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公开(公告)号：NO152064C
公开(公告)日：1985-07-24
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
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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公开(公告)号：GB2115116A
公开(公告)日：1983-09-01
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
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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公开(公告)号：NO823115L
公开(公告)日：1983-08-11
申请号：NO823115
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
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.
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公开(公告)号：DK153183C
公开(公告)日：1988-11-14
申请号：DK410182
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
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.
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公开(公告)号：DK153183B
公开(公告)日：1988-06-20
申请号：DK410182
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
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.
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Patent Agency Ranking
公开(公告)号：HK36588A
公开(公告)日：1988-05-27
申请号：HK36588
申请日：1988-05-19
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
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.
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公开(公告)号：CA1190434A
公开(公告)日：1985-07-16
申请号：CA411465
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
Abstract: WING HOUSING AND COVER RELEASE ASSEMBLY FOR SELF-ERECTING WING A self-erecting collapsible wing for an airframe includes a telescoping strut assembly including a leading strut and a trailing strut each pivoted at an inner end to fixed pins 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 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.
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公开(公告)号：NO150820B
公开(公告)日：1984-09-10
申请号：NO823115
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
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.
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公开(公告)号：DE3234267A1
公开(公告)日：1983-08-25
申请号：DE3234267
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C , RENDA RAMON J
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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公开(公告)号：NO823115A
公开(公告)日：1983-08-11
申请号：NO823115
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： DITOMMASO ANTHONY , INGLIS RONALD T , WORLEY RICHARD C
CPC classification number: F42B10/146 , E05C9/02
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