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公开(公告)号：EP3336485B1
公开(公告)日：2020-09-23
申请号：EP16204453.1
申请日：2016-12-15
发明人： Cokonaj, Valerijan , Collett, Laura
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公开(公告)号：EP3611093A1
公开(公告)日：2020-02-19
申请号：EP19188563.1
申请日：2019-07-26
申请人： The Boeing Company
发明人： ALLEY, Christopher M , CAMPBELL, Leanne M , DEFRANCISCI, Gabriela K , VERING, Gregory J , KNOCK, Aaron P , MELLOR, Mitchell , COTTET, Justin D
摘要： A landing gear (100A, 100B) including an outer cylinder (110) rotatably coupled to a frame of an aircraft (1000) about a trunnion axis of rotation, a shock strut assembly (120) movably coupled to the outer cylinder (110) so as to reciprocate along a longitudinal axis (115) of the outer cylinder, and a shrink mechanism (130A, 130B) including a first shrink link member (140) pivotally coupled to the outer cylinder, a second shrink link member (150) coupling the first shrink link member to the shock strut assembly (120), a crank member (160) pivotally coupled to the outer cylinder (110), a drive member (170) coupling the crank member (160) to a walking beam (210) of a landing gear retract mechanism (200), and a driven member (180) coupling the crank member (160) to the first shrink link member (140).
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公开(公告)号：EP3450306A1
公开(公告)日：2019-03-06
申请号：EP17189451.2
申请日：2017-09-05
发明人： Hilliard, Matthew
摘要： A telescopic device (10, 30) comprising: a housing (12) having an inner side wall surface defining a bore (B) with an open end; a rod (14) having an end slidably mounted within the bore to linearly move relative to the housing along a longitudinal axis between an extended position, where the telescopic device is relatively long, and a retracted position, where the telescopic device is relatively compressed; a first bearing (16) and a second bearing (18) each defining a bearing surface arranged to provide sliding engagement between the rod and housing, the first bearing being mounted relatively close to the open end of the bore and the second bearing being mounted relatively far from the open end of the bore relative to the first bearing, wherein the second bearing is annular in shape with a central axis, the bearing has a radially outer mounting surface of arcuate cross-section and a radially inner bearing surface for sliding engagement with an outer surface of the rod and wherein the inner sidewall is provided with an annular groove having a second mounting surface of arcuate cross-section to house and retain the second bearing.
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94.发明公开
公开(公告)号：EP3418190A1
公开(公告)日：2018-12-26
申请号：EP18179663.2
申请日：2018-06-25
申请人： Goodrich Corporation
CPC分类号： B64C25/58 , B64C25/60 , B64C2025/008
摘要： A landing gear arrangement may comprise a lever (230) configured to be coupled between an axle and a strut piston of a shock strut (201), a load damper (250, 450) configured to be externally coupled between the shock strut (201) and the lever (230), wherein the load damper (250, 450) is configured to increase a length of the landing gear arrangement in response to an extension force of the load damper increasing above a ground force reacted through the landing gear arrangement. The load damper (250, 450) may be located externally from the strut piston.
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公开(公告)号：EP3000728B1
公开(公告)日：2018-11-28
申请号：EP15186603.5
申请日：2015-09-24
申请人： Goodrich Corporation
发明人： Noel C., HAYNES , Marilea, MANZINI
CPC分类号： B64C25/58 , B64C25/10 , B64D2045/009 , C22C19/07 , F16F9/3235
摘要： The present disclosure includes landing gear components, such as an outer cylinder (104) of a shock strut assembly (102). The outer cylinder (104) includes one or more structural attachment pins (105) configured to engage with other components of the landing gear including pintle frames (110), drag braces (106), and torque links (124). The pins (105) include a cobalt alloy mated to a cobalt containing coating (140) for improved wear resistance, which may eliminate the need for a bushing between the pin (105) and the receptacle (107) of the corresponding landing gear component.
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公开(公告)号：EP3395681A1
公开(公告)日：2018-10-31
申请号：EP18169168.4
申请日：2018-04-25
发明人： KLIM, Graeme Peter Arthur , AMBERG, Steven Kevin , RODRIGUES DE SOUZA MEIRELES, Clément , ADHIKARI, Min Prasad , ELAHIKAHOUKER, Mohammad Moeid , HASHEMI, Seyed Mohammad
摘要： A shock strut (100) for a vehicle includes a housing (130) with a through channel (131) and a motor mount (134), and a motor (150) fixed to the housing (130). The cylinder (106) of a shock strut (100) is configured to define a lead screw (107) on its outer surface. The cylinder (106) extends through the housing (130). The piston (104) of the shock strut (100) is attached to a ground engaging assembly (110). A gear nut (140) rotatably mounted in the housing (130) threadably engages the threaded cylinder (106), and is configured to be driven by the motor (150). The housing (130) is attached to the vehicle, and the gear nut (140) is controllably rotated to extend and retract the shock strut (100). A sensor (155) provided on the assembly monitors the position of the shock strut (100). A torsion link assembly (120) reacts rotational forces on the cylinder (106).
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公开(公告)号：EP2630036B1
公开(公告)日：2018-03-28
申请号：EP11834911.7
申请日：2011-10-14
CPC分类号： B64C25/50 , B64C25/14 , B64C2025/006 , F16C11/02 , F16C11/045 , F16C2326/43 , Y10T403/602
摘要： A torque link member for aircraft landing gear includes a first end for connecting to a lower portion or an upper portion of the aircraft landing gear and a second end for connecting to another torque link member. A locking pin is disposed on one of the upper portion, the lower portion, the first end or the second end. The locking pin is axially movable between an engaged position wherein the pin protrudes for interengagement with a cooperating aperture on the first end, the second end, the upper portion, the lower portion, or the second end of the other torque link member, and a disengaged position. The locking pin is biased toward the engaged position and movable against the biasing to the disengaged position.
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公开(公告)号：EP2598772A4
公开(公告)日：2017-12-06
申请号：EP11811707
申请日：2011-07-28
发明人： BESLIU MARIN
CPC分类号： B64C25/505 , F16F9/065 , F16F9/325 , F16F13/007
摘要： A hydraulic shimmy damper that resolves drawbacks in several known shimmy dampers, such as damping characteristics that are dependent on oil temperature variations. The disclosed shimmy damper includes a hydraulic compensator (40) having an internal fluid volume that is significantly more important than a fluid volume expelled from the body of the shimmy damper when its piston moves fore and aft. The shimmy damper also includes a hydraulic manifold (30) arranged between the body and the hydraulic compensator and defining a transfer channel between chambers in the piston that is connected to the hydraulic compensator. The manifold receives interchangeable hydraulic cartridge-type valves (CV1,RV1; CV2,RV2) for metering the fluid flowing from the chambers to the transfer channel, and allows the fluid to freely enter the chambers from the transfer channel. The present shimmy damper is therefore much less sensitive to oil temperature variation under intense shimmy.
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99.发明公开IMPROVED SERVICING PROCEDURE FOR SINGLE-STAGE MIXED FLUID/GAS SHOCK STRUT 审中-公开改进的单级混合流体/气体冲击柱的维修程序
公开(公告)号：EP3165456A1
公开(公告)日：2017-05-10
申请号：EP16197134.6
申请日：2016-11-03
申请人： Goodrich Corporation
发明人： FAZELI, Amir , CEPIC, Adnan , REBER, Susanne
CPC分类号： F16F9/3271 , B64C25/58 , B64C25/60 , B64F5/40 , F16F9/06 , F16F2230/46 , H05K999/99
摘要： Methods for servicing shock struts (104;210) are provided. In various embodiments, a method for servicing a shock strut (104;210) may comprise deflating the shock strut (104;210); compressing the shock strut (104;210) until the shock strut (104;210) is in a fully compressed position; and charging the shock strut (104;210) with a liquid until a pressure of the liquid decreases a volume of a residual air located inside of the shock strut (104;210). In various embodiments, charging the shock strut (104;210) with liquid under pressure may reduce the volume of trapped air inside of the shock strut (104;210) to a negligible volume, eliminating the servicing variations.
摘要翻译： 提供了用于维修减震支柱（104; 210）的方法。 在各种实施例中，用于维修减震支柱（104; 210）的方法可包括使减震支柱（104; 210）缩小; 压缩减震支柱（104; 210）直到减震支柱（104; 210）处于完全压缩位置; 以及用液体给所述减震支柱（104; 210）充电，直到所述液体的压力减小位于所述减震支柱（104; 210）内部的残余空气的体积。 在各种实施例中，用压力下的液体给减震支柱（104; 210）充电可以将减震支柱（104; 210）内的截留空气的体积减小到可忽略的体积，从而消除了维修变化。
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100.发明公开LANDING GEAR COMPONENTS HAVING IMPROVED JOINTS 审中-公开FAHRWERK MIT KOMPONENTEN MIT VERBESSERTEN GELENKEN
公开(公告)号：EP3000728A1
公开(公告)日：2016-03-30
申请号：EP15186603.5
申请日：2015-09-24
申请人： Goodrich Corporation
发明人： Noel C., HAYNES , Marilea, MANZINI
CPC分类号： B64C25/58 , B64C25/10 , B64D2045/009 , C22C19/07 , F16F9/3235
摘要： The present disclosure includes landing gear components, such as an outer cylinder (104) of a shock strut assembly (102). The outer cylinder (104) includes one or more structural attachment pins (105) configured to engage with other components of the landing gear including pintle frames (110), drag braces (106), and torque links (124). The pins (105) include a cobalt alloy mated to a cobalt containing coating (140) for improved wear resistance, which may eliminate the need for a bushing between the pin (105) and the receptacle (107) of the corresponding landing gear component.
摘要翻译： 本公开包括起落架部件，例如冲击支柱组件（102）的外筒（104）。 外筒（104）包括一个或多个结构连接销（105），其构造成与起落架的其他部件啮合，包括枢轴框架（110），拖拉支架（106）和扭矩连杆（124）。 销（105）包括配合到含钴涂层（140）的钴合金，用于改善耐磨性，这可以消除对相应起落架部件的销（105）和接收器（107）之间的衬套的需要。
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