公开(公告)号：US09238511B2

公开(公告)日：2016-01-19

申请号：US14196570

申请日：2014-03-04

申请人： MRA Systems, Inc.

发明人： Allen Madsen Woolley ,  Brian Kelby Clegg ,  Michael Scott Just ,  Rameshchandra Dahyabhai Patel

IPC分类号： B64D27/26 ,  B64D29/02

CPC分类号： B64D27/26 ,  B64D27/12 ,  B64D29/02 ,  B64D2027/264 ,  B64D2027/268 ,  Y02T50/44

摘要： A pylon structure for mounting an aircraft engine to a wing. The pylon structure comprises a torque box having a wing mount on the aft portion, a first engine mount on the fore portion and second engine mount on the aft portion.

摘要翻译： 用于将飞机发动机安装在机翼上的挂架结构。 该塔架结构包括：扭矩箱，其具有在后部上的机翼安装件，在前部上的第一发动机支架和在后部分上的第二发动机支架。

公开(公告)号：US08668864B2

公开(公告)日：2014-03-11

申请号：US13118885

申请日：2011-05-31

申请人： Mahendra Maheshwari ,  Xiaomei Fang

发明人： Mahendra Maheshwari ,  Xiaomei Fang

IPC分类号： B29C70/02

CPC分类号： B32B5/28 ,  C08J5/24 ,  F01D5/282 ,  Y02T50/672 ,  Y02T50/673

摘要： Processes for fabricating polymer composite materials that contain a polymer matrix, reinforcement fabrics, and particles of a filler material. The processes include spraying the particles of the filler material on at least two articles that each comprise at least one of the reinforcement fabrics to form particle-laden articles. The particle-laden articles are stacked to form a stacked structure, and a resin present within the stacked structure is then cured to form a laminate polymer composite material. The process can be employed in the fabrication of at least a portion of an aircraft engine nacelle, for example, the inlet lip of a fan nacelle.

摘要翻译： 用于制造含有聚合物基质，增强织物和填充材料颗粒的聚合物复合材料的方法。 这些方法包括将填料材料的颗粒喷洒在至少两个制品上，每个制品包括至少一个增强织物以形成载有颗粒的制品。 将载有颗粒的物品层叠以形成堆叠结构，然后将存在于堆叠结构内的树脂固化以形成层压聚合物复合材料。 该方法可以用于制造飞机发动机机舱的至少一部分，例如风扇机舱的入口唇缘。

公开(公告)号：US20140014776A1

公开(公告)日：2014-01-16

申请号：US13685861

申请日：2012-11-27

申请人： MRA SYSTEMS INC. ,  KELLY AEROSPACE THERMAL SYSTEMS LLC

发明人： David Patrick Calder ,  Julian Alexander Opificius ,  Mark Fairbert ,  Erik Thomas Pederson ,  David Cenit Flosdorf

IPC分类号： B64D15/12

CPC分类号： B64D15/12 ,  B64D2033/0233

摘要： A system and method thereof is provided for electrically heating a component. The system includes at least one heating element adapted to be adhesively bonded to a surface on the component and means for controlling flow and duration of an electrical current to the heating element from a power supply. The controlling means comprises a first heating cycle for curing an adhesive to bond the heating element to the surface and has a second heating cycle for providing ice protection to the surface.

摘要翻译： 提供了一种用于电加热部件的系统及其方法。 该系统包括至少一个加热元件，该加热元件适于粘合地结合到元件上的表面，以及用于控制从电源到加热元件的电流的流动和持续时间的装置。 控制装置包括用于固化粘合剂以将加热元件结合到表面的第一加热循环，并具有用于向表面提供冰保护的第二加热循环。

公开(公告)号：US20110297325A1

公开(公告)日：2011-12-08

申请号：US13210483

申请日：2011-08-16

申请人： Mahendra Maheshwari ,  James Joseph Velten

发明人： Mahendra Maheshwari ,  James Joseph Velten

IPC分类号： B29C70/00 ,  B32B38/00

CPC分类号： B29C70/545 ,  B29C43/027 ,  B29C43/10 ,  B29C2043/3655 ,  B29K2995/0002 ,  B29L2031/3076 ,  B29L2031/737 ,  Y10S264/57 ,  Y10S264/70 ,  Y10S264/78 ,  Y10S425/037 ,  Y10T156/1028 ,  Y10T156/1056 ,  Y10T156/1057 ,  Y10T156/1062 ,  Y10T156/1304

摘要： A process and apparatus for producing perforated composite structures, such as acoustic skins suitable for aircraft engine nacelle and duct components. The process includes placing a mat member, a non-impregnated fabric member, and a resin film on a tool surface so that pins disposed on the mat member project through the fabric member and resin film to define holes therein. The fabric member is between the mat member and resin film, and the fabric member and resin film define a stack that conforms to the mat member and tool surface. A caul member is then placed on the stack so that apertures in the caul member are penetrated by the pins. The stack is heated to melt the resin film and cause molten resin to infuse the fabric member and yield a resin-infused fabric stack, after which the molten resin within the resin-infused fabric stack is at least partially cured.

摘要翻译： 用于生产穿孔复合结构的方法和设备，例如适用于飞机发动机机舱和管道部件的声学皮肤。 该方法包括将垫子，非浸渍的织物构件和树脂膜放置在工具表面上，使得设置在垫构件上的销突出穿过织物构件和树脂膜以在其中限定孔。 织物构件在垫材和树脂膜之间，织物和树脂膜限定了与垫材和工具表面一致的叠层。 然后将一个止动件放置在堆叠上，使得止动件中的孔被销钉穿透。 将该叠层加热熔化树脂膜，使熔融树脂注入织物，并产生树脂输入的织物叠层，此后树脂注入的织物叠层内的熔融树脂至少部分固化。

公开(公告)号：US09309001B2

公开(公告)日：2016-04-12

申请号：US14812610

申请日：2015-07-29

申请人： MRA Systems Inc. ,  Kelly Aerospace Thermal Systems, LLC

发明人： David Patrick Calder ,  Julian Alexander Opificius ,  Erik Thomas Pederson ,  David Cenit Flosdorf

IPC分类号： B64D15/12 ,  B64D15/14

CPC分类号： B64D15/14 ,  B64D15/12 ,  Y10T156/10 ,  Y10T156/1052

摘要： A system and method for ice protection of a component, wherein the system is adapted to be adhesively bonded to a surface of the component. The system includes a heating element layer, at least one thermally conductive adhesive layer that adhesively bonds a first side of the heating element layer to the component, an insulation layer, at least one thermally insulating adhesive layer that adhesively bonds a second side of the heating element to the insulation layer, an electrical bus bar adapted to provide a connection between a power supply and the heating element layer, and at least one temperature sensor.

公开(公告)号：US20150344142A1

公开(公告)日：2015-12-03

申请号：US14293589

申请日：2014-06-02

申请人： MRA Systems, Inc.

发明人： Andrew Michael Roach ,  Graham Frank Howarth

IPC分类号： B64D33/02 ,  E04B1/82

CPC分类号： B64D33/02 ,  B64D2033/0206 ,  E04B1/82 ,  F02C7/045 ,  F05D2250/283 ,  F05D2260/96 ,  G10K11/172

摘要： An aircraft engine assembly comprising a nacelle configured to surround the aircraft engine having an inlet open to ambient air and an annular acoustic panel provided within the nacelle. Sound emitted from the aircraft engine is attenuated by the annular acoustic panel. The annular acoustic panel comprises an open framework, made from a first material, forming a plurality of cells.

摘要翻译： 一种飞机发动机组件，其包括构造成围绕具有与周围空气相通的入口的飞机发动机的机舱和设置在机舱内的环形隔音板。 飞机发动机发出的声音被环形隔音板衰减。 环形声学板包括由第一材料制成的开放框架，形成多个单元。

公开(公告)号：US09188026B2

公开(公告)日：2015-11-17

申请号：US13524127

申请日：2012-06-15

申请人： David P. Calder ,  Graham F. Howarth

发明人： David P. Calder ,  Graham F. Howarth

IPC分类号： B64D29/06 ,  F01D25/28 ,  F02C7/20

CPC分类号： F01D25/28 ,  B64D29/06 ,  F02C7/20 ,  F05D2230/72

摘要： A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end. The fan cowl is coupled to an engine mounting pylon via a slider-type mounting system that includes at least one slider track assembly defining at least one slot therein. The at least one slot is configured to receive at least one fan cowl slider fitting.

摘要翻译： 用于容纳发动机的机舱包括尺寸适于覆盖发动机的至少第一轴向部分的风扇罩。 发动机包括入口端，排气端以及从入口端经过排气端延伸穿过发动机的轴线。 风扇罩通过滑块式安装系统联接到发动机安装塔架，滑块式安装系统包括至少一个在其中限定至少一个狭槽的滑块轨道组件。 所述至少一个狭槽被配置为容纳至少一个风扇整流罩滑块配件。

公开(公告)号：US10174675B2

公开(公告)日：2019-01-08

申请号：US14984767

申请日：2015-12-30

申请人： General Electric Company ,  MRA SYSTEMS, INC.

发明人： Michael Moses Martinez ,  Rudramuni Kariveerappa Majjigi ,  Steven Thomas Davies ,  Egbert Geertsema

IPC分类号： F02C7/045 ,  B64D33/02 ,  F04D29/66 ,  G10K11/168 ,  G10K11/172

摘要： A single degree of freedom (SDOF) acoustic liner includes a porous face sheet, a substantially imperforate back sheet generally parallel to and opposing said porous face sheet and defining a thickness therebetween, and an acoustic core layer of contiguous adjacent resonant cavities disposed between the porous face sheet and the imperforate back sheet. The acoustic core layer includes a first resonant cell having a first internal volume therein and a second resonant cell having a second internal volume therein different than the first internal volume. A cell partition wall extends between the porous face sheet and the imperforate back sheet, and separates and seals the first resonant cell from the second resonant cell. In a thickness direction, and perpendicular to a plane generally parallel with the porous face sheet and the substantially imperforate back sheet, the first internal volume overlaps the second internal volume over the cell partition wall.

公开(公告)号：US09835112B2

公开(公告)日：2017-12-05

申请号：US14176200

申请日：2014-02-10

申请人： MRA Systems, Inc.

发明人： David Patrick Calder ,  Graham Frank Howarth

IPC分类号： F02K1/72 ,  B33Y80/00

CPC分类号： F02K1/72 ,  B33Y80/00 ,  F05D2230/31 ,  F05D2300/603 ,  Y02T50/672

摘要： A thrust reverser cascade having a frame and a body. The body comprises multiple layers formed by an additive manufacturing process where at least one of the layers is coupled to the frame.

公开(公告)号：US09404507B2

公开(公告)日：2016-08-02

申请号：US13862941

申请日：2013-04-15

申请人： MRA Systems, Inc.

发明人： Antony Brett Scarr ,  Thomas Joseph Weir ,  Allen Madsen Woolley ,  Carol Marie Janzon

IPC分类号： B64D27/00 ,  F04D29/40 ,  B64D29/06

CPC分类号： F04D29/40 ,  B64D29/06

摘要： An inner cowl structure for circumscribing at least a portion of a jet engine extending from an aircraft includes an apron configured to mount directly to the engine independent of the pylon and overly an upper portion of the jet engine, and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron.

摘要翻译： 用于围绕从飞行器延伸的喷气发动机的至少一部分的内部罩壳结构包括被构造成直接安装在发动机上而不依赖于塔架并且越过喷气发动机的上部的挡板，以及构造成围绕 喷气发动机的一部分没有被围裙限制。