US3754497A - Transporting and firing chest for self-propelled projectiles - Google Patents
Transporting and firing chest for self-propelled projectiles Download PDFInfo
- Publication number
- US3754497A US3754497A US00166110A US3754497DA US3754497A US 3754497 A US3754497 A US 3754497A US 00166110 A US00166110 A US 00166110A US 3754497D A US3754497D A US 3754497DA US 3754497 A US3754497 A US 3754497A
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- chest
- firing
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- projectiles
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Links
- 238000010304 firing Methods 0.000 title claims abstract description 36
- 239000000463 material Substances 0.000 claims abstract description 9
- 239000004020 conductor Substances 0.000 claims description 2
- 210000000038 chest Anatomy 0.000 description 57
- 238000009413 insulation Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 229920002635 polyurethane Polymers 0.000 description 3
- 239000004814 polyurethane Substances 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 239000000945 filler Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012856 packing Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000004794 expanded polystyrene Substances 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 235000011837 pasties Nutrition 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
- F41F3/0455—Bazookas
Definitions
- ABSTRACT A transporting and firing chest for self-propelled projectiles comprising guide tubes for the projectiles mounted in a support frame and fuses and firing connections for the projectiles.
- the said frame is rigidly attached to at least one member for fixing the chest to a support, a filling of light semi-rigid material is disposed in the empty spaces between said tubes and between these latter and a tubular external envelope constituting the lateral walls of the chest, so as to insulate mechanically and thermally the support frame and the guide tubes with respect to the external envelope of the chest.
- the present invention has as object the provision of a transporting and firing chest for self-propelled projectiles comprising projectile guide tubes mounted in a supporting frame and fuses and firing connections for projectiles.
- This chest is characterized in that said frame is rigidly attached to at least one member for fixing the chest to a support and in that a filling oflight semi-rigid material is disposed in the empty spaces between said tubes and between these latter and an external tubular envelope constituting the lateral walls of the chest.
- FIG. 1 is a general view of the chest in longitudinal section along I I of FIG. 2,
- FIG. 2 is a transverse sectional view along II II of FIG. 1,
- FIGS. 3 and 4 represent schematically chests mounted on a suitable aiming device, seen respectively from the side and from the rear;
- FIG. 5 is a partial view to a larger scale in longitudinal section of the chest of FIGS. 1 and 2, showing its fixing to the aiming device of FIGS. 3 and 4;
- FIG. 6 is a partial longitudinal section of the chest of FIG. 1 showing the firing connections for the fuse of one of the projectiles;
- FIG. 7 is a partial transverse section similar to FIG. 2, showing the firing connections of the projectiles assembly contained in the chest;
- FIG. 8 is a general view of the variant of the chest in longitudinal section along VIII VIII of FIG. 9,
- FIG. 9 is a transverse section along IX IX of FIG.
- FIGS. 10 and 11 show an aiming support for the chest variant shown in FIGS. 8 and 9 respectively, seen from the side and from above;
- FIG. 12 is a partial view to a larger scale in longitudinal section of the chest variant of FIGS. 8 and 9, showing its rear fixing to the firing device of the aiming support of FIGS. 10 and 11.
- FIGS. 1, 6, 8 the chests are shown on the drawings with projectile inside them (FIGS. 1, 6, 8) either mounted on a suitable aiming support or on elements of such a support (FIGS. 3 5, and 9 12) but it is to be understood that the subject of the invention is the chest itself.
- the transporting and firing chest shown in FIGS. 1 and 2 comprises an external envelope 1, preferably of metal, of tubular form and shaped in cross-section as a square with rounded comers.
- a rigid supporting frame comprising three metal elements 2, preferably mounted transversally to said external envelope 1 respectively at its ends and at its centre and four guide tubes 3 each mounted in three successive coaxial orifices 4 possessed by the elements 2 of the frame.
- the guide tubes 3 are constructed of cardboard, plastic or plasticised cloth, for example and possess arresting stops 5 intended to prevent any backward movement of the projectile 6 which they are designed to con tain as well as a retaining device 7 for holding the projectile 6 by its rear end, attached to the rear frame element, and designed to prevent any forward movement of the projectile 6.
- the frame elements 2 also each possess a central orifice 8, in which is mounted a rigid tube 9, preferably of metal, designed for mounting the chest on a support mandrel 10 when the chest is placed in the firing position.
- the empty spaces between said tubes 8 and 9, the frame element 2 and the envelope 1 of the chest are filled with a light semi-rigid packing material 11, preferably made of expanded polyurethane.
- the rear frame element also possesses in its lower part an orifice 12, in which is mounted an electrical plug 13, to which are connected electrical firing conections 14 for the electrical fuses 15 of the projectile. These electrical connections 14 are also partially buried in the expanded polyurethane material 11.
- the front and rear frame elements 2 are also covered with a removable filler plate 16, for example of expanded polystyrene, against which is applied the bottom of the covers 17, the edges of which rest against the open ends of the external envelope 1 of the chest.
- a removable filler plate 16 for example of expanded polystyrene
- the locking of these covers 17 on the ends of the envelope l is ensured by a bar 18, threaded at its ends, disposed in the rigid tube 9.
- the threaded ends of the rod 18 penetrate into orifices opposite the bases of the two covers 17 and wing nuts 19 are screwed onto these threaded ends of the bar 18 to ensure the locking of said covers 17 onto the ends of the envelope 1.
- the electrical connections 14 of the chest are connected firstly to the plug 13 and secondly to four plugs 21, one for each projectile 6, into which are inserted male terminals with which the ends of the respective electrical connections 22 of each of the electrical fuses 15 of the projectiles are furnished.
- This plugging in of the electrical connections 22 of each of said electrical fuses 15 into the respective plugs 21 may thus be easily carried out during the placing of the projectiles 6 into the chest.
- the rigid tube 9 may comprise conducting rings connected by electrical connections to the fuses 15.
- the projectiles may be plugged in automatically, by the placing of the chest on the mandrel of the support stand which would carry corresponding conducting rings, to the firing device which could be carried by this support stand.
- FIGS. 3 and 4 show standard tripods which may be furnished with aiming devices and which each possess firstly three supporting mandrels 10 designed to engage respectively into the rigid tube 9 of three chests and three terminals 23 designed to engage respectively in the electrical plug 13 of each of these three chests. These terminals 23 are connected secondly to one or more standard firing controls (not shown).
- the rear frame element 2 of each chest preferably possesses a catch 24 designed to engage a pawl 25 possessed by the rear end of the mandrel 10.
- the mandrel 10 may possess a locking pawl acting in conjunction with a shape formed on the tube 9 to lock the chest onto the mandrel.
- the mandrel 10 could be sealed in a fixed firing position on theedge of a loophole of a fortification or in a mobile firing position on a military vehicle for example.
- FIGS. 8 and 9 Such a variant is shown in FIGS. 8 and 9, where two slides 35 and 36 rigidly attached to the median frame member 2 are provided on the lower external face of the envelope 1. These slides 35 and 36 are designed to engage onto two studs 27 and 28 mounted on the plate 29 of an aiming support, of the type shown in FIGS. 10 and 11.
- the locking catch 24 of the rear frame element 2 of the chest will be provided on the upper edge of the orifice 12 for the plug 13, and the pawl for locking the chest onto the plate will be provided on the firing terminal 23 which should therefore be rigidly attached to the rear edge of the support plate.
- the position and the form of the frame elements 2 may also be modified, provided that they form a rigid assembly with the guide tubes and that at least one of them is rigidly attached to a fixing member for attaching the chest to a support.
- thermal and mechanical insulation is obtained of the assembly comprising the support frame and the guide tubes for the projectiles, with respect to the external envelope of the chest.
- the mechanical insulation makes it possible to prevent the projectiles from being subjected to violent vibrations or shocks, even if the transporting and firing chest is dropped or otherwise roughly handled.
- the chest is designed in such a way as to offer sufficient resistance to shocks of any type, as well as to ensure effective protection for the ammunition and for all the fixing members, electrical connections, and closure members, incorporated within its own volume. All projecting external parts are avoided.
- This design makes it possible, in case of shocks, to prevent any transmission of deformations to the principal members of the chest or to the projectiles, and also to prevent any adverse effect upon the firing properties.
- the thermal insulation thus obtained is considerable, since it enables the variations in temperature to which the projectiles are subjected to be reduced; this is important in view of the changes that take place in the characteristics of explosives and propellants, as well as, in some cases, in the electrical apparatus, as a function of temperature.
- this firing chest is preferably used in conjunction 'with the tripod support described in Pat. No. (Swiss Patent Application No. 11.827/).
- Transporting and firing chest for self-propelled projectiles having electrical firing devices comprising guide tubes for the projectiles, a rigid support frame in which said guide tubes are mounted, said frame comprising a plurality of rigid plates transverse to the tubes and having openings in which the tubes are mounted, means fixedly interconnecting said plates in spaced parallel relationship, firing connections for the projectiles carried by said chest, said firing connections comprising at least one female plug carried by one of said plates and connected by conductors to the firing device of each projectile, at least one member to which at least one of said plates is rigidly attached for fixing the chest to a support, an external tubular envelope surrounding and spaced outwardly from the tubes and plates, a filling of light semi-rigid material disposed between the tubes and plates on the one hand and said envelope on the other hand and surrounding said female plug, the connection between said plates and said at least one member and said support supporting said plates and tubes, said plates and tubes supporting said filling and said envelope, so that damage to said envelope and said filling does not affect said connection.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A transporting and firing chest for self-propelled projectiles comprising guide tubes for the projectiles mounted in a support frame and fuses and firing connections for the projectiles. The said frame is rigidly attached to at least one member for fixing the chest to a support, a filling of light semi-rigid material is disposed in the empty spaces between said tubes and between these latter and a tubular external envelope constituting the lateral walls of the chest, so as to insulate mechanically and thermally the support frame and the guide tubes with respect to the external envelope of the chest.
Description
ite
Rusbach States Patent [191 Aug. 28, 1973 1 TRANSPORTING AND FIRING CHEST FOR SELF-PROPELLED PROJECTILES [75] Inventor: Maurlce Rusbach, Vernier-Geneva,
Switzerland [30] Foreign Application Priority Data 3,167,278 1/1965 Roberge 89/1.8l6 X 2,961,927 11/1960 Dufour 89/1.8l6 2,972,933 2/1961 Guthrie et al.... 89/l.8l7 X 3,089,390 5/1963 Wilson 89/1.8l9 X 3,194,119 7/1965 Robert et 89/l.8l4
3,357,305 12/1967 Clutz et a]. 89/1.816 X 3,495,497 2/1970 Stangl et a1. 89/1.8l5
Primary Examiner-Samuel W. Engle Attorney-Young & Thompson [5 7] ABSTRACT A transporting and firing chest for self-propelled projectiles comprising guide tubes for the projectiles mounted in a support frame and fuses and firing connections for the projectiles. The said frame is rigidly attached to at least one member for fixing the chest to a support, a filling of light semi-rigid material is disposed in the empty spaces between said tubes and between these latter and a tubular external envelope constituting the lateral walls of the chest, so as to insulate mechanically and thermally the support frame and the guide tubes with respect to the external envelope of the chest.
1 Claim, 12 Drawing Figures PATENTEBAme ms 3.754497 sum 3 0F 6 FIG. 4
"I23 FIG. 5
PATENTED M1828 I975 SHEET Q 0F 6 FIG.
TRANSPORTING AND FIRING CHEST FOR SELF-PROPELLED PROJECTILES The present invention has as object the provision of a transporting and firing chest for self-propelled projectiles comprising projectile guide tubes mounted in a supporting frame and fuses and firing connections for projectiles.
This chest is characterized in that said frame is rigidly attached to at least one member for fixing the chest to a support and in that a filling oflight semi-rigid material is disposed in the empty spaces between said tubes and between these latter and an external tubular envelope constituting the lateral walls of the chest.
The attached drawings represent by way of example various embodiments of transporting and firing chests in accordance with the invention.
FIG. 1 is a general view of the chest in longitudinal section along I I of FIG. 2,
FIG. 2 is a transverse sectional view along II II of FIG. 1,
FIGS. 3 and 4 represent schematically chests mounted on a suitable aiming device, seen respectively from the side and from the rear;
FIG. 5 is a partial view to a larger scale in longitudinal section of the chest of FIGS. 1 and 2, showing its fixing to the aiming device of FIGS. 3 and 4;
FIG. 6 is a partial longitudinal section of the chest of FIG. 1 showing the firing connections for the fuse of one of the projectiles;
FIG. 7 is a partial transverse section similar to FIG. 2, showing the firing connections of the projectiles assembly contained in the chest;
FIG. 8 is a general view of the variant of the chest in longitudinal section along VIII VIII of FIG. 9,
FIG. 9 is a transverse section along IX IX of FIG.
FIGS. 10 and 11 show an aiming support for the chest variant shown in FIGS. 8 and 9 respectively, seen from the side and from above;
FIG. 12 is a partial view to a larger scale in longitudinal section of the chest variant of FIGS. 8 and 9, showing its rear fixing to the firing device of the aiming support of FIGS. 10 and 11.
In order to assist in a better understanding of the invention, the chests are shown on the drawings with projectile inside them (FIGS. 1, 6, 8) either mounted on a suitable aiming support or on elements of such a support (FIGS. 3 5, and 9 12) but it is to be understood that the subject of the invention is the chest itself.
The transporting and firing chest shown in FIGS. 1 and 2 comprises an external envelope 1, preferably of metal, of tubular form and shaped in cross-section as a square with rounded comers. A rigid supporting frame, comprising three metal elements 2, preferably mounted transversally to said external envelope 1 respectively at its ends and at its centre and four guide tubes 3 each mounted in three successive coaxial orifices 4 possessed by the elements 2 of the frame.
The guide tubes 3 are constructed of cardboard, plastic or plasticised cloth, for example and possess arresting stops 5 intended to prevent any backward movement of the projectile 6 which they are designed to con tain as well as a retaining device 7 for holding the projectile 6 by its rear end, attached to the rear frame element, and designed to prevent any forward movement of the projectile 6. The frame elements 2 also each possess a central orifice 8, in which is mounted a rigid tube 9, preferably of metal, designed for mounting the chest on a support mandrel 10 when the chest is placed in the firing position.
The empty spaces between said tubes 8 and 9, the frame element 2 and the envelope 1 of the chest are filled with a light semi-rigid packing material 11, preferably made of expanded polyurethane.
The rear frame element also possesses in its lower part an orifice 12, in which is mounted an electrical plug 13, to which are connected electrical firing conections 14 for the electrical fuses 15 of the projectile. These electrical connections 14 are also partially buried in the expanded polyurethane material 11.
The front and rear frame elements 2 are also covered with a removable filler plate 16, for example of expanded polystyrene, against which is applied the bottom of the covers 17, the edges of which rest against the open ends of the external envelope 1 of the chest. The locking of these covers 17 on the ends of the envelope l is ensured by a bar 18, threaded at its ends, disposed in the rigid tube 9. The threaded ends of the rod 18 penetrate into orifices opposite the bases of the two covers 17 and wing nuts 19 are screwed onto these threaded ends of the bar 18 to ensure the locking of said covers 17 onto the ends of the envelope 1.
It will be noted that these ends tripod, the external envelope 1 of the chest are furnished with a flexible, the edge packing 20 of rubber for example extending beyond the junction of the edges of the covers 17 and of said ends of the external envelope of the chest.
As shownin FIGS. 6 and 7, the electrical connections 14 of the chest are connected firstly to the plug 13 and secondly to four plugs 21, one for each projectile 6, into which are inserted male terminals with which the ends of the respective electrical connections 22 of each of the electrical fuses 15 of the projectiles are furnished. This plugging in of the electrical connections 22 of each of said electrical fuses 15 into the respective plugs 21 may thus be easily carried out during the placing of the projectiles 6 into the chest.
It should be noted that in this embodiment of the chest, the rigid tube 9 may comprise conducting rings connected by electrical connections to the fuses 15.
Thus the projectiles may be plugged in automatically, by the placing of the chest on the mandrel of the support stand which would carry corresponding conducting rings, to the firing device which could be carried by this support stand.
FIGS. 3 and 4 show standard tripods which may be furnished with aiming devices and which each possess firstly three supporting mandrels 10 designed to engage respectively into the rigid tube 9 of three chests and three terminals 23 designed to engage respectively in the electrical plug 13 of each of these three chests. These terminals 23 are connected secondly to one or more standard firing controls (not shown).
As shown in FIG. 5, the rear frame element 2 of each chest preferably possesses a catch 24 designed to engage a pawl 25 possessed by the rear end of the mandrel 10.
In one variant, the mandrel 10 may possess a locking pawl acting in conjunction with a shape formed on the tube 9 to lock the chest onto the mandrel.
In order to place a chest loaded with projectiles into the firing position, it is therefore necessary only to uncrew one of the two wing nuts 19 holding the two covers 17 of the chest in place, to remove the two covers and the bar 18, to engage the rear end of the tube 9 on a mandrel 10 which forms a part of a support and/ or aiming device ofsome kind, and to engage the terminal 23 of a firing control in the plug 13 of the chest. Once all the projectiles of the chest have been fired, it is necessary only to press on the trip lever 26 of the pawl 25 to free the empty chest and to replace it by a chest filled with projectiles, in order to be able to continue to fire.
Instead of being mounted on a tropod, the mandrel 10 could be sealed in a fixed firing position on theedge of a loophole of a fortification or in a mobile firing position on a military vehicle for example.
Numerous other variants for fixing a chest onto an aiming support may also be envisaged involving modifications in detail to be applied to the chest itself.
Such a variant is shown in FIGS. 8 and 9, where two slides 35 and 36 rigidly attached to the median frame member 2 are provided on the lower external face of the envelope 1. These slides 35 and 36 are designed to engage onto two studs 27 and 28 mounted on the plate 29 of an aiming support, of the type shown in FIGS. 10 and 11.
In this case the locking catch 24 of the rear frame element 2 of the chest will be provided on the upper edge of the orifice 12 for the plug 13, and the pawl for locking the chest onto the plate will be provided on the firing terminal 23 which should therefore be rigidly attached to the rear edge of the support plate.
Numerous other modifications may also be applied to the chest described. For example its external envelope could be formed of stratified synthetic resin or any other suitable material. Numerous other variants of the front and rear covers 17 may be imagined, as also many variants of the locking device for attaching the covers 17 onto the ends of the envelope 1.
The position and the form of the frame elements 2 may also be modified, provided that they form a rigid assembly with the guide tubes and that at least one of them is rigidly attached to a fixing member for attaching the chest to a support.
Instead of the expanded polyurethane filler, the use of any other semi-rigid material which is easy to introduce, preferably in the liquid or pasty state, into the free spaces between the guide tubes and the external wall of the chest may be envisaged.
It will be noted that in all the embodiments described, thermal and mechanical insulation is obtained of the assembly comprising the support frame and the guide tubes for the projectiles, with respect to the external envelope of the chest.
The mechanical insulation makes it possible to prevent the projectiles from being subjected to violent vibrations or shocks, even if the transporting and firing chest is dropped or otherwise roughly handled. The chest is designed in such a way as to offer sufficient resistance to shocks of any type, as well as to ensure effective protection for the ammunition and for all the fixing members, electrical connections, and closure members, incorporated within its own volume. All projecting external parts are avoided.
This design makes it possible, in case of shocks, to prevent any transmission of deformations to the principal members of the chest or to the projectiles, and also to prevent any adverse effect upon the firing properties.
The thermal insulation thus obtained is considerable, since it enables the variations in temperature to which the projectiles are subjected to be reduced; this is important in view of the changes that take place in the characteristics of explosives and propellants, as well as, in some cases, in the electrical apparatus, as a function of temperature.
The bringing into firing position, utilisation and engagement of these firing chests are similar to those described with reference to the equipment forming the subject of Swiss Pat. No. 498,359.
Finally, this firing chest is preferably used in conjunction 'with the tripod support described in Pat. No. (Swiss Patent Application No. 11.827/).
I claim:
1. Transporting and firing chest for self-propelled projectiles having electrical firing devices, comprising guide tubes for the projectiles, a rigid support frame in which said guide tubes are mounted, said frame comprising a plurality of rigid plates transverse to the tubes and having openings in which the tubes are mounted, means fixedly interconnecting said plates in spaced parallel relationship, firing connections for the projectiles carried by said chest, said firing connections comprising at least one female plug carried by one of said plates and connected by conductors to the firing device of each projectile, at least one member to which at least one of said plates is rigidly attached for fixing the chest to a support, an external tubular envelope surrounding and spaced outwardly from the tubes and plates, a filling of light semi-rigid material disposed between the tubes and plates on the one hand and said envelope on the other hand and surrounding said female plug, the connection between said plates and said at least one member and said support supporting said plates and tubes, said plates and tubes supporting said filling and said envelope, so that damage to said envelope and said filling does not affect said connection.
Claims (1)
1. Transporting and firing chest for self-propelled projectiles having electrical firing devices, comprising guide tubes for the projectiles, a rigid support frame in which said guide tubes are mounted, said frame comprising a plurality of rigid plates transverse to the tubes and having openings in which the tubes are mounted, means fixedly interconnecting said plates in spaced parallel relationship, firing connections for the projectiles carried by said chest, said firing connections comprising at least one female plug carried by one of said plates and connected by conductors to the firing device of each projectile, at least one member to which at least one of said plates is rigidly attached for fixing the chest to a support, an external tubular envelope surrounding and spaced outwardly from the tubes and plates, a filling of light semi-rigid material disposed between the tubes and plates on the one hand and said envelope on the other hand and surrounding said female plug, the connection between said plates and said at least one member and said support supporting said plates and tubes, said plates and tubes supporting said filling and said envelope, so that damage to said envelope and said filling does not affect said connection.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH1182570A CH528058A (en) | 1970-08-06 | 1970-08-06 | Transport and firing case for self-propelled projectiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3754497A true US3754497A (en) | 1973-08-28 |
Family
ID=4377246
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00166110A Expired - Lifetime US3754497A (en) | 1970-08-06 | 1971-07-26 | Transporting and firing chest for self-propelled projectiles |
Country Status (15)
| Country | Link |
|---|---|
| US (1) | US3754497A (en) |
| JP (1) | JPS5632559B1 (en) |
| AT (1) | AT320476B (en) |
| BE (1) | BE770706A (en) |
| CA (1) | CA934197A (en) |
| CH (1) | CH528058A (en) |
| DE (1) | DE2138807C3 (en) |
| FI (1) | FI56447C (en) |
| FR (1) | FR2103870A5 (en) |
| GB (1) | GB1329514A (en) |
| IL (1) | IL37394A (en) |
| IT (1) | IT939753B (en) |
| NL (1) | NL163622C (en) |
| SE (1) | SE389392B (en) |
| ZA (1) | ZA714996B (en) |
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| US3981224A (en) * | 1975-07-11 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Army | Missile trans porter-launcher |
| US3988961A (en) * | 1975-08-08 | 1976-11-02 | The United States Of America As Represented By The Secretary Of The Army | Integrated rocket shipping container and launcher |
| US4007660A (en) * | 1975-09-29 | 1977-02-15 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defense | Rocket retention and ignition assembly |
| US4296669A (en) * | 1979-05-25 | 1981-10-27 | The United States Of America As Represented By The Secretary Of The Army | Rocket tube launcher with cast-in place tube support bulkhead |
| US4604939A (en) * | 1984-08-20 | 1986-08-12 | The United States Of America As Represented By The Secretary Of The Army | Lightweight composite launcher pod |
| US4719839A (en) * | 1985-02-14 | 1988-01-19 | Werkzeugmaschinenfabrik | Rotary storage magazine |
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| US5115711A (en) * | 1991-03-25 | 1992-05-26 | Fmc Corporation | Missile canister and method of fabrication |
| US5327809A (en) * | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
| US5413024A (en) * | 1993-07-16 | 1995-05-09 | Alliant Techsystems Inc. | Disposable flare dispenser magazine for infrared decoy flares |
| US6142055A (en) * | 1998-06-17 | 2000-11-07 | United Defense, L.P. | Matrix gun system |
| US6311604B1 (en) * | 1990-04-30 | 2001-11-06 | Raytheon Company | Protective missile launch tube enclosure |
| US20050242230A1 (en) * | 2002-06-28 | 2005-11-03 | Marc Vallier | Adapter device for projectile fired from a launching tube |
| US8789453B1 (en) * | 2013-02-21 | 2014-07-29 | The United States Of America As Represented By The Secretary Of The Navy | Dispenser pod |
| ES2585603A1 (en) * | 2015-07-01 | 2016-10-06 | Anortec, Sl | Adjustable mount for single-use launcher tube light launcher (Machine-translation by Google Translate, not legally binding) |
| CN114543583A (en) * | 2022-04-28 | 2022-05-27 | 成都航天万欣科技有限公司 | Precision adjusting device and method for storage and transportation launching box |
| USD956712S1 (en) * | 2020-07-13 | 2022-07-05 | Frog Design Inc. | Wireless headphone |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2441825A1 (en) * | 1978-11-16 | 1980-06-13 | British Aerospace | MISSILE LAUNCHING DEVICE |
| AT385593B (en) * | 1984-11-30 | 1988-04-25 | Gibler Ferdinand Dipl Ing Dr | SHOT DEVICE |
| IL94671A0 (en) * | 1990-06-08 | 1991-04-15 | Israel State | Pack and launcher for pyrotechnic grenades |
| EP1873474B1 (en) * | 2006-06-30 | 2009-08-12 | Saab Ab | Dispenser arrangement for discharging countermeasure means |
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| US2936676A (en) * | 1953-11-27 | 1960-05-17 | Robert Roger Aime | System for releasing objects suspended from aircraft |
| US2961927A (en) * | 1955-10-04 | 1960-11-29 | Brevets Aero Mecaniques | Rocket launching systems |
| US2972933A (en) * | 1957-12-23 | 1961-02-28 | Gen Dynamics Corp | Missile hand launching system |
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| US3495497A (en) * | 1967-05-19 | 1970-02-17 | Bolkow Gmbh | Coupling member for a missile firing and guiding device |
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| GB917707A (en) * | 1958-09-23 | 1963-02-06 | English Electric Co Ltd | Improvements in and relating to storage and packing containers |
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| AT248290B (en) * | 1963-10-16 | 1966-07-25 | Bofors Ab | Device for fastening a projectile in a housing |
| NL6411455A (en) * | 1963-10-16 | 1965-04-20 |
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- 1970-08-06 CH CH1182570A patent/CH528058A/en not_active IP Right Cessation
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1971
- 1971-07-22 GB GB3437871A patent/GB1329514A/en not_active Expired
- 1971-07-23 NL NL7110165.A patent/NL163622C/en not_active IP Right Cessation
- 1971-07-26 US US00166110A patent/US3754497A/en not_active Expired - Lifetime
- 1971-07-27 IL IL37394A patent/IL37394A/en unknown
- 1971-07-27 ZA ZA714996A patent/ZA714996B/en unknown
- 1971-07-30 BE BE770706A patent/BE770706A/en unknown
- 1971-07-30 CA CA119596A patent/CA934197A/en not_active Expired
- 1971-08-02 FR FR7128281A patent/FR2103870A5/fr not_active Expired
- 1971-08-03 DE DE2138807A patent/DE2138807C3/en not_active Expired
- 1971-08-04 SE SE7109978A patent/SE389392B/en unknown
- 1971-08-05 AT AT685671A patent/AT320476B/en active
- 1971-08-05 IT IT69646/71A patent/IT939753B/en active
- 1971-08-05 FI FI2209/71A patent/FI56447C/en active
- 1971-08-06 JP JP5950071A patent/JPS5632559B1/ja active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2936676A (en) * | 1953-11-27 | 1960-05-17 | Robert Roger Aime | System for releasing objects suspended from aircraft |
| US2961927A (en) * | 1955-10-04 | 1960-11-29 | Brevets Aero Mecaniques | Rocket launching systems |
| US2972933A (en) * | 1957-12-23 | 1961-02-28 | Gen Dynamics Corp | Missile hand launching system |
| US3089390A (en) * | 1960-03-11 | 1963-05-14 | Short Brothers & Harland Ltd | Launching apparatus for guided missiles |
| US3031932A (en) * | 1960-04-19 | 1962-05-01 | Mimx Corp | Anti-radiation and dunnage device |
| US3194119A (en) * | 1962-07-17 | 1965-07-13 | Louise Rosemonde Paulette Jacq | Closing devices for rocket bomb nozzle |
| US3167278A (en) * | 1962-10-04 | 1965-01-26 | Francis D Roberge | Ordnance aerial transfer system |
| US3319522A (en) * | 1965-02-16 | 1967-05-16 | Mb Assoc | Launching device |
| US3357305A (en) * | 1965-12-15 | 1967-12-12 | Garland W Clutz | Expendable dual-purpose rocket launcher shipping container |
| US3495497A (en) * | 1967-05-19 | 1970-02-17 | Bolkow Gmbh | Coupling member for a missile firing and guiding device |
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3981224A (en) * | 1975-07-11 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Army | Missile trans porter-launcher |
| US3988961A (en) * | 1975-08-08 | 1976-11-02 | The United States Of America As Represented By The Secretary Of The Army | Integrated rocket shipping container and launcher |
| US4007660A (en) * | 1975-09-29 | 1977-02-15 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defense | Rocket retention and ignition assembly |
| US4296669A (en) * | 1979-05-25 | 1981-10-27 | The United States Of America As Represented By The Secretary Of The Army | Rocket tube launcher with cast-in place tube support bulkhead |
| US4604939A (en) * | 1984-08-20 | 1986-08-12 | The United States Of America As Represented By The Secretary Of The Army | Lightweight composite launcher pod |
| US4719839A (en) * | 1985-02-14 | 1988-01-19 | Werkzeugmaschinenfabrik | Rotary storage magazine |
| US6311604B1 (en) * | 1990-04-30 | 2001-11-06 | Raytheon Company | Protective missile launch tube enclosure |
| US5058481A (en) * | 1990-10-15 | 1991-10-22 | The United States Of America As Represented By The Secretary Of The Navy | Dual modular rocket launcher |
| AU656560B2 (en) * | 1991-03-25 | 1995-02-09 | Fmc Corporation | Missile canister and method of fabrication |
| US5115711A (en) * | 1991-03-25 | 1992-05-26 | Fmc Corporation | Missile canister and method of fabrication |
| EP0505927A3 (en) * | 1991-03-25 | 1993-12-01 | Fmc Corp | Missile canister and method of fabrication |
| NL9400447A (en) * | 1993-03-24 | 1994-10-17 | Fmc Corp | Dual rocket holder. |
| US5327809A (en) * | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
| US5413024A (en) * | 1993-07-16 | 1995-05-09 | Alliant Techsystems Inc. | Disposable flare dispenser magazine for infrared decoy flares |
| US6142055A (en) * | 1998-06-17 | 2000-11-07 | United Defense, L.P. | Matrix gun system |
| US20050242230A1 (en) * | 2002-06-28 | 2005-11-03 | Marc Vallier | Adapter device for projectile fired from a launching tube |
| US7036419B2 (en) * | 2002-06-28 | 2006-05-02 | Mbda | Adapter device for projectile fired from a launching tube |
| US8789453B1 (en) * | 2013-02-21 | 2014-07-29 | The United States Of America As Represented By The Secretary Of The Navy | Dispenser pod |
| US20140230636A1 (en) * | 2013-02-21 | 2014-08-21 | United States Of America As Represented By The Secretary Of The Navy | Dispenser pod |
| ES2585603A1 (en) * | 2015-07-01 | 2016-10-06 | Anortec, Sl | Adjustable mount for single-use launcher tube light launcher (Machine-translation by Google Translate, not legally binding) |
| USD956712S1 (en) * | 2020-07-13 | 2022-07-05 | Frog Design Inc. | Wireless headphone |
| CN114543583A (en) * | 2022-04-28 | 2022-05-27 | 成都航天万欣科技有限公司 | Precision adjusting device and method for storage and transportation launching box |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1329514A (en) | 1973-09-12 |
| CH528058A (en) | 1972-09-15 |
| IT939753B (en) | 1973-02-10 |
| SE389392B (en) | 1976-11-01 |
| DE2138807A1 (en) | 1972-02-10 |
| NL163622B (en) | 1980-04-15 |
| DE2138807B2 (en) | 1979-10-31 |
| NL163622C (en) | 1980-09-15 |
| ZA714996B (en) | 1972-04-26 |
| IL37394A (en) | 1975-02-10 |
| FI56447C (en) | 1980-01-10 |
| NL7110165A (en) | 1972-02-08 |
| BE770706A (en) | 1972-01-31 |
| AT320476B (en) | 1975-02-10 |
| IL37394A0 (en) | 1971-11-29 |
| DE2138807C3 (en) | 1980-07-10 |
| FR2103870A5 (en) | 1972-04-14 |
| JPS5632559B1 (en) | 1981-07-28 |
| FI56447B (en) | 1979-09-28 |
| CA934197A (en) | 1973-09-25 |
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