Control box
    41.
    发明授权
    Control box 有权
    控制箱

    公开(公告)号:US09193434B2

    公开(公告)日:2015-11-24

    申请号:US13761767

    申请日:2013-02-07

    摘要: A control box for selectively delivering orders to receivers (8, 12). The control box comprises a shaft (14) mounted to turn about an axis of rotation (X), while being capable of sliding along the axis (X) between a rest position towards which it is urged by return means (24), and an active position. An order delivery apparatus (16, 11) co-operates with the shaft (14) to deliver orders as a function of the angular position of the shaft (14). A rotary drive (15) causes the shaft to turn. A safety actuator (23) causes the shaft to slide from the rest position in which anti-rotation structure (27, 28) prevents the shaft from turning to the active position in which the anti-rotation structure (27, 28) leave the shaft free to turn under drive from the rotary drive (15).

    摘要翻译: 一种用于选择性地向接收器(8,12)递送订单的控制箱。 所述控制箱包括安装成围绕旋转轴线(X)旋转的轴(14),同时能够在其被所述返回装置(24)所推动的静止位置之间沿所述轴线(X)滑动;以及 积极的位置 订单传送装置(16,11)与轴(14)协作,作为轴(14)的角位置传递订单。 旋转驱动器(15)使轴转动。 安全致动器(23)使得轴从静止位置滑动,其中防旋转结构(27,28)防止轴转动到防转动结构(27,28)离开轴的有效位置 在旋转驱动器(15)的驱动下自由转动。

    Air-ground detection system for semi-levered landing gear
    42.
    发明授权
    Air-ground detection system for semi-levered landing gear 有权
    半起落架起落架空地探测系统

    公开(公告)号:US08939400B2

    公开(公告)日:2015-01-27

    申请号:US13031525

    申请日:2011-02-21

    IPC分类号: B64C25/34 B64C25/00

    摘要: A method and apparatus for air-ground detection. A truck beam of a semi-levered landing gear is mounted on a pivot pin. The truck beam is configured to rotate about the pivot pin between a toes down position and a toes up position. A positioning mechanism is connected to a semi-levered linkage assembly that secures an angle of the truck beam in the toes up position. The semi-levered linkage assembly is secured in a steady state and configured to change from the steady state to a locked state in response to an initial ground contact. A sensor is connected to the semi-levered linkage assembly. The sensor is configured to detect a change from the steady state to the locked state.

    摘要翻译: 一种用于空地检测的方法和装置。 半顶起落架的卡车梁安装在枢轴销上。 卡车梁构造成在脚趾向下位置和脚趾位置之间围绕枢转销旋转。 定位机构连接到半杠杆联动组件,其将卡车梁的角度固定在脚趾上方位置。 半杠杆连杆组件固定在稳定状态并且被配置为响应于初始地面接触而从稳定状态改变到锁定状态。 传感器连接到半杠连杆组件。 传感器被配置为检测从稳定状态到锁定状态的变化。

    CONTROL BOX
    43.
    发明申请
    CONTROL BOX 有权
    控制箱

    公开(公告)号:US20150021432A1

    公开(公告)日:2015-01-22

    申请号:US14511008

    申请日:2014-10-09

    IPC分类号: B64C1/14 B64C25/00

    摘要: The invention provides a control box for selectively delivering orders to receivers (8, 12), the control box comprising: a shaft (14) mounted to turn about an axis of rotation (X), while being capable of sliding along said axis (X) between a rest position towards which it is urged by return means (24), and an active position; order delivery means (16, 11) co-operating with the shaft (14) to deliver orders as a function of the angular position of the shaft (14); rotary drive means (15) for causing the shaft to turn; and safety actuation means (23) for causing the shaft to slide from the rest position in which anti-rotation means (27, 28) prevent the shaft from turning to the active position in which the anti-rotation means (27, 28) leave the shaft free to turn under drive from the rotary drive means (15).

    摘要翻译: 本发明提供了一种用于向接收器(8,12)选择性地传送订单的控制箱,所述控制箱包括:安装成围绕旋转轴线(X)旋转的轴(14),同时能够沿所述轴线(X )在其被所述返回装置(24)推动的静止位置和活动位置之间; 与所述轴(14)配合的订单传送装置(16,11)作为所述轴(14)的角位置递送订单; 旋转驱动装置(15),用于使轴转动; 以及用于使轴从静止位置滑动的安全致动装置(23),在该位置,防转动装置(27,28)防止轴转动到防转动装置(27,28)离开的有效位置 所述轴在旋转驱动装置(15)的驱动下自由转动。

    METHOD AND SYSTEM FOR DETERMINING FRICTION COEFFICIENT μ FOR AN AIRCRAFT LANDING EVENT
    46.
    发明申请
    METHOD AND SYSTEM FOR DETERMINING FRICTION COEFFICIENT μ FOR AN AIRCRAFT LANDING EVENT 有权
    用于确定飞机登陆事件的摩擦系数μ的方法和系统

    公开(公告)号:US20140107990A1

    公开(公告)日:2014-04-17

    申请号:US14005500

    申请日:2012-03-16

    IPC分类号: G06F17/50

    摘要: Method and system of determining ground-to-tyre friction coefficient for an aircraft landing event. The method uses an aircraft computational model to repeatedly model the landing event, varying one or more initial conditions of the aircraft model until a best match between a modelled value and a provided value of aircraft vertical acceleration is determined. The method uses initial conditions associated with the best match of modelled and provided vertical acceleration values and a strain value from a sensor on the aircraft landing gear, with the ground-to-tyre friction coefficient is a variable. The method models the landing gear to generate a modelled strain value and compares this with the measured strain value, and repeats the landing gear modelling step with a different value for the ground-to-tyre friction coefficient until a best match between the modelled strain value and the measured strain value is determined and outputting the respective friction coefficient value.

    摘要翻译: 确定飞机着陆事件的地面与轮胎摩擦系数的方法和系统。 该方法使用飞行器计算模型来重复模拟着陆事件,改变飞行器模型的一个或多个初始条件,直到确定了建模值和所提供的飞机垂直加速度值之间的最佳匹配。 该方法使用与建模和提供的垂直加速度值的最佳匹配的初始条件和来自飞机起落架上的传感器的应变值,其中地对轮胎摩擦系数是变量。 该方法对起落架进行建模以产生建模应变值,并将其与测量的应变值进行比较,并重复起落架建模步骤,其具有不同的地对轮胎摩擦系数值,直到建模的应变值之间的最佳匹配 并且确定测量的应变值并输出相应的摩擦系数值。

    MECHANICAL POSITION INDICATOR
    47.
    发明申请
    MECHANICAL POSITION INDICATOR 有权
    机械位置指示器

    公开(公告)号:US20140026808A1

    公开(公告)日:2014-01-30

    申请号:US13989597

    申请日:2011-11-09

    IPC分类号: B64D45/00

    摘要: A mechanical position indicator for providing a visual indication that a first part of an aircraft landing gear has assumed a predetermined position relative to a second part, the position indicator being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element in a deployed position, the position indicator being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator from the first state to a second state in which the indicator element is displaced from the deployed position, the position indicator being arranged to inhibit the indicator element thereafter returning to the deployed position.

    摘要翻译: 一种用于提供飞行器起落架的第一部分相对于第二部分已经具有预定位置的视觉指示的机械位置指示器,所述位置指示器布置成联接到所述第一和第二部分中的第一部分,并且以 第一状态被布置成将指示器元件保持在展开位置,位置指示器布置成使得在第一部分相对于第二部分呈现预定位置时,第一部分和第二部分中的第二部分将位置指示器从第一部分 状态到第二状态,其中指示元件从展开位置移位,位置指示器布置成阻止指示元件返回到展开位置。

    Method And Apparatus For Measuring The Weight Of A C-130 Aircraft With Jack-Screw Retraction Mechanism For The Main Landing Gear
    48.
    发明申请
    Method And Apparatus For Measuring The Weight Of A C-130 Aircraft With Jack-Screw Retraction Mechanism For The Main Landing Gear 审中-公开
    用于测量C-130飞机重量的方法和装置,其中主起落架采用千斤顶螺旋退缩机构

    公开(公告)号:US20130327579A1

    公开(公告)日:2013-12-12

    申请号:US13911603

    申请日:2013-06-06

    申请人: C. Kirk Nance

    发明人: C. Kirk Nance

    IPC分类号: G01G19/08 B64C25/00

    摘要: A method and apparatus for determining the weight of a C-130 aircraft with jack-screw landing gear compression loads applied to a C-130 aircraft main landing gear strut jack-screw friction washer. For each main landing gear, a thru-hole load cell is mounted to the bottom of the jack-screw so that the weight of the aircraft bears on the load cell. The load cells are connected to a computer which measures the loads and determining the weight and center of gravity of the aircraft.

    摘要翻译: 一种用于确定C-130飞机的重量的方法和装置,其具有应用于C-130飞机主起落架支柱螺杆摩擦垫圈的千斤顶起落架压缩载荷。 对于每个主起落架,通孔测力传感器安装在千斤顶螺丝的底部,以便飞机的重量承载在称重传感器上。 称重传感器连接到测量载荷并确定飞机重量和重心的计算机。

    SYSTEMS AND METHODS FOR LANDING IDENTIFICATION

    公开(公告)号:US20130144559A1

    公开(公告)日:2013-06-06

    申请号:US13312073

    申请日:2011-12-06

    IPC分类号: G06F15/00 H03K21/00

    摘要: Systems and methods disclosed herein may be useful for use in landing identification. In this regard, a method is provided comprising receiving pulse information over a first time period, wherein the pulse information is indicative of an angular distance traveled by a first wheel, comparing the pulse information to a threshold value, and determining a likelihood of a landing event based upon the comparison. In various embodiments, a system is provided comprising a monstable multivibrator in electrical communication with a metal-oxide-semiconductor field-effect transistor (MOSFET), a resistor-capacitor network in electrical communication with the MOSFET, and a comparator that receives a voltage from the resistor-capacitor network and a reference voltage.

    Energy absorber system for an undercarriage, and an aircraft provided with said energy absorber system
    50.
    发明授权
    Energy absorber system for an undercarriage, and an aircraft provided with said energy absorber system 有权
    用于起落架的能量吸收器系统,以及设有所述能量吸收器系统的飞行器

    公开(公告)号:US08439304B2

    公开(公告)日:2013-05-14

    申请号:US13088511

    申请日:2011-04-18

    IPC分类号: B64C25/58

    摘要: An energy absorber system (10) provided with a shock absorber (11) extending from a first end (12) suitable for being connected to a rocker arm (5) of an undercarriage (3) housed in a wheel bay (4), towards a second end (13). In addition, the system includes a fitting (20) connected to said second end (13), and guide means (30) for guiding said fitting (20) in translation that is suitable for being fastened to a flank (4″) of said wheel well (4), said system (10) including deformable energy absorber means (40) fastened to said fitting (20) and suitable for being fastened to a structure (4″) of said bay (4) and also to fusible retention means (50) suitable for fastening said fitting (20) to said flank (4″), said fusible retention means (50) rupturing from a predetermined threshold in order to allow said fitting (20) to move under guidance from said guide means (30) so as to deform said energy absorber means (40).

    摘要翻译: 一种能量吸收器系统(10),其具有从适于连接到容纳在轮舱(4)中的起落架(3)的摇臂(5)的第一端(12)延伸的减震器(11),朝向 第二端(13)。 此外,该系统包括连接到所述第二端(13)的接头(20)和用于引导所述接头(20)平移的引导装置(30),所述引导装置适于紧固到侧面(4“)的侧面 所述轮井(4),所述系统(10)包括紧固到所述配件(20)并且适于紧固到所述托架(4)的结构(4“)的可变形能量吸收器装置(40) 适于将所述配件(20)紧固到所述侧面(4“)的保持装置(50),所述可熔保持装置(50)从预定阈值破裂,以便允许所述配件(20)在所述引导件 装置(30),以使所述能量吸收装置(40)变形。