Helicopter drip pan
    1.
    发明授权

    公开(公告)号:US09897254B2

    公开(公告)日:2018-02-20

    申请号:US15269626

    申请日:2016-09-19

    摘要: A drip pan apparatus for use in a helicopter includes a drip pan and a frame having a plurality of frame sides and a plurality of frame corners that define an inwardly-facing peripheral surface. A first frame angle is formed between a first inwardly-facing surface and a second inwardly-facing surface. The first frame angle is an acute angle. The drip pan has an outwardly-facing peripheral surface. The outwardly-facing peripheral surface defines a plurality of sides, including a first side and a second side, to cooperate with the inwardly-facing peripheral surface of the frame. A first angle is formed between the first side and the second side. The first angle is an acute angle. A method of installing a drip pan includes modifying at least a portion of a skirt on the helicopter and then securing the frame to one or both of the modified skirt and the helicopter structure.

    HELICOPTER DRIP PAN
    2.
    发明申请
    HELICOPTER DRIP PAN 审中-公开
    直升机DRI​​P PAN

    公开(公告)号:US20160238192A1

    公开(公告)日:2016-08-18

    申请号:US15054649

    申请日:2016-02-26

    IPC分类号: F16N31/00

    摘要: A drip pan apparatus for a “M” model BLACK HAWK® helicopter and the like includes an expanded corner structure for accommodating an access port also positioned further outwardly in the corner than in prior drip pan apparatuses, facilitating filter viewing while retaining peripheral o-ring seal. An expanded corner of the airframe skirt is accommodated by the expanded corresponding corner of a frame, which also defines a small radius internal curve. The removable pan has a small radius curve cooperating with the small radius curve of the frame and is sealed thereto by the peripheral o-ring seal sealing the entire pan to the frame. Physical access to the filter is enhanced.

    摘要翻译: 用于“M”型BLACKHAWK®直升机等的滴水器装置包括扩展的角结构,用于容纳还比现有的滴水盘装置更靠近角落定位的进入口,便于过滤器观察同时保持外围O形环 密封。 机身裙部的扩展角由框架的扩展的相应角部容纳,其也限定了小的半径内部曲线。 可移动盘具有与框架的小半径曲线协作的小半径曲线,并且通过将整个盘密封到框架的外围O形环密封件将其密封。 增强了对过滤器的物理访问。

    HELICOPTER DRIP PAN APPARATUS AND METHOD OF MAKING AND USING SUCH AN APPARATUS
    3.
    发明申请
    HELICOPTER DRIP PAN APPARATUS AND METHOD OF MAKING AND USING SUCH AN APPARATUS 审中-公开
    直升机拖动装置及其制造和使用方法

    公开(公告)号:US20150274310A1

    公开(公告)日:2015-10-01

    申请号:US14741891

    申请日:2015-06-17

    摘要: A drip pan apparatus for a helicopter includes a frame and a drip pan. The frame is secured to a skirt on the airframe of the helicopter. The apparatus includes a drip pan for cooperation with a frame to cover an access opening to a transmission. The drip pan includes a substantially planar member of a fiber-reinforced composite and has a seal surface that is configured to cooperate with a seal surface of the frame. A seal member may be disposed between the substantially planar member and the frame to form a fluid-tight seal. The fiber-reinforced composite may be a carbon fiber-reinforced composite. A method of making the drip pan apparatus includes placing a plurality of sheets of an uncured fiber-reinforced composite material on one another to form an uncured stack. The uncured stack is then cured. A frame and a drip pan may be cut from the cured stack.

    摘要翻译: 用于直升机的滴水盘装置包括框架和滴水盘。 框架固定在直升机的机身上的裙子上。 该装置包括与框架配合以覆盖变速器的进入开口的滴盘。 滴水盘包括纤维增强复合材料的基本平坦的构件,并且具有构造成与框架的密封表面配合的密封表面。 密封构件可以设置在基本平坦的构件和框架之间以形成流体密封。 纤维增强复合材料可以是碳纤维增强复合材料。 制造滴水盘装置的方法包括将多片未固化的纤维增强复合材料片彼此放置以形成未固化的叠层。 然后固化未固化的叠层。 可以从固化的堆叠中切割框架和滴盘。

    Helicopter drip pan
    4.
    发明授权
    Helicopter drip pan 有权
    直升机滴水盘

    公开(公告)号:US09447920B2

    公开(公告)日:2016-09-20

    申请号:US13839551

    申请日:2013-03-15

    摘要: A drip pan apparatus for use in a helicopter includes a drip pan and a frame having a plurality of frame sides and a plurality of frame corners that define an inwardly-facing peripheral surface. A first frame angle is formed between a first inwardly-facing surface and a second inwardly-facing surface. The first frame angle is an acute angle. The drip pan has an outwardly-facing peripheral surface. The outwardly-facing peripheral surface defines a plurality of sides, including a first side and a second side, to cooperate with the inwardly-facing peripheral surface of the frame. A first angle is formed between the first side and the second side. The first angle is an acute angle. A method of installing a drip pan includes modifying at least a portion of a skirt on the helicopter and then securing the frame to one or both of the modified skirt and the helicopter structure.

    摘要翻译: 用于直升机的滴水盘装置包括滴水盘和具有多个框架侧面的框架和限定向内的周向表面的多个框架拐角。 在第一向内的表面和第二向内的表面之间形成第一框架角度。 第一帧角度是锐角。 滴水盘具有向外的外围表面。 面向外的外围表面限定了包括第一侧和第二侧的多个侧面,以与框架的向内的外周表面配合。 在第一侧和第二侧之间形成第一角度。 第一个角度是一个锐角。 安装滴水盘的方法包括修改直升机上的裙部的至少一部分,然后将框架固定到修改的裙部和直升机结构中的一个或两个上。

    HELICOPTER DRIP PAN
    5.
    发明申请
    HELICOPTER DRIP PAN 有权
    直升机DRI​​P PAN

    公开(公告)号:US20140008484A1

    公开(公告)日:2014-01-09

    申请号:US13684828

    申请日:2012-11-26

    IPC分类号: F16N31/00

    摘要: A drip pan apparatus for a “M” model BLACK HAWK® helicopter and the like includes an expanded corner structure for accommodating an access port also positioned further outwardly in the corner than in prior drip pan apparatuses, facilitating filter viewing while retaining peripheral o-ring seal. An expanded corner of the airframe skirt is accommodated by the expanded corresponding corner of a frame, which also defines a small radius internal curve. The removable pan has a small radius curve cooperating with the small radius curve of the frame and is sealed thereto by the peripheral o-ring seal sealing the entire pan to the frame. Physical access to the filter is enhanced.

    摘要翻译: 用于“M”型BLACKHAWK®直升机的滴水器装置包括扩展的角结构,用于容纳还比现有的滴水盘装置更靠近角落定位的进入口,便于过滤器观察同时保持外围O形环 密封。 机身裙部的扩展角由框架的扩展的相应角部容纳,其也限定了小的半径内部曲线。 可移动盘具有与框架的小半径曲线协作的小半径曲线,并且通过将整个盘密封到框架的外围O形环密封件将其密封。 增强了对过滤器的物理访问。

    HELICOPTER DRIP PAN
    6.
    发明申请
    HELICOPTER DRIP PAN 审中-公开
    直升机DRI​​P PAN

    公开(公告)号:US20170067599A1

    公开(公告)日:2017-03-09

    申请号:US15269626

    申请日:2016-09-19

    IPC分类号: F16N31/00 B64C27/04 B64D47/00

    摘要: A drip pan apparatus for use in a helicopter includes a drip pan and a frame having a plurality of frame sides and a plurality of frame corners that define an inwardly-facing peripheral surface. A first frame angle is formed between a first inwardly-facing surface and a second inwardly-facing surface. The first frame angle is an acute angle. The drip pan has an outwardly-facing peripheral surface. The outwardly-facing peripheral surface defines a plurality of sides, including a first side and a second side, to cooperate with the inwardly-facing peripheral surface of the frame. A first angle is formed between the first side and the second side. The first angle is an acute angle. A method of installing a drip pan includes modifying at least a portion of a skirt on the helicopter and then securing the frame to one or both of the modified skirt and the helicopter structure.

    摘要翻译: 用于直升机的滴水盘装置包括滴水盘和具有多个框架侧面的框架和限定向内的周向表面的多个框架拐角。 在第一向内的表面和第二向内的表面之间形成第一框架角度。 第一帧角度是锐角。 滴水盘具有向外的外围表面。 面向外的外围表面限定了包括第一侧和第二侧的多个侧面,以与框架的向内的外周表面配合。 在第一侧和第二侧之间形成第一角度。 第一个角度是一个锐角。 安装滴水盘的方法包括修改直升机上的裙部的至少一部分,然后将框架固定到修改的裙部和直升机结构中的一个或两个上。

    Helicopter drip pan
    7.
    发明授权
    Helicopter drip pan 有权
    直升机滴水盘

    公开(公告)号:US09285077B2

    公开(公告)日:2016-03-15

    申请号:US13684828

    申请日:2012-11-26

    IPC分类号: B64C27/04 F16N31/00

    摘要: A drip pan apparatus for a “M” model BLACK HAWK® helicopter and the like includes an expanded corner structure for accommodating an access port also positioned further outwardly in the corner than in prior drip pan apparatuses, facilitating filter viewing while retaining peripheral o-ring seal. An expanded corner of the airframe skirt is accommodated by the expanded corresponding corner of a frame, which also defines a small radius internal curve. The removable pan has a small radius curve cooperating with the small radius curve of the frame and is sealed thereto by the peripheral o-ring seal sealing the entire pan to the frame. Physical access to the filter is enhanced.

    摘要翻译: 用于“M”型BLACKHAWK®直升机的滴水器装置包括扩展的角结构,用于容纳还比现有的滴水盘装置更靠近角落定位的进入口,便于过滤器观察同时保持外围O形环 密封。 机身裙部的扩展角由框架的扩展的相应角部容纳,其也限定了小的半径内部曲线。 可移动盘具有与框架的小半径曲线协作的小半径曲线,并且通过将整个盘密封到框架的外围O形环密封件将其密封。 增强了对过滤器的物理访问。

    HELICOPTER DRIP PAN
    8.
    发明申请
    HELICOPTER DRIP PAN 有权
    直升机DRI​​P PAN

    公开(公告)号:US20140263819A1

    公开(公告)日:2014-09-18

    申请号:US13839551

    申请日:2013-03-15

    IPC分类号: F16N31/00 B64D47/00

    摘要: A drip pan apparatus for use in a helicopter includes a drip pan and a frame having a plurality of frame sides and a plurality of frame corners that define an inwardly-facing peripheral surface. A first frame angle is formed between a first inwardly-facing surface and a second inwardly-facing surface. The first frame angle is an acute angle. The drip pan has an outwardly-facing peripheral surface. The outwardly-facing peripheral surface defines a plurality of sides, including a first side and a second side, to cooperate with the inwardly-facing peripheral surface of the frame. A first angle is formed between the first side and the second side. The first angle is an acute angle. A method of installing a drip pan includes modifying at least a portion of a skirt on the helicopter and then securing the frame to one or both of the modified skirt and the helicopter structure.

    摘要翻译: 用于直升机的滴水盘装置包括滴水盘和具有多个框架侧面的框架和限定向内的周向表面的多个框架拐角。 在第一向内的表面和第二向内的表面之间形成第一框架角度。 第一帧角度是锐角。 滴水盘具有向外的外围表面。 面向外的外围表面限定了包括第一侧和第二侧的多个侧面,以与框架的向内的外周表面配合。 在第一侧和第二侧之间形成第一角度。 第一个角度是一个锐角。 安装滴水盘的方法包括修改直升机上的裙部的至少一部分,然后将框架固定到修改的裙部和直升机结构中的一个或两个上。