公开(公告)号：KR860000220B1

公开(公告)日：1986-03-15

申请号：KR820004174

申请日：1982-09-15

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  ENGLIS RONALD T ,  WILLY RICHARD C

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

Abstract: The housing is for a self-erecting type fin (14) in a missile body. Space is provided for the retracted fin and there is also an opening (26) through which the fin can emerge. Over this opening is a cover which can be freed. A movable lock is provided to hold the cover over the opening. The space and lock extend along the axis of the missile body. The lock has a number of pivots that support a cover plate with lugs fitting the pivots.

公开(公告)号：KR860001011B1

公开(公告)日：1986-07-26

申请号：KR820004173

申请日：1982-02-10

Applicant: GEN DYNAMICS CORP

Inventor： DITOMMASO ANTHONY ,  ENGLIS RONALD T ,  WALLY RICHARD C ,  RENDA RAMOND J

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

Abstract: The strut system is extensible and is used for a self positioning fin. There are two stays (32, 40), one on the leading edge and one on the trailing edge. Both have a lower telescopic tube which pivots on its lower end on a fixed pivot (28, 30). There is also an upper telescopic tube, moving in the lower one, which is pivoted on a common pivot (36). Inside both types of struts are compression springs (38, 44). The struts are aligned by a spindle (34, 42) and slot on one of them. The spring is fully compressed when the struts are folded.

公开(公告)号：NO823114A

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

CPC classification number: F42B10/146

公开(公告)号：DK410182A

公开(公告)日：1983-08-11

申请号：DK410182

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 ,  F42B

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：DK154105C

公开(公告)日：1989-03-20

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 ,  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：CA1190433A

公开(公告)日：1985-07-16

申请号：CA411461

申请日：1982-09-15

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 ,  F42B13/00

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.

公开(公告)号：NO152064B

公开(公告)日：1985-04-15

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 ,  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：GB2115117A

公开(公告)日：1983-09-01

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：DK154105B

公开(公告)日：1988-10-10

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 ,  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：HK92686A

公开(公告)日：1986-12-12

申请号：HK92686

申请日：1986-12-04

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 ,  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.