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1. 发明申请

WO2010129960A1 PNEUMATIC BLOW-DOWN ACTUATOR 审中-公开
标题翻译：气动吹风致动器
公开(公告)号：WO2010129960A1
公开(公告)日：2010-11-11
申请号：PCT/US2010/034261
申请日：2010-05-10
申请人： SPECTRUM AERONAUTICAL, LLC
发明人： MASON, Garth, L.
IPC分类号： B64C25/18
CPC分类号： B64C25/18 , B64C25/22 , B64C25/30 , Y10T74/18592
摘要： An electromechanical linear actuator includes a pneumomechanical back-up system to ensure extension of retractable landing gear for landing an aircraft. Structurally, the linear actuator includes a stator forming a channel for receiving a ball screw. Further, the actuator includes a ball screw housing forming a chamber for receiving the ball screw. Specifically, the ball screw and the housing are in threaded engagement to translate rotation of the ball screw into axial extension of the housing. To power electromechanical extension of the actuator, the ball screw is selectively engaged to a motor with a gear train. Importantly, fluid communication between the ball screw housing and a pressurized fluid is selectively provided by a valve. If electromechanical extension of the actuator fails, the gear train is disconnected from the ball screw and the pressurized fluid is introduced into the chamber to drive pneumomechanical extension.
摘要翻译：机电线性致动器包括气动机械备用系统，以确保用于着陆飞机的可伸缩起落架的延伸。在结构上，线性致动器包括形成用于接收滚珠丝杠的通道的定子。此外，致动器包括形成用于接收滚珠丝杠的腔室的滚珠丝杠壳体。具体地，滚珠丝杠和壳体是螺纹接合的，以将滚珠丝杠的旋转转移到壳体的轴向延伸。为了对致动器的机电延伸进行动力，滚珠丝杠选择性地与具有齿轮系的马达接合。重要的是，滚珠丝杠壳体和加压流体之间的流体连通由阀选择性地提供。如果执行机构的机电延伸器故障，齿轮系与滚珠丝杠断开，加压流体被引入腔室，以驱动气力机械延伸。

2. 发明申请

WO2009036285A1 REINFORCED COMPOSITE PANEL 审中-公开
标题翻译：增强复合面板
公开(公告)号：WO2009036285A1
公开(公告)日：2009-03-19
申请号：PCT/US2008/076184
申请日：2008-09-12
申请人： SPECTRUM AERONAUTICAL, LLC
发明人： ASHTON, Larry, J. , ALLMAN, Michael, G. , WHITE, Troy, L. , SIMPSON, Craig, B. , TA'ALA, Benko, S.
IPC分类号： E04C2/34
CPC分类号： E04C2/326 , E04C2/20
摘要： A reinforced panel, made of a composite material, includes a single base layer. A first plurality of mutually parallel ridges is affixed to the surface of the base layer. A second plurality of mutually parallel ridges is also affixed to the surface of the base layer, but oriented transverse to the first plurality. Structurally, the ridges and the base layer are co-cured to create an integral, continuous structure that provides stiffness and rigidity to the panel.
摘要翻译：由复合材料制成的加强板包括单个基层。第一多个相互平行的脊固定到基层的表面。第二多个相互平行的脊也固定在基层的表面上，但是横向于第一多个脊定向。在结构上，脊和基层被共同固化以产生整体的，连续的结构，其为面板提供刚度和刚度。

3. 发明申请

WO2008097383A2 UNITARY ONE-PIECE WINDSHIELD 审中-公开
标题翻译：单位一体式WINDSHIELD
公开(公告)号：WO2008097383A2
公开(公告)日：2008-08-14
申请号：PCT/US2007/081288
申请日：2007-10-12
申请人： SPECTRUM AERONAUTICAL, LLC , BLUE, Linden, S. , COONEY, Daniel, E.
发明人： BLUE, Linden, S. , COONEY, Daniel, E.
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A windshield for a pressurized aircraft includes a single transparent unit that functions structurally to allow pressurization of the aircraft and to support the aircraft's fuselage in response to external loads. The windshield also functions operationally to provide the pilot with an unobstructed field of vision through an extended arc of more than two hundred degrees. For its manufacture, layers of the transparent unit are respectively bent along a straight center line to establish two curved portions that are symmetrical relative to a common plane. The layers are then laminated.
摘要翻译：用于加压飞机的挡风玻璃包括单个透明单元，其在结构上起作用以允许飞行器加压并且响应于外部载荷来支持飞行器的机身。挡风玻璃还通过延伸的弧度超过两百度，在飞行员的作用下为飞行员提供无障碍的视野。为了制造，透明单元的层分别沿直线中心线弯曲以形成相对于公共平面对称的两个弯曲部分。然后层压层。

4. 发明申请

WO2009036291A1 METHOD FOR MANUFACTURING A REINFORCED PANEL OF COMPOSITE MATERIAL 审中-公开
标题翻译：制造复合材料增强板的方法
公开(公告)号：WO2009036291A1
公开(公告)日：2009-03-19
申请号：PCT/US2008/076198
申请日：2008-09-12
申请人： SPECTRUM AERONAUTICAL, LLC
发明人： ASHTON, Larry, J. , ALLMAN, Michael, G. , WHITE, Troy, L. , TA'ALA, Benko, S.
IPC分类号： B32B3/12
CPC分类号： B29C70/023 , B29C35/02 , B29C65/02 , B29C66/1122 , B29C66/438 , B29C66/63 , B29C66/636 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/7394 , B29C66/91411 , B29C66/91431 , B29C66/919 , B29C66/9241 , B29C66/929 , B29C66/949 , B29C70/342 , B29D99/0014 , B29K2063/00 , B29K2105/06 , B29K2307/00 , B29K2307/04 , B29K2077/00
摘要： A method for manufacturing rigid panels made of a composite material requires a caul sheet having a smooth surface that is formed with a plurality of grooves. A first layer of the composite material is laid on the caul sheet, and is cut to create flaps that extend into the respective grooves. Strips of composite material are then placed along the edges of the groove to extend and overlap each other in the groove. Next, a unidirectional ply is placed along the length of the groove, and this combination is then covered with a second layer of the composite material. Together, the combination of the first and second layers, the strips and the unidirectional ply are co-cured to create a rigid panel with integral stiffening members.
摘要翻译：用于制造由复合材料制成的刚性板的方法需要具有形成有多个槽的光滑表面的密封片。复合材料的第一层被放置在覆盖片上，并且被切割以产生延伸到相应凹槽中的折片。然后沿着凹槽的边缘放置复合材料条，以在凹槽中彼此延伸和重叠。接下来，沿着槽的长度放置单向帘布层，然后用第二层复合材料覆盖该组合。一起，第一和第二层，条带和单向帘布层的组合被共同固化以产生具有整体加强构件的刚性面板。

5. 发明申请

WO2008048908A3 AIRCRAFT SEAT 审中-公开
公开(公告)号：WO2008048908A3
公开(公告)日：2008-04-24
申请号：PCT/US2007/081279
申请日：2007-10-12
申请人： SPECTRUM AERONAUTICAL, LLC
发明人： GARDINER, Richard, J. , GARDINER, Richard, J. , ISAACMAN, Ben , HARKNESS, Kip, Devon
IPC分类号： A47C1/00
摘要： An aircraft seat includes a hollow seat structure that is made from a single layer of a reinforced composite material. In a unitary construction, the seat structure has a seat portion and a backrest, and it is formed with a convex surface that is located under the seat portion. A base frame formed with a concave surface is attached to the aircraft fuselage, and it is oriented for juxtaposition with the convex surface of the seat structure to provide for a relative sliding motion of the seat structure on the base frame. A connector is also provided for selectively holding the convex surface of the seat structure in a fixed orientation relative to the concave surface of the base frame.

6. 发明申请

WO2008048908A2 AIRCRAFT SEAT 审中-公开
标题翻译：飞机座椅
公开(公告)号：WO2008048908A2
公开(公告)日：2008-04-24
申请号：PCT/US2007081279
申请日：2007-10-12
申请人： SPECTRUM AERONAUTICAL LLC
发明人： GARDINER RICHARD J , ISAACMAN BEN , HARKNESS KIP DEVON
IPC分类号： A47C1/00
CPC分类号： B64D11/064 , B64D11/06 , B64D11/0649 , B64D11/0696
摘要： An aircraft seat includes a hollow seat structure that is made from a single layer of a reinforced composite material. In a unitary construction, the seat structure has a seat portion and a backrest, and it is formed with a convex surface that is located under the seat portion. A base frame formed with a concave surface is attached to the aircraft fuselage, and it is oriented for juxtaposition with the convex surface of the seat structure to provide for a relative sliding motion of the seat structure on the base frame. A connector is also provided for selectively holding the convex surface of the seat structure in a fixed orientation relative to the concave surface of the base frame.
摘要翻译：飞机座椅包括由单层增强复合材料制成的空心座椅结构。在一体的结构中，座椅结构具有座椅部分和靠背，并且其形成有位于座椅部分下方的凸形表面。形成有凹面的底架被安装在飞行器机身上，并且它被定位成与座椅结构的凸形表面并置以提供座椅结构在基架上的相对滑动运动。还提供连接器，用于相对于基架的凹面有选择地将座椅结构的凸面保持在固定的方位。

7. 发明申请

WO2009036296A1 FLYAWAY KABOBS 审中-公开
公开(公告)号：WO2009036296A1
公开(公告)日：2009-03-19
申请号：PCT/US2008/076207
申请日：2008-09-12
申请人： SPECTRUM AERONAUTICAL, LLC
发明人： ASHTON, Larry, J. , ALLMAN, Michael, G. , WHITE, Troy, L. , STARK, Danny, L.
IPC分类号： B64C3/24
CPC分类号： B64C3/24 , A63B2209/02 , B64C3/185 , B64C3/187 , Y02T50/43
摘要： An aircraft wing made of a composite material, and its method of manufacture, require a plurality of kabobs (i.e. substantially rectangular shaped hollow tubes having an open end and a closed end). Of these kabobs, several are aligned end-to-end, to create a section. Several sections are then positioned side-by-side and covered by a layer of composite material to define an aerodynamic surface for the wing. The juxtaposed sections also establish spar webs for the wing, and the closed ends of the juxtaposed sections establish transverse ribs for the wing. Thus, the kabobs form the main load-bearing member of the wing. The sections of composite material are co-cured with the composite material of the aerodynamic surface.
摘要翻译：由复合材料制成的飞机机翼及其制造方法需要多个卡布巴（即具有开口端和封闭端的大致矩形的中空管）。在这些kabobs中，几个对齐端到端，以创建一个部分。然后将几个部分并排设置并被一层复合材料覆盖以限定机翼的空气动力学表面。并列部分还建立翼的翼梁网，并列的部分的封闭端设置用于机翼的横向肋。因此，卡布尔形成机翼的主承重构件。复合材料的截面与空气动力学表面的复合材料共同固化。

8. 发明申请

WO2008097383A3 UNITARY ONE-PIECE WINDSHIELD 审中-公开
标题翻译：一次性单件风挡
公开(公告)号：WO2008097383A3
公开(公告)日：2008-11-13
申请号：PCT/US2007081288
申请日：2007-10-12
申请人： SPECTRUM AERONAUTICAL LLC , BLUE LINDEN S , COONEY DANIEL E
发明人： BLUE LINDEN S , COONEY DANIEL E
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A windshield for a pressurized aircraft includes a single transparent unit that functions structurally to allow pressurization of the aircraft and to support the aircraft's fuselage in response to external loads. The windshield also functions operationally to provide the pilot with an unobstructed field of vision through an extended arc of more than two hundred degrees. For its manufacture, layers of the transparent unit are respectively bent along a straight center line to establish two curved portions that are symmetrical relative to a common plane. The layers are then laminated.
摘要翻译：用于加压式飞机的挡风玻璃包括单个透明单元，其在结构上起作用以允许飞机加压并且响应于外部负载来支撑飞机的机身。挡风玻璃的功能还在于通过超过二百度的延伸弧向飞行员提供畅通无阻的视野。为了制造，透明单元的各层分别沿着一条平直的中心线弯曲，以建立相对于一个共同平面对称的两个弯曲部分。然后将这些层层压。

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