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公开(公告)号：DK150259C
公开(公告)日：1988-01-25
申请号：DK299680
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
IPC: F42B10/14 , F42B15/01 , B64C3/56 , F42B13/32 , F42B15/053
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：NO146828B
公开(公告)日：1982-09-06
申请号：NO802088
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：NO802088L
公开(公告)日：1981-03-25
申请号：NO802088
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：DK150259B
公开(公告)日：1987-01-19
申请号：DK299680
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：NO802088A
公开(公告)日：1981-03-25
申请号：NO802088
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
CPC classification number: F42B10/146
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Patent Agency Ranking
公开(公告)号：NO146828C
公开(公告)日：1982-12-15
申请号：NO802088
申请日：1980-07-11
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：IT8049210D0
公开(公告)日：1980-07-10
申请号：IT4921080
申请日：1980-07-10
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：IT1218440B
公开(公告)日：1990-04-19
申请号：IT4921080
申请日：1980-07-10
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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公开(公告)号：CH636956A5
公开(公告)日：1983-06-30
申请号：CH522880
申请日：1980-07-08
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
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公开(公告)号：CA1146409A
公开(公告)日：1983-05-17
申请号：CA355200
申请日：1980-07-02
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE , WEDERTZ LARRY D , YOST KENNETH M
Abstract: DOUBLE FABRIC, RETRACTABLE SELF-ERECTING WING FOR MISSILE A retractable, self-erecting wing for a low speed missile, having a double walled fabric body held in extended position by spring loaded struts, the fabric enclosing an air pocket which acts as a damper to prevent the wing from fluttering under certain aerodynamic conditions. The wing is extended by a hinged strut structure and folds into a very small space adjacent the outer wall of the missile body. The structure enables a large area wing to be stowed in a minimum of space so that the maximum internal volume is available for payload. In stowed condition the wing is completely enclosed in the body for minimum drag during any high speed portion of the missile flight, multiple wings being released when required by a simple mechanism.
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