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公开(公告)号：WO2010138229A2
公开(公告)日：2010-12-02
申请号：PCT/US2010/026465
申请日：2010-03-08
Applicant: SIKORSKY AIRCRAFT CORPORATION , TONI, Darryl M. , MCCARTHY, Mary , BARR, Bruce, H. , STOBIECKI, Anthony, Z. , SWIFT, Thomas , DZIEKONSKI, Thomas
Inventor： TONI, Darryl M. , MCCARTHY, Mary , BARR, Bruce, H. , STOBIECKI, Anthony, Z. , SWIFT, Thomas , DZIEKONSKI, Thomas
Abstract: An external hook system for a rotary-wing aircraft includes a lower frame interface which accommodates longitudinal and lateral loads and an upper frame interface. A tension member is mountable between the lower frame interface and the upper frame interface to transfer tension loads between the lower frame interface and the upper frame interface.
Abstract translation: 用于旋转翼飞行器的外部钩系统包括容纳纵向和横向载荷的下部框架接口以及上部框架接口。 张紧构件可安装在下框架接口和上框架接口之间，以在下框架接口和上框架接口之间传递张力负荷。
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公开(公告)号：WO2010138229A3
公开(公告)日：2011-02-17
申请号：PCT/US2010026465
申请日：2010-03-08
Applicant: SIKORSKY AIRCRAFT CORP , TONI DARRYL M , MCCARTHY MARY , BARR BRUCE H , STOBIECKI ANTHONY Z , SWIFT THOMAS , DZIEKONSKI THOMAS
Inventor： TONI DARRYL M , MCCARTHY MARY , BARR BRUCE H , STOBIECKI ANTHONY Z , SWIFT THOMAS , DZIEKONSKI THOMAS
Abstract: An external hook system for a rotary-wing aircraft includes a lower frame interface which accommodates longitudinal and lateral loads and an upper frame interface. A tension member is mountable between the lower frame interface and the upper frame interface to transfer tension loads between the lower frame interface and the upper frame interface.
Abstract translation: 用于旋转翼飞行器的外部钩系统包括容纳纵向和横向载荷的下部框架接口以及上部框架接口。 张紧构件可安装在下框架接口和上框架接口之间，以在下框架接口和上框架接口之间传递张力负荷。
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公开(公告)号：WO2009102372A3
公开(公告)日：2009-10-01
申请号：PCT/US2008084450
申请日：2008-11-23
Applicant: SIKORSKY AIRCRAFT CORP , TONI DARRYL M , BARR BRUCE H , SAUER JEFFREY G , BREMMER JONATHAN , RANALLI THOMAS , NORWID ALAN J
Inventor： TONI DARRYL M , BARR BRUCE H , SAUER JEFFREY G , BREMMER JONATHAN , RANALLI THOMAS , NORWID ALAN J
CPC classification number: B32B17/02 , B32B3/02 , B32B3/12 , B32B3/263 , B32B5/024 , B32B5/12 , B32B5/26 , B32B7/12 , B32B9/00 , B32B27/08 , B32B27/20 , B32B27/38 , B32B2260/021 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/718 , B32B2307/73 , B32B2307/734 , B32B2605/00 , B32B2605/18 , B64C1/06 , D03D15/0011 , D03D15/0016 , D10B2505/00 , Y10T428/249921 , Y10T442/30 , Y10T442/3431 , Y10T442/3447 , Y10T442/3463 , Y10T442/3488 , Y10T442/3496 , Y10T442/352
Abstract: A composite sandwich panel a first facing and a second facing over a core layer, the first and second facings having at least one fiberglass layer between an inner and an outer graphite layer.
Abstract translation: 一种复合夹层板，其面向第一和第二面向芯层，所述第一和第二面板在内部和外部石墨层之间具有至少一个玻璃纤维层。
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公开(公告)号：WO2009102372A2
公开(公告)日：2009-08-20
申请号：PCT/US2008/084450
申请日：2008-11-23
Applicant: SIKORSKY AIRCRAFT CORPORATION , TONI, Darryl, M. , BARR, Bruce, H. , SAUER, Jeffrey, G. , BREMMER, Jonathan , RANALLI, Thomas , NORWID, Alan, J.
Inventor： TONI, Darryl, M. , BARR, Bruce, H. , SAUER, Jeffrey, G. , BREMMER, Jonathan , RANALLI, Thomas , NORWID, Alan, J.
CPC classification number: B32B17/02 , B32B3/02 , B32B3/12 , B32B3/263 , B32B5/024 , B32B5/12 , B32B5/26 , B32B7/12 , B32B9/00 , B32B27/08 , B32B27/20 , B32B27/38 , B32B2260/021 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/718 , B32B2307/73 , B32B2307/734 , B32B2605/00 , B32B2605/18 , B64C1/06 , D03D15/0011 , D03D15/0016 , D10B2505/00 , Y10T428/249921 , Y10T442/30 , Y10T442/3431 , Y10T442/3447 , Y10T442/3463 , Y10T442/3488 , Y10T442/3496 , Y10T442/352
Abstract: A composite sandwich panel a first facing and a second facing over a core layer, the first and second facings having at least one fiberglass layer between an inner and an outer graphite layer.
Abstract translation: 一种复合夹层板，第一面层和第二面层覆盖核心层，第一和第二面层在内层和外层石墨层之间具有至少一个玻璃纤维层。
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