1994009424A1

公开(公告)日：1994-04-28

申请号：PCT/US1992008684

申请日：1992-10-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  DYER, Gerald, P.

IPC: G05D07/01

CPC classification number: G05D7/0126 ,  Y10T137/7737

Abstract: A pressure regulating flow control apparatus comprises a flow metering valve (10) for controllably discharging a fluid from a spring-biased throttling spool (30) thereof to a fluidic device at a regulated pressure and a pressure modulating valve (100) operatively associated with the throttling spool (30) of the flow metering valve (10) for modulating the fluid pressure in subchamber (18) of the metering valve (10) to alter the position of the throttling spool to adjust the regulated pressure in response to fluid temperature over a relatively large temperature range so as to compensate for the variation of fluid viscosity with fluid temperature.

Abstract translation: 压力调节流量控制装置包括流量计量阀（10），用于将流体从弹簧偏压节流阀芯（30）可控地排出到调节压力下的流体装置和与压力调节阀（100）可操作地相关联的压力调节阀 流量计量阀（10）的节流阀芯（30），用于调节计量阀（10）的子室（18）中的流体压力，以改变节流阀芯的位置，以响应于流体温度 相对较大的温度范围，以补偿流体粘度随流体温度的变化。

公开(公告)号：WO1994004856A1

公开(公告)日：1994-03-03

申请号：PCT/US1993006503

申请日：1993-07-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  OLSON, Eric, G.

IPC: F16J15/34

CPC classification number: F16J15/3404

Abstract: A sealed assembly (46) for a rotary machine (10) is disclosed. Various construction details are developed which block the migration of oil from a compartment such as a bearing compartment (22). In one detailed embodiment, an annular clearance gap (G) is provided with an outwardly tapered surface (98; 118; 98, 118) to energize a boundary layer or to block lubricating fluid from migrating from the bearing compartment.

Abstract translation: 公开了一种用于旋转机器（10）的密封组件（46）。 开发了各种构造细节，其阻止油从诸如轴承室（22）的隔室的迁移。 在一个详细的实施例中，环形间隙（G）设置有向外锥形的表面（98; 118; 98,118），以激励边界层或阻止润滑流体从轴承隔室迁移。

公开(公告)号：WO1994002357A1

公开(公告)日：1994-02-03

申请号：PCT/US1993007031

申请日：1993-07-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： UNITED TECHNOLOGIES CORPORATION ,  FRADENBURGH, Evan, A. ,  MILLER, Gordon, Glenn

IPC: B64C27/54

CPC classification number: B64C27/46 ,  B64C11/003 ,  B64C27/54

Abstract: A drive system for varying the diameter of a variable diameter rotor has a gear assembly associated with a single coaxial shaft (13) lower end which includes a gear set for increasing the speed of rotation of the central shaft (13) relative to the rotor drive shaft (2) to change the diameter of the variable diameter blades. A pair of brakes are used, one (37) to slow the coaxial shaft relative to the drive shaft and another (25) to lock the rotor shaft (2) and coaxial shaft (13) together for corotation during constant diameter flight conditions. Utilizing a lower gear assembly reduces hub complexity and allows the variable diameter rotor drive system to be adapted to gimballed rotors which require shaft flexibility. Since only a single shaft extends through the rotor drive shaft, hub complexity is reduced.

Abstract translation: 用于改变可变直径转子的直径的驱动系统具有与单个同轴轴（13）下端相关联的齿轮组件，其包括用于增加中心轴（13）相对于转子驱动器（13）的旋转速度的齿轮组 轴（2）以改变可变直径叶片的直径。 使用一对制动器，一个（37）相对于驱动轴减慢同轴轴，另一个（25）将转子轴（2）和同轴轴（13）锁定在一起，以保持恒定直径的飞行状态。 利用下部齿轮组件减少轮毂的复杂性，并允许可变直径的转子驱动系统适应需要轴的灵活性的摇摆转子。 由于只有单个轴延伸穿过转子驱动轴，轮毂的复杂性降低。