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21. 发明申请

WO2013122811A1 METHOD FOR ATTACHING A COMPONENT TO AN INTERNAL PORTION OF AN AIRCRAFT FUSELAGE 审中-公开
标题翻译：将组件连接到飞行器熔接件的内部部分的方法
公开(公告)号：WO2013122811A1
公开(公告)日：2013-08-22
申请号：PCT/US2013/025152
申请日：2013-02-07
申请人： LUCAS, Michael Eugene , GULFSTREAM AEROSPACE CORPORATION
发明人： LUCAS, Michael Eugene
IPC分类号： F16F13/24
CPC分类号： B64C1/403 , B23P19/10 , B23P2700/01 , F16B5/0692 , Y10T29/49826 , Y10T29/49895
摘要： A method for attaching a component to an internal portion of an aircraft fuselage is disclosed herein. The method includes, but is not limited to, mounting a vibration isolator assembly to the internal portion of the aircraft fuselage. The vibration isolator assembly has a protruding engagement portion having a flange. The method further includes, but is not limited to defining an opening in a vibration-deadening body. The method further includes, but is not limited to positioning the vibration-deadening body over the vibration isolator such that the protruding engagement portion is received within the opening. The method further includes, but is not limited to pressing a retaining member onto the protruding engagement portion such that the retaining member engages the flange.
摘要翻译：本文公开了将部件附接到飞行器机身的内部的方法。该方法包括但不限于将防振器组件安装到飞行器机身的内部。隔振器组件具有突出的接合部分，其具有凸缘。该方法还包括但不限于在防振体中限定开口。该方法还包括但不限于将防振体定位在隔振器上方，使得突出接合部分被容纳在开口内。该方法还包括但不限于将保持构件按压到突出接合部分上，使得保持构件接合凸缘。

22. 发明申请

WO2013116447A1 METHODS AND SYSTEMS FOR REQUESTING AND RETRIEVING AIRCRAFT DATA DURING FLIGHT OF AN AIRCRAFT 审中-公开
标题翻译：在飞机飞行期间要求和检索航空数据的方法和系统
公开(公告)号：WO2013116447A1
公开(公告)日：2013-08-08
申请号：PCT/US2013/024025
申请日：2013-01-31
申请人： O'DELL, Robert , GALLAGHER, Jim , CONZACHI, Keith , BRITT, Noëlle , KEREKESH, William , GEARY, Robert J. , GULFSTREAM AEROSPACE CORPORATION
发明人： O'DELL, Robert , GALLAGHER, Jim , CONZACHI, Keith , BRITT, Noëlle , KEREKESH, William , GEARY, Robert J.
IPC分类号： G06F7/70
CPC分类号： B64D45/00 , B64D2045/0085 , B64F5/60 , G08G5/0013 , H04B7/18508 , H04L67/125
摘要： The disclosed embodiments relate to methods and systems for requesting and retrieving aircraft data during flight of an aircraft. This aircraft data can be used to perform additional monitoring of aircraft sub-systems to detect an abnormal condition, and/or to identify one or more sources that are causing the abnormal condition. In one embodiment, aircraft data for one or more relevant parameters can be requested from the ground, measured on-board the aircraft, and stored in a data file that is then communicated back to personnel on the ground. The real-time aircraft data for one or more relevant parameters can then be analyzed to identify the one or more sources that are causing the abnormal condition.
摘要翻译：所公开的实施例涉及用于在飞行器飞行期间请求和检索飞行器数据的方法和系统。该飞行器数据可以用于对飞行器子系统执行附加监视以检测异常状况，和/或识别导致异常状况的一个或多个源。在一个实施例中，用于一个或多个相关参数的飞行器数据可以从飞机上的地面请求，并存储在数据文件中，然后将数据文件传回给地面上的人员。然后可以分析用于一个或多个相关参数的实时飞行器数据，以识别导致异常状况的一个或多个源。

23. 发明申请

WO2013116139A1 METHODS AND SYSTEMS FOR AIRCRAFT HEALTH AND TREND MONITORING 审中-公开
标题翻译：用于航空卫生和趋势监测的方法和系统
公开(公告)号：WO2013116139A1
公开(公告)日：2013-08-08
申请号：PCT/US2013/023396
申请日：2013-01-28
申请人： Gallagher, James , O'Dell, Robert , GULFSTREAM AEROSPACE CORPORATION
发明人： Gallagher, James , O'Dell, Robert
IPC分类号： G06F17/00
CPC分类号： B64F5/60 , B64D2045/0085
摘要： The disclosed embodiments relate to methods and systems for monitoring sub-systems of an aircraft to detect an abnormal condition, and for identifying one or more sources that are causing the abnormal condition. In response to detecting a trigger event during flight of the aircraft, data for a plurality of relevant parameters is measured and stored in a parameter file. The parameter file is transmitted from the aircraft over a wireless communication link, and relayed to a ground support network. At the ground support network, the measured data for the plurality of the relevant parameters is then used to identify the one or more sources that are causing the abnormal condition.
摘要翻译：所公开的实施例涉及用于监视飞机的子系统以检测异常状况以及用于识别导致异常状况的一个或多个源的方法和系统。响应于在飞行器飞行期间检测到触发事件，测量多个相关参数的数据并将其存储在参数文件中。参数文件通过无线通信链路从飞机发送，并转发到地面支持网络。在地面支持网络中，然后使用多个相关参数的测量数据来识别引起异常状况的一个或多个源。

24. 发明申请

WO2013109332A1 VENTILATION SYSTEM AND METHOD OF ASSEMBLY 审中-公开
标题翻译：通风系统和组装方法
公开(公告)号：WO2013109332A1
公开(公告)日：2013-07-25
申请号：PCT/US2012/063222
申请日：2012-11-02
申请人： GULFSTREAM AEROSPACE CORPORATION , DAVIS, Allen , LYNCH, Kristopher , WHITE, Adam , GROVENSTEIN, J.R.
发明人： DAVIS, Allen , LYNCH, Kristopher , WHITE, Adam , GROVENSTEIN, J.R.
IPC分类号： B64D13/08
CPC分类号： B64D13/00 , B60H1/3442 , B60H2001/3478 , B64D2013/003 , Y10T29/49826
摘要： A ventilation system for ventilating a passenger compartment of an aircraft is disclosed herein. The ventilation system includes, but is not limited to, a nozzle that is adapted to be mounted proximate an interior of the aircraft and that is configured to direct a stream of air into the passenger compartment. The ventilation system further includes a valve that is spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle. The ventilation system still further includes a conduit that fluidly couples the valve to the nozzle. The conduit is configured to convey the flow of air from the valve to the nozzle.
摘要翻译：本文公开了一种用于通风飞机乘客舱的通风系统。通风系统包括但不限于适于安装在飞行器内部附近并且被配置成将空气流引导到乘客舱中的喷嘴。通风系统还包括与喷嘴间隔开并定位在喷嘴上游的阀，阀构造成控制到喷嘴的空气流。通风系统还包括将阀流体地连接到喷嘴的导管。导管构造成将空气流从阀传送到喷嘴。

25. 发明申请

WO2007008185A2 METHOD AND ARRANGEMENT FOR AIRCRAFT FUEL DISPERSION 审中-公开
标题翻译：用于飞机燃料分配的方法和装置
公开(公告)号：WO2007008185A2
公开(公告)日：2007-01-18
申请号：PCT/US2004/043618
申请日：2004-12-29
申请人： GULFSTREAM AEROSPACE CORPORATION , WOZNIAK, Gregg , LAMB, David , LE, Dung
发明人： WOZNIAK, Gregg , LAMB, David , LE, Dung
IPC分类号： B64D37/00
CPC分类号： B64C17/10 , B64D37/00
摘要： Method and arrangement for dispersing fuel (62) within a fuel containment system (60) of an aircraft (30) including utilizing a fuel containment system on an aircraft that is located at least partially within a wing (34) of the aircraft and defines a reservoir portion (42) and a remote portion (44). Fuel is pumped during aircraft flight from the reservoir portion to the remote portion at a pumped rate (80), while simultaneously fuel that is contained in the remote portion of the fuel containment system is permitted to drain to the reservoir portion at a drainage rate (82). The drainage rate is less than the pumped rate. A fuel mass (64) is accumulated in the remote portion of the fuel containment system because of a difference between the pumped rate and the drainage rate and as a result, a counteractive moment (49) is induced in the aircraft that is opposingly directed to a lift moment (46) caused by wing-lift (45) during aircraft flight.
摘要翻译：将燃料（62）分散在飞行器（30）的燃料容纳系统（60）内的方法和装置，包括在至少部分位于飞机的翼（34）内的飞机上使用燃料密封系统，并且限定储存器部分（42）和远端部分（44）。在飞行器飞行期间以泵送速率（80）从储存部分向远程部分泵送燃料，同时燃料容纳系统的偏远部分中容纳的燃料以排水速率排放到储存器部分 82）。排水率小于抽水率。由于泵送速率和排水速率之间的差异，燃料箱（64）积聚在燃料容纳系统的远端部分，结果是在相对地指向的飞行器中引起了反作用力矩（49）在飞机飞行期间由机翼提升（45）引起的升力时刻（46）。

26. 发明申请

WO2023064679A1 PROPULSION SYSTEM FOR AN AIRCRAFT 审中-公开
公开(公告)号：WO2023064679A1
公开(公告)日：2023-04-20
申请号：PCT/US2022/077160
申请日：2022-09-28
申请人： GULFSTREAM AEROSPACE CORPORATION
发明人： BENNETT, Shawn , GAVIN, Joe , POWELL, Nicholas , FREUND, Donald , MUZYCHKA, Derek , LOUIS, John
IPC分类号： B64D33/02 , F02C7/042 , B64D27/20
摘要： An aircraft (20, 22) propulsion system includes an engine. The propulsion system further includes an inlet (36) having a forward cowl lip (38, 3, 40) and an aft cowl lip (40). The forward cowl lip (38, 3, 40) moves between retracted and deployed positions. The forward cowl lip (38, 3, 40) is adjacent to the aft cowl lip (40) when retracted. The forward cowl lip (38, 3, 40) is spaced apart from the aft cowl lip (40) when deployed. The forward cowl lip (38, 3, 40) has a smaller radius of curvature (R2) than the aft cowl lip (40). The propulsion system further includes a controller (52) coupled with the engine and inlet (36). The controller (52) restricts the maximum thrust commanded position of the engine when the aircraft (20, 22) is on the ground and moving below a predetermined speed. The controller (52) lifts the restriction when the aircraft (20, 22) is moving at at least the predetermined speed. The controller (52) controls the inlet (36) to deploy the cowl lip when the aircraft (20, 22) is on the ground.

27. 发明申请

WO2021026002A1 QUADTREE TERRAIN DATA COMPRESSION USING DISTANCE-BASED PRUNING 审中-公开
公开(公告)号：WO2021026002A1
公开(公告)日：2021-02-11
申请号：PCT/US2020/044524
申请日：2020-07-31
申请人： GULFSTREAM AEROSPACE CORPORATION
发明人： HOWE, Gregory
IPC分类号： G06F16/29 , G06F16/901 , G06T17/05 , G08G5/04
摘要： A tree structure represents a terrain area as nested polygons organized in a parent-child relationship, each polygon associated to a specific geographic location. The tree structure defines at least one parent node and a plurality of child nodes, some being leaf nodes containing a height value. A processor uses a distance measure to change the tree structure topology assessing whether all leaf node children of a first parent node lie outside a predetermined distance from an aircraft runway, and if so, converting the first parent node into a leaf node by storing in the first parent node a height value representing the greatest of the respective height values of the leaf node children and by removing the leaf node children; and iteratively repeating for each remaining parent node until it has been determined that every remaining parent node in the data structure cannot be pruned without violating accuracy requirements.

28. 发明申请

WO2016048737A1 METHODS AND SYSTEMS FOR COLLISION AVIODANCE USING VISUAL INDICATION OF WINGTIP PATH 审中-公开
标题翻译：使用WINGTIP路径的视觉指示的碰撞定位的方法和系统
公开(公告)号：WO2016048737A1
公开(公告)日：2016-03-31
申请号：PCT/US2015/050346
申请日：2015-09-16
申请人： GULFSTREAM AEROSPACE CORPORATION
发明人： ODELL, Robert , MANOCHIO, Frank , MEADE, Jason , BOOST, Michael
IPC分类号： G08G5/04 , G08G5/06 , H04N7/18
CPC分类号： B64D47/08 , B64C23/069 , G06K9/00624 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065 , H04N7/181 , Y02T50/164
摘要： The disclosed embodiments relate to methods and systems for avoiding a collision between an aircraft on the ground and an obstacle using a three-dimensional visual indication of the area or plane of winglets on the wingtips of the aircraft. The method includes receiving a video image from a camera positioned in one of the winglets, the video image representing a field of view through which the winglet of the aircraft will pass along a present heading of the aircraft. Next a processor determines a three-dimensional area or plane within the field of view through which the winglet of the aircraft will pass. An overlay is displayed within the field of view to assist the pilot in avoiding collisions with obstacles within the field of view.
摘要翻译：所公开的实施例涉及用于避免飞机在地面上与飞行器的翼尖之间的小翼的面积或平面的三维视觉指示的障碍物之间的碰撞的方法和系统。所述方法包括从位于所述小翼之一中的照相机接收视频图像，所述视频图像表示所述飞机的小翼将沿着飞行器的当前航向通过的视场。接下来，处理器确定在飞行器的小翼通过的视野范围内的三维区域或平面。在视野范围内显示覆盖物，以帮助飞行员避免与视场内的障碍物的碰撞。

29. 发明申请

WO2015137996A1 COMPONENTS MADE FROM PANELS AND METHODS OF PRODUCING THE SAME 审中-公开
标题翻译：从面板制成的部件及其制造方法
公开(公告)号：WO2015137996A1
公开(公告)日：2015-09-17
申请号：PCT/US2014/052664
申请日：2014-08-26
申请人： GULFSTREAM AEROSPACE CORPORATION
发明人： DAGGETT, Susan , AITKEN, Charles
IPC分类号： B29C44/12 , B29C70/08
CPC分类号： B32B37/185 , B29C44/1233 , B29C70/086 , B29D99/0021 , B32B5/18 , B32B7/12 , B32B2266/0221 , B32B2266/0264 , B32B2266/0271 , B32B2305/02 , B32B2305/72 , B32B2607/00 , Y10T428/2495
摘要： Methods for producing panels (30) and components (60) made from panels (62,78) are provided. A method of producing a panel includes positioning an expandable film (36) between a first (32) and second (34) layer, where the first and second layer include a fiber and a resin. The expandable film is expanded such that a distance between the first and second layers increases as the expandable film expands. Expansion of the expandable film is terminated when a panel thickness is within 1% of a panel thickness specification, and a polymer in the expandable film is crosslinked while the panel thickness is within 1% of the panel thickness specification.
摘要翻译：提供了由面板（62,78）制成的面板（30）和部件（60）的方法。制造面板的方法包括将可膨胀膜（36）定位在第一（32）和第二（34）层之间，其中第一和第二层包括纤维和树脂。可膨胀膜膨胀使得第一和第二层之间的距离随着可膨胀膜膨胀而增加。当面板厚度在面板厚度规格的1％以内时，可膨胀膜的膨胀终止，并且当板厚度在面板厚度规格的1％内时，可膨胀膜中的聚合物交联。

30. 发明申请

WO2014197016A1 RUNWAY OVERRUN MONITOR 审中-公开
标题翻译：运行监视器
公开(公告)号：WO2014197016A1
公开(公告)日：2014-12-11
申请号：PCT/US2014/018714
申请日：2014-02-26
申请人： GULFSTREAM AEROSPACE CORPORATION , HORNE, Thomas , LANDERS, Thomas , MAYO, John
发明人： HORNE, Thomas , LANDERS, Thomas , MAYO, John
IPC分类号： B60T8/17 , B64C25/42
CPC分类号： B64D45/00 , B64C25/426 , B64D45/04 , B64D2045/008 , G01C23/005 , G08G5/0021 , G08G5/025
摘要： Disclosed is a runway alerting method and system for a landing an aircraft. The method includes determining stopping positions for the aircraft along the runway using aircraft energy state, deceleration and braking information and displaying the stopping positions on a display. A system is provided that includes a first apparatus that is configured to determine an aircraft speed relative to the ground, a second apparatus that is configured to determine the aircraft's position, and a third apparatus that can provide information about the runway of intended landing. A flight system coupled to the first and second apparatus is configured to determine a minimum and corporate stopping position for the aircraft using the aircraft speed and the position relative to the runway. The minimum and corporation stopping positions are presented to the aircraft pilot on a display to as assist the pilot in safely landing the aircraft.
摘要翻译：公开了一种用于着陆飞机的跑道报警方法和系统。该方法包括使用飞机能量状态，减速度和制动信息确定飞机沿着跑道的停止位置，并在显示器上显示停止位置。提供了一种系统，其包括被配置为确定相对于地面的飞行器速度的第一装置，被配置为确定飞机的位置的第二装置，以及可以提供关于预期着陆的跑道的信息的第三装置。耦合到第一和第二装置的飞行系统被配置为使用飞行器速度和相对于跑道的位置来确定飞行器的最小和公司停止位置。最低限度和公司停止位置在展示架上呈现给飞行员，以协助飞行员安全着陆飞机。

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