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1. 发明申请

WO2006036724A1 AIR CYCLE MACHINE FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM 审中-公开
标题翻译：用于航空环境控制系统的空气循环机
公开(公告)号：WO2006036724A1
公开(公告)日：2006-04-06
申请号：PCT/US2005/033924
申请日：2005-09-22
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： MCAULIFFE, Christopher , MERRITT, Brent, J. , BEERS, Craig, M.
IPC分类号： B64D13/06 , F25B11/04
CPC分类号： F25B9/004 , B64D13/06 , B64D2013/0614 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： An ECS system provides an ACM which locates the compressor (20) upon a common shaft (84) between a first turbine (22) and a second turbine (24). Each RAF is located remote from the ACM such that the turbines (22, 24) are located outboard on each end of the ACM to provide the highest efficiency possible with each turbine using a straight axial outlet diffuser. As the compressor (20) is located between the turbines (22, 24) the bypass circuits from the turbines are less circuitous and more efficient. Integral valve ports formed into the ACM housing portions results in a weight reduced design due to increase bypass efficiencies and simplified installations.
摘要翻译： ECS系统提供了将压缩机（20）定位在第一涡轮机（22）和第二涡轮机（24）之间的公共轴（84）上的ACM。每个RAF位于远离ACM的位置，使得涡轮机（22,24）位于ACM的每端的外侧，以使用直的轴向出口扩散器可以为每个涡轮机提供最高的效率。当压缩机（20）位于涡轮机（22,24）之间时，来自涡轮机的旁路回路较不迂回且更有效率。由于增加了旁路效率和简化的安装，形成在ACM壳体部分中的积分阀口导致重量减少的设计。

2. 发明申请

WO2005002025A1 ELECTRIC STARTER MOTOR WITH INTEGRAL CLUTCH 审中-公开
标题翻译：带起动离合器的电动起动马达
公开(公告)号：WO2005002025A1
公开(公告)日：2005-01-06
申请号：PCT/US2003/038700
申请日：2003-12-05
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： GUSTAFSON, James, R.
IPC分类号： H02K7/108
CPC分类号： F02C7/275 , F02C7/32 , H02K5/1735 , H02K7/108 , H02K7/116 , H02K7/14
摘要： A gas turbine engine system (10) includes an electric starter motor (16) which utilizes a partially hollow or cupped shaped rotor (36). Space is provided inside the rotor to fit the required clutch (18), bearing (44a, 44b), and drive shaft (28). A short package is provided due to the telescoped architecture while retaining the maximum length for electromagnetics.
摘要翻译：燃气涡轮发动机系统（10）包括利用部分中空或杯状转子（36）的电动起动电动机（16）。在转子内设置空间，以装配所需的离合器（18），轴承（44a，44b）和驱动轴（28）。由于可伸缩的结构，提供了一个短的封装，同时保留了电磁学的最大长度。

3. 发明申请

WO2004042910A2 ELECTRIC MOTOR CONTROL SYSTEM INCLUDING POSITION DETERMINATION AND ERROR CORRECTION 审中-公开
标题翻译：电动机控制系统包括位置确定和误差校正
公开(公告)号：WO2004042910A2
公开(公告)日：2004-05-21
申请号：PCT/US2003/035079
申请日：2003-11-04
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： GAMES, John, E. , SIMMONS, Howard
IPC分类号： H02P7/62
CPC分类号： H02P6/18
摘要： A system for controlling an electric motor includes a controller and a position indicator that provides position information regarding at least one motor component to the controller. The controller utilizes phase relationships indicative of the position information to determine the actual position of the component of interest. The phase information in one example is derived from the output of a resolver that provides two output signals corresponding to sin (θ) and cos (θ), where θ is the angular position. Utilizing the phase relationship simplifies the task of determining accurate position information that is useful to modify motor control signals to compensate for latency when making position determinations, velocity calculations or both. The inventive system makes it possible to use less expensive electronics to arrive at more reliable results.
摘要翻译：用于控制电动机的系统包括控制器和位置指示器，该位置指示器将关于至少一个电动机部件的位置信息提供给控制器。控制器利用指示位置信息的相位关系来确定感兴趣组分的实际位置。在一个例子中的相位信息是从提供对应于sin（θ）和cos（θ）的两个输出信号的旋转变压器的输出导出的，其中θ是角度位置。利用相位关系简化了确定准确位置信息的任务，该位置信息有助于修改电机控制信号，以便在进行位置确定，速度计算或两者时补偿延迟。本发明的系统使得可以使用更便宜的电子设备来获得更可靠的结果。

4. 发明申请

WO2006036570A2 BUMP FOIL HYDRODYNAMIC THRUST BEARING 审中-公开
标题翻译： BUMP FOIL HYDRODYNAMIC THRUST轴承
公开(公告)号：WO2006036570A2
公开(公告)日：2006-04-06
申请号：PCT/US2005/032929
申请日：2005-09-15
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： STRUZIAK, Ronald , MCAULIFFE, Christopher , MERRITT, Brent , ROSEN, Seth
IPC分类号： F16C17/04 , F16C27/02
CPC分类号： F16C17/042 , F16C27/08 , F16C2300/02
摘要： A thrust bearing for a rotary machine includes first, second and third layers. The second layer includes a corrugated foil arranged between the first and third layers. The corrugated foil includes a wall having peaks engaging the first layer and valleys engaging the third layer. A depression is arranged in the wall between first and second peaks. The depression is spaced from the first and third layers. The first layer includes multiple arcuate top foils that are arranged adjacent to a thrust runner of a rotatable shaft. A corresponding number of arcuate corrugated foils may be used to support the top foils. The third layer, which is provided by an annular main plate, includes multiple arcuate spacers arranged circumferentially on the main plate. The spacers are generally aligned with a trailing edge of the top foils. The depressions decrease the stiffness of the bump foils. The spacers direct the axial load through the thrust bearing in a desired manner.
摘要翻译：用于旋转机器的推力轴承包括第一层，第二层和第三层。第二层包括布置在第一层和第三层之间的波纹箔。波纹箔包括具有接合第一层的峰和与第三层接合的谷的壁。在第一和第二峰之间的壁中布置凹陷。凹陷与第一和第三层间隔开。第一层包括与旋转轴的推力滑轮相邻布置的多个弓形顶部箔。可以使用相应数量的弧形波纹箔来支撑顶部箔。由环形主板提供的第三层包括在主板周向布置的多个弧形间隔件。间隔件通常与顶部箔片的后缘对准。凹陷降低凸块箔的刚度。间隔件以期望的方式将轴向载荷引导通过推力轴承。

5. 发明申请

WO2006019771A1 PROJECTILE RESISTANT ARMOR 审中-公开
标题翻译：防弹装甲
公开(公告)号：WO2006019771A1
公开(公告)日：2006-02-23
申请号：PCT/US2005/024775
申请日：2005-07-13
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： DEAN, W., Clark , HAWES, Kevin, G. , WICHOWSKI, Robert , PHO, Thinh
IPC分类号： F41H1/02
CPC分类号： F41H1/02
摘要： A body armor assembly (30) includes a plurality of rigid tiles that are supported in a manner to provide movement and flexibility while still providing the protection of rigid armor. In a disclosed example, a tile holder maintains a plurality of tiles in a selected alignment. The tile holder maintains a minimum overlap dimension between adjacent tiles. Some of the tiles are maintained by the tile holder in a manner that allows for the overlap dimension to increase beyond the minimum overlap dimension. In a disclosed example, at least two rigid layers have at least one ballistic material layer (170) between them to provide a rigid armor material composition.
摘要翻译：身体装甲组件（30）包括多个刚性瓦片，其以提供运动和灵活性的方式被支撑，同时仍然提供对刚性护甲的保护。在公开的示例中，瓦片保持器以选定的对准方式保持多个瓦片。瓦片支架在相邻瓦片之间保持最小重叠尺寸。一些瓷砖由瓷砖保持器以允许重叠尺寸增加到超过最小重叠尺寸的方式保持。在公开的示例中，至少两个刚性层在它们之间具有至少一个防弹材料层（170），以提供刚性的装甲材料组合物。

6. 发明申请

WO2005030581A1 AIRCRAFT AIR CONDITIONING SYSTEM MIXER 审中-公开
标题翻译：飞机空调系统混合器
公开(公告)号：WO2005030581A1
公开(公告)日：2005-04-07
申请号：PCT/US2004/030941
申请日：2004-09-22
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： MCCOLGAN, Charles, J. , DESMARAIS, Donald, R., Jr. , HADDAD, Christopher, G. , ZYWIAK, Thomas, M.
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2013/0688 , F24F13/04
摘要： A mixer (16) includes a fresh air tube (40) defining a passage (42) having an inlet (44) receiving conditioned air (14) from an air conditioning pack (12). The fresh air tube (40) includes an outlet (46) providing mixed air (18) to a cabin (22) of the aircraft. An outer tube (48) at least partially surrounds the fresh air tube (40) and receives recirculated air (26) from the cabin (22). Multiple holes (54) in the fresh air tube (40) fluidly connect the outer tube (48) to the fresh air tube (40). The warm recirculation air (26) surrounds the portion of the fresh air tube (40) to heat it preventing ice from forming. The warm recirculation air (26) entering the fresh air tube (40) through the holes homogeneously mixes with the conditioned (14) air from the pack (12) to provide a uniform mixture of air within the fresh air tube (40), which further ensures the prevention of ice build up.
摘要翻译：混合器（16）包括限定通道（42）的新鲜空气管（40），所述通道具有从空调包装（12）接收调节空气（14）的入口（44）。新鲜空气管（40）包括向飞机的舱室（22）提供混合空气（18）的出口（46）。外管（48）至少部分地围绕新鲜空气管（40）并从舱（22）接收再循环空气（26）。新鲜空气管（40）中的多个孔（54）将外管（48）流体连接到新鲜空气管（40）。温暖的再循环空气（26）围绕新鲜空气管（40）的部分以加热，防止冰形成。通过孔进入新鲜空气管（40）的温暖的再循环空气（26）与来自包装（12）的调节空气（14）均匀地混合，以提供新鲜空气管（40）内的均匀的空气混合物，进一步确保防止积冰。

7. 发明申请

WO2005017399A1 ZERO CLEARANCE C-RING ASSSEMBLY 审中-公开
标题翻译：零间隙C型环组件
公开(公告)号：WO2005017399A1
公开(公告)日：2005-02-24
申请号：PCT/US2004/020414
申请日：2004-06-24
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： MAROCCHINI, Francis
IPC分类号： F16K27/04
CPC分类号： F16K27/041 , F16B3/04 , F16B21/18 , Y10T29/49948 , Y10T137/6007 , Y10T137/6065 , Y10T137/8663 , Y10T403/60
摘要： A support structure for a C-ring (34) includes a pair of circumferentially spaced holding members (37) on catch plates. The holding members may be moved individually into the C-ring after the C-ring is mounted within an outer housing (21). The two holding members thus provide support to an inner periphery of the C-ring. A locking plate (40) has support structure moved between circumferential ends of the housing members, thus providing effective support for the C-ring around its entire inner periphery. In this way, the two parts (21, 30) secured by the C-ring need not be moved relative to each other to insert the C-ring. The clearance or ability to move one of the two parts relative to the other which has been required in the past to mount a C-ring, is not necessary. This makes the inventive C-ring particularly useful for new applications, such as holding a porting sleeve within a valve housing.
摘要翻译：用于C形环（34）的支撑结构包括在捕获板上的一对周向间隔开的保持构件（37）。在将C形环安装在外壳体（21）中之后，保持构件可以分别移动到C形环中。因此，两个保持构件为C形环的内周提供支撑。锁定板（40）具有在壳体构件的周向端部之间移动的支撑结构，从而为C形环围绕其整个内周提供有效的支撑。以这种方式，由C形环固定的两个部分（21,30）不必相对于彼此移动以插入C形环。相对于过去需要安装C形环的两个部件之一的间隙或能力不是必需的。这使得本发明的C形环特别适用于新的应用，例如将移动套筒保持在阀壳体内。

8. 发明申请

WO2004106157A1 SNOW FILTER 审中-公开
标题翻译：雪花过滤器
公开(公告)号：WO2004106157A1
公开(公告)日：2004-12-09
申请号：PCT/US2004/015565
申请日：2004-05-18
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： TADDEY, Edmund, P. , SCHWEMMER, John, A. , HARRIS, Mark, L. , PREMONT, Robert, A.
IPC分类号： B64D13/00
CPC分类号： B01D46/2403 , B01D45/04 , B01D46/0021 , B01D2273/10 , B01D2275/201 , B64D13/00
摘要： A snow filter (10) for an airplane cabin air supply system is provided with a coned inlet screen (23) which allows some air to pass through and some snow to be retained. The coned configuration (22) diverts much of the air and snow toward a downstream conical retaining and collecting screen (26) positioned toward the outlet (30) of the snow filter. Snow is retained and collected at this point while air is able to pass through the screen (27). Downstream of the coned inlet screen and upstream of the conical retaining and collecting screen is an open air flow mid-portion (24) that enables tortuous flow of air as the snow is directed toward the conical retaining and collecting screen in an annular collection volume (160). The outlet of the snow filter is provided with a contact sleeve (32) that allows the snow filter to be fittingly received by a surrounding corresponding air duct. Thus a snow filter is provided that effectively separates snow from a flow of air while maintaining a clog-free path.
摘要翻译：用于飞机机舱空气供应系统的雪过滤器（10）设置有锥形入口筛网（23），其允许一些空气通过并且一些积雪被保留。锥形构造（22）将大部分空气和雪转向朝向雪过滤器的出口（30）定位的下游锥形保持和收集筛（26）。此时，空气能够通过屏幕（27）而保持并收集雪。锥形入口筛和锥形保持和收集筛的上游的下游是敞开的气流中间部分（24），当空气朝向锥形保持和收集筛网以环形收集容积（24） 160）。雪过滤器的出口设置有接触套筒（32），其允许积雪过滤器由周围的相应的空气管道适合地接收。因此，提供了一种有效地将雪与空气流隔开同时保持无阻塞路径的积雪过滤器。

9. 发明申请

WO2003080430A1 ACTUATION SYSTEM FOR A CONTROLLABLE PITCH PROPELLER 审中-公开
标题翻译：一种可控式搅拌螺旋桨的启动系统
公开(公告)号：WO2003080430A1
公开(公告)日：2003-10-02
申请号：PCT/US2003/005770
申请日：2003-02-25
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： AREL, David, V. , PERKINSON, Robert , DANIELSON, David
IPC分类号： B64C11/38
CPC分类号： B64C11/38 , B63H3/082
摘要： A propeller control system (20) provides for actuation through supply pressure only. A transfer bearing (38) thereby requires only a single land. The supply pressure is metered at a pitch change valve (40) within the rotating propeller shaft (28) downstream of the transfer bearing (38) to provide hydraulic pressure for actuation and control. A feather override mode is provided by energizing a feathering solenoid (44). The increased supply pressure changes the hydraulic force balance of the pitch change valve (40) to allow the increased supply pressure into a Coarse Pitch chamber and simultaneously allow fluid within the Fine Pitch chamber to flow to drain pressure. The flow to drain changes the hydraulic balance on the Pitch Change Actuator Piston (48) to drive a pitch link (50) attached to each propeller blade (32)and thereby change the pitch thereof towards coarse pitch.
摘要翻译：螺旋桨控制系统（20）仅通过供应压力提供致动。因此，转运轴承（38）仅需要单个的地面。供应压力在转动轴承（38）下游的旋转传动轴（28）内的变桨阀（40）处计量，以提供用于致动和控制的液压。通过对羽化螺线管（44）通电来提供羽毛超驰模式。增加的供应压力改变变桨阀（40）的液压力平衡，以允许增加的供应压力进入粗桨距腔室，并同时允许精细间距腔室内的流体流入排水压力。到排水的流量改变变桨促动器活塞（48）上的液压平衡，以驱动连接到每个螺旋桨叶片（32）的俯仰杆（50），从而将其俯仰改变为粗桨距。

10. 发明申请

WO2005030582A1 AIRCRAFT AIR CONDITIONING SYSTEM MIXER WITH CORRUGATIONS 审中-公开
标题翻译：具有校正功能的飞机空调系统混合器
公开(公告)号：WO2005030582A1
公开(公告)日：2005-04-07
申请号：PCT/US2004/030943
申请日：2004-09-22
申请人： HAMILTON SUNDSTRAND CORPORATION
发明人： MCCOLGAN, Charles, J. , DESMARAIS, Donald, R., Jr. , HADDAD, Christopher, G. , ZYWIAK, Thomas, M.
IPC分类号： B64D13/00
CPC分类号： F24F13/04 , B64D13/00 , B64D2013/0688
摘要： A mixer includes a fresh air tube (40) defining a passage (42) having an inlet (44) receiving conditioned air (14) from an air conditioning pack (12). The fresh air tube includes an outlet (46) providing mixed air (18) to a cabin of the aircraft. An outer tube (48) at least partially surrounds the fresh air tube (48) and receives recirculated air (26) from the cabin (22). A circumferential corrugation (51, 53, 54, 55) in the fresh tube (40) forms multiple lobes (54) in the fresh air tube (40) fluidly connect the outer tube (48) to the fresh air tube (40). The warm recirculation air (26) surrounds the portion (52) of the fresh air tube to heat it preventing ice from forming. The warm recirculation air (26) entering the fresh air tube (40) through the lobes (54) homogeneously mixes with the conditioned air (26) from the pack (12) to provide a uniform mixture of air within the fresh air tube (40), which further ensures the prevention of ice build up.
摘要翻译：混合器包括限定通道（42）的新鲜空气管（40），所述通道具有从空调包（12）接收调节空气（14）的入口（44）。新鲜空气管包括向飞机的舱室提供混合空气（18）的出口（46）。外管（48）至少部分地围绕新鲜空气管（48）并从舱（22）接收再循环空气（26）。新鲜管（40）中的圆周波纹（51,53,54,55）在新鲜空气管（40）中形成多个叶片（54），将外管（48）流体地连接到新鲜空气管（40）。温暖的再循环空气（26）围绕新鲜空气管的部分（52）以加热它，防止冰形成。通过叶片（54）进入新鲜空气管（40）的温暖的再循环空气（26）与来自包装（12）的调节空气（26）均匀地混合，以提供新鲜空气管（40）内的均匀的空气混合物），进一步确保防止积冰。

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