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    LANDING GEAR INCLUDING A COMPOSITE STRUT TUBE AND METHODS FOR ASSEMBLING THE SAME
    1.
    发明公开
    LANDING GEAR INCLUDING A COMPOSITE STRUT TUBE AND METHODS FOR ASSEMBLING THE SAME 有权
    FAHRWERK MIT EINEM VERBUNDTRAGROHR UND MONTAGEVERFAHRENDAFÜR

    公开(公告)号：EP3127806A1

    公开(公告)日：2017-02-08

    申请号：EP16182411.5

    申请日：2016-08-02

    申请人： Goodrich Corporation

    发明人： LUCE, William E.

    IPC分类号： B64C25/02 ,  B64C25/12

    CPC分类号： B64C25/10 ,  B64C25/02 ,  B64C25/12 ,  B64C2025/125

    摘要： A landing gear is provided. The landing gear includes a composite strut tube (116) having a first lug (122a) and a second lug (122b) thereon. A first brace (112) is coupled to the composite strut tube (116) with a first two-force member (128) via the first lug (122a) and a second brace (114) is coupled to the composite strut tube (116) with a second two-force member (128) via the second lug (122b). A method for assembling the landing gear is also provided.

    摘要翻译： 提供起落架。 起落架包括在其上具有第一凸耳（122a）和第二凸耳（122b）的复合支柱管（116）。 第一支架（112）经由第一凸耳（122a）与第一双向力构件（128）联接到复合支柱管（116），并且第二支撑件（114）联接到复合支柱管（116） 通过第二凸耳（122b）具有第二两个力构件（128）。 还提供了组装起落架的方法。

    QUICK CHANGE WHEEL LANDING GEAR
    7.
    发明公开
    QUICK CHANGE WHEEL LANDING GEAR 失效
    快速更换轮胎齿轮

    公开(公告)号：EP0403501A4

    公开(公告)日：1991-05-08

    申请号：EP89902486

    申请日：1988-12-08

    申请人： BELL HELICOPTER TEXTRON INC.

    发明人： DAVIS, CHARLES, E. ,  DUPPSTADT, J., ROBERT

    IPC分类号： B64C25/04 ,  B64C25/02

    CPC分类号： B64C25/02 ,  B64C2025/325

    摘要： A quick change wheel landing gear assembly (10) is provided as a replacement for a skid landing gear system on a vertical take-off and landing aircraft. The wheel landing gear assembly (10) includes a pair of spaced-apart fore and aft longitudinal tubes (16, 18) attached to a pair of short, spaced-apart cross tubes (20, 22) that are adapted to mount on the structural saddles (12, 14) used to mount the skid landing gear on the underside of the aircraft. The longitudinal tubes (16, 18) are connected together at the forward end for mounting a fully swiveling nose gear (26) thereto. Aft main gear wheels (30, 32) are mounted on cantilever landing gear legs (34, 36) that extend laterally from the longitudinal tubes (16, 18) adjacent the aft cross tube (22). Landing loads on the landing gear may be absorbed by resilient springs (25), deflection of the gear legs (34, 36) and the aft cross tube (22), torsion of the fore and aft longitudinal tubes (16, 18), or any combination of these actions. The wheel landing gear assembly (10) is designed to be mounted on existing aircraft structural saddles which eliminates the need for special landing support structure needed in the prior art.

    AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE
    8.
    发明公开
    AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE 审中-公开
    空气动力学噪音减少薄皮登陆齿轮结构

    公开(公告)号：EP3257749A1

    公开(公告)日：2017-12-20

    申请号：EP17176442.6

    申请日：2017-06-16

    申请人： Goodrich Corporation

    发明人： HIMMELMANN, Richard A.

    IPC分类号： B64C25/02 ,  B64C25/60

    CPC分类号： B64C25/10 ,  B64C25/02 ,  B64C25/34 ,  B64C25/60 ,  B64C2025/003

    摘要： A landing gear assembly is also provided. The landing gear assembly may include a thin-skin support member (102) defining a cavity (200) and a cylindrical cavity (300). A cylinder may extend from the cylindrical cavity with an axle (114) extending from the cylinder. A torsion link (116) may be coupled to the axle and a torsion interface (314) of the thin-skin support member.

    摘要翻译： 还提供了起落架组件。 起落架组件可包括限定空腔（200）和圆柱形空腔（300）的薄皮支撑构件（102）。 圆柱体可以从圆柱形腔体延伸，并具有从圆柱体延伸的轴（114）。 扭转连杆（116）可以联接到薄皮支撑构件的轴和扭转界面（314）。