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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：NO142547B
公开(公告)日：1980-05-27
申请号：NO772180
申请日：1977-06-20
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE
IPC: F41G20060101 , F42B15/18
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公开(公告)号：FR2396947A1
公开(公告)日：1979-02-02
申请号：FR7721144
申请日：1977-07-08
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE
Abstract: A missile is disclosed on which constant burning thrust reaction motors are provided integral with the tail panels of the missile to enhance the effect thereof, particularly during the boost phase of flight. The motors provide thrust along the chord of the tail panel and are moved about the axis of rotation of the tail panel by the servo motor associated therewith. The servo motors are activated by central missile control circuitry.
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公开(公告)号：AU2628677A
公开(公告)日：1979-01-04
申请号：AU2628677
申请日：1977-06-21
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE
Abstract: A missile is disclosed on which constant burning thrust reaction motors are provided integral with the tail panels of the missile to enhance the effect thereof, particularly during the boost phase of flight. The motors provide thrust along the chord of the tail panel and are moved about the axis of rotation of the tail panel by the servo motor associated therewith. The servo motors are activated by central missile control circuitry.
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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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Patent Agency Ranking
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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公开(公告)号：FR2465644A1
公开(公告)日：1981-03-27
申请号：FR8015478
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：CA1078253A
公开(公告)日：1980-05-27
申请号：CA282157
申请日：1977-07-06
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE
Abstract: A missile is disclosed on which constant burning thrust reaction motors are provided integral with the tail panels of the missile to enhance the effect thereof, particularly during the boost phase of flight. The motors provide thrust along the chord of the tail panel and are moved about the axis of rotation of the tail panel by the servo motor associated therewith. The servo motors are activated by central missile control circuitry.
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公开(公告)号：NO772180L
公开(公告)日：1978-12-21
申请号：NO772180
申请日：1977-06-20
Applicant: GEN DYNAMICS CORP
Inventor： MAUDAL INGE
IPC: F41G20060101 , F41G
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