公开(公告)号：DK410082A

公开(公告)日：1983-08-11

申请号：DK410082

申请日：1982-09-14

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C ,  RENDA RAMON J

IPC: B64C3/56 ,  B64C5/12 ,  F42B10/14 ,  F42B15/00 ,  F42B

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.

公开(公告)号：GB2115116B

公开(公告)日：1986-07-02

申请号：GB8225046

申请日：1982-09-02

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C ,  RENDA RAMON J

IPC: B64C3/56 ,  B64C5/12 ,  F42B10/14 ,  F42B15/00 ,  F42B13/32

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.

公开(公告)号：GB2115117B

公开(公告)日：1985-11-06

申请号：GB8225459

申请日：1982-09-07

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C

IPC: B64C3/56 ,  B64C5/10 ,  E05C9/02 ,  F42B10/14 ,  F42B15/00 ,  F42B13/32

Abstract: A self-erecting collapsible wing for an airframe includes a telescoping strut assembly, Figure 4, including a leading strut 32, 34 and a trailing strut 40, 42 each pivoted at an inner end to fixed pins 28, 30 on a base support structure of a wing housing within a slot in the airframe for retraction to a colinear position within the housing and spring biased to an outward fully deployed position. A releasable cover 26, Figure 7, conforming to the curvature of the airframe is normally latched in position over the slot when the wing is in the collapsed position within the wing housing and is jettisoned to permit automatic self-erection of the wing.

公开(公告)号：NO150820C

公开(公告)日：1985-01-09

申请号：NO823115

申请日：1982-09-14

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C

IPC: B64C3/56 ,  B64C5/10 ,  E05C9/02 ,  F42B10/14 ,  F42B15/00 ,  F42B13/32

Abstract: A self-erecting collapsible wing for an airframe includes a telescoping strut assembly, Figure 4, including a leading strut 32, 34 and a trailing strut 40, 42 each pivoted at an inner end to fixed pins 28, 30 on a base support structure of a wing housing within a slot in the airframe for retraction to a colinear position within the housing and spring biased to an outward fully deployed position. A releasable cover 26, Figure 7, conforming to the curvature of the airframe is normally latched in position over the slot when the wing is in the collapsed position within the wing housing and is jettisoned to permit automatic self-erection of the wing.

公开(公告)号：DE3234269A1

公开(公告)日：1983-08-25

申请号：DE3234269

申请日：1982-09-15

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C

IPC: B64C3/56 ,  B64C5/10 ,  E05C9/02 ,  F42B10/14 ,  F42B15/00 ,  F42B13/32

Abstract: A self-erecting collapsible wing for an airframe includes a telescoping strut assembly, Figure 4, including a leading strut 32, 34 and a trailing strut 40, 42 each pivoted at an inner end to fixed pins 28, 30 on a base support structure of a wing housing within a slot in the airframe for retraction to a colinear position within the housing and spring biased to an outward fully deployed position. A releasable cover 26, Figure 7, conforming to the curvature of the airframe is normally latched in position over the slot when the wing is in the collapsed position within the wing housing and is jettisoned to permit automatic self-erection of the wing.

公开(公告)号：NO823114L

公开(公告)日：1983-08-11

申请号：NO823114

申请日：1982-09-14

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C ,  RENDA RAMON J

IPC: B64C5/12 ,  B64C3/56 ,  F42B10/14 ,  F42B15/00 ,  F42B

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.

公开(公告)号：AU530407B2

公开(公告)日：1983-07-14

申请号：AU8843182

申请日：1982-09-18

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  INGLIS RONALD T ,  WORLEY RICHARD C

IPC: B64C3/56 ,  B64C5/12 ,  F42B10/14 ,  F42B15/00 ,  F42B15/10

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.