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公开(公告)号：KR860000221B1
公开(公告)日：1986-03-15
申请号：KR820004172
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , CARISH JOHN A
Abstract: The launcher has a central support frame with attachment points that permit attachment to the aircraft or other launching platform. It has a central frame with a launch tube saddle-support assembly at each side of the frame, quick-detachable clamps and an alignment guide for quickly positioning and securing the launch tubes into position, auto connectors for automatically connecting the electronic control system and coolant gas to the launch tube assembly when the assembly is clamped into position. An aerodynamically shaped shell is used to enclose the support structure and the electronic control system.
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公开(公告)号：DK158024B
公开(公告)日：1990-03-12
申请号：DK409982
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：AU530447B2
公开(公告)日：1983-07-14
申请号：AU8843282
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：FR2520699B1
公开(公告)日：1986-10-10
申请号：FR8215512
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：DK158024C
公开(公告)日：1990-08-06
申请号：DK409982
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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Patent Agency Ranking
公开(公告)号：CA1172105A
公开(公告)日：1984-08-07
申请号：CA411466
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: AIRBORNE MISSILE LAUNCHER An airborne missile launcher for air launching of manportable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：DE3234268A1
公开(公告)日：1983-08-18
申请号：DE3234268
申请日：1982-09-15
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：NO159684C
公开(公告)日：1989-01-25
申请号：NO823113
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：NO823113L
公开(公告)日：1983-08-01
申请号：NO823113
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
Abstract: An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.
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公开(公告)号：NO823113A
公开(公告)日：1983-08-01
申请号：NO823113
申请日：1982-09-14
Applicant: GEN DYNAMICS CORP
Inventor： OLDHAM DELBERT J , KARISH JOHN A
CPC classification number: F41F3/06
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