2.
    发明专利
    未知

    公开(公告)号:DE3234267A1

    公开(公告)日:1983-08-25

    申请号:DE3234267

    申请日:1982-09-15

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    3.
    发明专利
    未知

    公开(公告)号:DK410082A

    公开(公告)日:1983-08-11

    申请号:DK410082

    申请日:1982-09-14

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    4.
    发明专利
    未知

    公开(公告)号:IT8249118D0

    公开(公告)日:1982-09-15

    申请号:IT4911882

    申请日:1982-09-15

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    5.
    发明专利
    未知

    公开(公告)号:DK154105C

    公开(公告)日:1989-03-20

    申请号:DK410082

    申请日:1982-09-14

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    SPRING-ERECTED TELESCOPIC WING SUPPORT STRUCTURE

    公开(公告)号:CA1190433A

    公开(公告)日:1985-07-16

    申请号:CA411461

    申请日:1982-09-15

    Abstract: SPRING-ERECTED TELESCOPIC WING SUPPORT STRUCTURE A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    7.
    发明专利
    未知

    公开(公告)号:NO152064B

    公开(公告)日:1985-04-15

    申请号:NO823114

    申请日:1982-09-14

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    SPRING-ERECTED TELESCOPIC WING SUPPORT STRUCTURE

    公开(公告)号:GB2115116B

    公开(公告)日:1986-07-02

    申请号:GB8225046

    申请日:1982-09-02

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    9.
    发明专利
    未知

    公开(公告)号:NO823114L

    公开(公告)日:1983-08-11

    申请号:NO823114

    申请日:1982-09-14

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

    10.
    发明专利
    未知

    公开(公告)号:DK154105B

    公开(公告)日:1988-10-10

    申请号:DK410082

    申请日:1982-09-14

    Abstract: A wing support structure for a self-erecting collapsible wing includes a telescoping strut assembly including a leading strut and a trailing strut each pinned at an inner end to fixed pins on a base support structure and pinned to a common pivot pin at the outer end and each strut being telescoping for retraction to a colinear position and spring biased to an outward fully deployed position. Each strut includes inner and outer tubular strut members in which is confined a compression spring with the inner and outer members including an antirotation lock and an anticollapse lock.

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