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2565 条记录 (耗时 0.028 秒)

    PASSIVE INTERNAL ICE PROTECTION SYSTEMS FOR ENGINE INLETS
    91.
    发明公开
    PASSIVE INTERNAL ICE PROTECTION SYSTEMS FOR ENGINE INLETS 有权
    用于发动机进气道的被动内冰保护系统

    公开(公告)号：EP3170751A1

    公开(公告)日：2017-05-24

    申请号：EP16170623.9

    申请日：2016-05-20

    申请人： Bell Helicopter Textron Inc.

    发明人： AUBERT, Roger J.

    IPC分类号： B64D27/14 ,  B64D33/02

    CPC分类号： F02C7/055 ,  B64C27/06 ,  B64D27/14 ,  B64D33/02 ,  B64D2033/022 ,  B64D2033/0233 ,  B64D2033/0246 ,  F02C7/047 ,  F05D2220/329 ,  F05D2230/60 ,  F05D2300/171 ,  F05D2300/614

    摘要： A system (230) includes an engine cover (124; 200) covering a side-facing rotorcraft engine (120) and having an opening (204) and an ice protection member (126; 210) mounted on the engine cover (124; 200) between the opening (204) and the engine (120), an area of the ice protection member (126; 210) smaller than an area of the opening (204). The ice protection member (126; 210) is configured to partially cover the opening (204) to prevent ice having a particular size from entering into the engine (120) and to allow air flow downstream into the engine (120).

    摘要翻译： 一种系统（230）包括覆盖侧向旋翼飞行器发动机（120）并且具有安装在发动机盖（124; 200）上的开口（204）和防冰构件（126; 210）的发动机盖（124; 200） ）在所述开口（204）和所述发动机（120）之间，所述防冰构件（126; 210）的面积小于所述开口（204）的面积。 防冰构件（126; 210）构造成部分地覆盖开口（204）以防止具有特定尺寸的冰块进入发动机（120）并且允许空气流向下游进入发动机（120）。

    FLIGHT CONTROL LAWS FOR A ROTARY AIRCRAFT
    94.
    发明公开
    FLIGHT CONTROL LAWS FOR A ROTARY AIRCRAFT 有权
    飞行控制功能，直升机

    公开(公告)号：EP3101505A3

    公开(公告)日：2017-03-01

    申请号：EP16176949.2

    申请日：2011-07-15

    申请人： Bell Helicopter Textron Inc.

    发明人： Christensen, Kevin Thomas ,  Shue, Shyhpyng Jack ,  Caudhill, Troy Sheldon

    IPC分类号： G05D1/06 ,  G05D1/10 ,  B64C19/00

    CPC分类号： B64C19/00 ,  G05D1/102

    摘要： The disclosure relates to a flight control system for a rotary aircraft, the rotary aircraft having a longitudinal controller, a lateral controller, a directional controller, and a vertical controller, the control system comprising a longitudinal loop design, a lateral loop design, a directional loop design and a vertical control loop design, a forward speed hold loop and a lateral speed hold loop automatically engaging when the longitudinal controller is returned to a detent position and the aircraft groundspeed is outside a first groundspeed threshold, longitudinal and lateral maneuverability being controlled by either a pitch attitude and lateral speed loop or a pitch rate and roll rate loop when the longitudinal controller is out of the detent position.

    TAIL SPAR SPRING
    95.
    发明授权
    TAIL SPAR SPRING 有权
    尾羽HOLM

    公开(公告)号：EP2982597B1

    公开(公告)日：2017-01-25

    申请号：EP15177693.7

    申请日：2015-07-21

    申请人： Bell Helicopter Textron Inc.

    发明人： Van Buskirk, Matthew Carl ,  Seifert, Michael Scott ,  Burnett, Michael Christopher ,  Isaac, Mark Loring

    IPC分类号： B64C1/26 ,  B64C5/00 ,  B64C29/00

    CPC分类号： B64C5/02 ,  B64C1/26 ,  B64C5/10 ,  B64C29/0033

    摘要： According to one embodiment, an empennage attachment system features an aft attachment mechanism (164) and a forward attachment system (200). The aft attachment mechanism (164) is configured to be coupled to a tail section of a body of an aircraft (100) and to an empennage (160) proximate to an aft spar (162) of the empennage (160). The aft attachment mechanism (164) defines a pitch axis (165) such that the aft attachment mechanism (164) allows the empennage (160) to rotate about the pitch axis (165). The forward attachment system (200) is configured to be coupled to the tail section of the body and to the empennage (160) proximate to a forward spar (166) of the empennage (160). The forward attachment system (200) is configured to restrict rotation of the empennage (160) about the pitch axis (165) to an allowable range of motion.

    LIGHTWEIGHT LANDING GEAR SKID SHOE ASSEMBLY
    99.
    发明授权
    LIGHTWEIGHT LANDING GEAR SKID SHOE ASSEMBLY 有权
    轻质SKID LANDING塔架工厂

    公开(公告)号：EP2679490B1

    公开(公告)日：2016-12-21

    申请号：EP12178623.0

    申请日：2012-07-31

    申请人： Bell Helicopter Textron Inc.

    发明人： McCollough, James ,  Amante, William

    IPC分类号： B64C25/52 ,  B64C25/32

    CPC分类号： B64C25/52 ,  B64C2025/325

    摘要： A lightweight skid shoe assembly (100) comprises a body (200) of wear resistant, non-metallic or partially metallic material; and a structure coupling mechanism (300); wherein the body prevents friction-related damage to the structure. Another lightweight skid shoe assembly (150) comprises a body of wear resistant, non-metallic or partially metallic material selected from the group consisting of: a polyamide or polyimide impregnated carbon fiber layup, a peek or PEI injection mold with carbon fiber, compression molded carbon fiber or fiberglass, a resin infusion with carbon fiber preform fabric, a fiber reinforced thermoset, acetal resin, machined acetal or thermoplastic, thermosetting plastic, or a metal-matrix composite; wherein the body prevents friction-related damage to a structure. Another lightweight skid shoe assembly (180) comprises a body of wear resistant, non-metallic or partially metallic material; and a shear-bearing mechanism (400); wherein the shear-bearing mechanism directs shear forces away from the body; and wherein the body prevents friction-related damage to the structure.