WO1996032610A1 - Bottom plate member - Google Patents
Bottom plate member Download PDFInfo
- Publication number
- WO1996032610A1 WO1996032610A1 PCT/SE1996/000469 SE9600469W WO9632610A1 WO 1996032610 A1 WO1996032610 A1 WO 1996032610A1 SE 9600469 W SE9600469 W SE 9600469W WO 9632610 A1 WO9632610 A1 WO 9632610A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- plate
- plate member
- flaps
- gas pressure
- bottom plate
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/06—Closures, e.g. cap, breakable member
Definitions
- This invention relates to a bottom plate member which is designed and made for initially tightening a chamber in which a high gas pressure is generated. Examples of such chambers can be found in ammunition rounds for recoilless weapons but also in pipes and containers within the pro ⁇ cess industry.
- the invention relates to a bottom plate member which is located at the rear end of a propellant charge chamber of an ammunition round for a re ⁇ coilless weapon. Initially the bottom plate member pro ⁇ vides a tightening and barrier for the propellant gases, for instance gases of powder, generated in the chamber when the round is fired, but is broken when the gas pres- sure within the chamber exceeds a certain level so that the gases are allowed to exit from the rear end of the am ⁇ munition round.
- the propellant gases for instance gases of powder
- Bottom plate members of this type have previously been used in ammunition rounds for recoilless weapon systems. It is the gas outlet rearwards, when the rear bottom plate is broken, that makes the weapon recoilless. It is also previously known to use similar bottom plates as so-called blasting foils in the process industry, in which the func- tion of the bottom plate is to break and evacuate the gas ⁇ es as soon as an inadmissible gas pressure is generated in a pipe or a container.
- the object of this invention is to solve the problems that have been discussed above and provide a more controlled and splinterfree process for the opening of the plate so that a substantially 100% safety is achieved for this pro ⁇ cess.
- this is achieved by pro ⁇ viding the bottom plate with a through hole in the center which gives an effective starting point for the cracking process, fractural impressions for controlling the crack ⁇ ing process so that the plate after the cracking start is divided into a number of well defined flaps, but which are connected to each other, and a number of straight edges, which number corresponds to the number of flaps, against which edges the base of the flaps are arranged to be fold ⁇ ed when the plate is opened up due to the gas pressure.
- FIG. 1 shows a complete ammunition round for a recoilless weapon system before firing as well as after firing
- fig ⁇ ure 3 shows the bottom plate with the fractural impres ⁇ sions more in detail
- figure 4 shows an insert member for the bottom plate
- figure 5 shows the two members bottom plate and insert member put together.
- Figure 1 shows a complete ammunition round 1 in firing po ⁇ sition in a launching barrel 2 of a recoilless weapon sys- tern, for example a 20 mm ammunition round.
- the launching barrel 2 has a rear conventional nozzle 3 for the exhaust ⁇ ing propellant gases.
- the ammunition round 1 comprises a chamber 4 with a propellant charge therein and a detonator 5.
- a bottom plate 6 is located at the rear end of the chamber 4 for tightening the chamber and providing a bar ⁇ rier for the generated powder gases so that an efficient ignition over the propellant charge is guaranteed.
- the bottom plate consists basically of a comparatively thin, circular disc 7 and a flange 8 arranged at the rearmost part of the chamber wall 9.
- the bottom plate 6 is dimensioned so that it is broken and blown open by the gases as soon as a specific gas pressure has been reached within the chamber. It is this gas pres ⁇ sure that makes the weapon recoilless.
- the plate member has been designed and made in such a way that basically 100% safety against such small and harmful fragments is guaranteed when the plate member is opened up by the gas pressure.
- the design of the bottom plate is illustrated more in de- tail in figure 3 by means of a front view as well as a cross-section.
- the circular disc part 7 of the plate member has a star fracture so that six flaps 11 are formed.
- the star-shaped fractural impression is made by means of material-reducing notches in the plate, in this case six symmetrically arranged notches 10.
- the notches are not extending all the way to the periphery of the plate, but end up at a certain dis ⁇ tance d from the edge of the plate so that an integral, annular part with no material reductions is remained.
- the center of the plate has a through hole 12.
- the hole is small compared to the di ⁇ mension of the plate, specifically the diameter of the hole is approximately 10% of the plate diameter.
- this hole 12 is a through hole and located in the center of the plate it provides an efficient starting point for the cracking process. With fractural impressions 10 alone, it has turned out that small fragments are broken away from the central portion of the plate 6 which fragments might be harmful for personnel and/or equipment. By introducing the through hole in the center of the plate the risk for such undesired fragments is substantially reduced, the central portion of the plate which otherwise might give rise to said loose fragments is simply removed from the beginning.
- the through hole in the plate has also another purpose.
- a high-amplitude pressure peak is obtained which might give rise to a pen ⁇ dulum pressure in the chamber.
- the hole 12 in the plate has a damping ability with respect to such pressure peak and reduces the risk of dangerous pendulum-type pressure.
- Figure 2 illustrates the ammunition round 1 after firing with the now empty propellant charge chamber and the opened bottom plate 6.
- the flaps 11 of the plate have been bent backwards and bear against the inner wall of the noz ⁇ zle with their tips.
- the bottom plate member comprises a ring-shaped insert member 14, see figure 4, which insert member abuts the flange 8 of the bottom plate with its outer, circumfe ⁇ rential surface 15 and which has a hexagonal inner part, i e six straight edges 16 against which the base portions of the flaps are bent.
- the bottom plate itself according to figure 3 is prefer ⁇ ably made of a ductile stainless steel material.
- the in ⁇ sert member 14 for the plate, see figure 4 is preferably made of a sintered stainless steel material or made from a rod-shaped material which is finish-turned on its outer surface and then cut off in suitable lengths.
- the bottom plate also could be made as a unitary member, in which case the straight edges 16 against which the flaps are bent are made directly in the flange 8 of the bottom plate itself.
- the fractional impression is made as a star- shaped pattern so that six flaps are formed when the bot ⁇ tom plate is blown up.
- any other pattern formed by the fractional impressions can be used so that the num ⁇ ber of flaps can be varied.
- the insert member 14 is made with a number of straight edges, which number corre ⁇ sponds to the number of flaps, which means that each flap has a straight edge to be bent around upon the release of gas pressure.
- the hole 12 has been illustrated as a through hole, but it is understood that the hole can be sealed by means of a foil or the like to make the chamber damp-proof, especial ⁇ ly during transport and storage. Such a thin sealing mem ⁇ ber does not change the described function of the hole 12, however.
- the invention has been described in connection with a pro ⁇ pellant charge chamber for a recoilless weapon system. It should be understood that the bottom plate can be used al ⁇ so in other applications in which a controlled opening of a plate is required when a certain pressure has been ex ⁇ ceeded. Examples of such applications can be found in the process industry.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Rigid Containers With Two Or More Constituent Elements (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/930,591 US5900575A (en) | 1995-04-11 | 1996-04-10 | Bottom plate member |
DE69622586T DE69622586D1 (de) | 1995-04-11 | 1996-04-10 | Bodenplatte |
EP96910281A EP0870165B1 (en) | 1995-04-11 | 1996-04-10 | Bottom plate member |
CA002217528A CA2217528C (en) | 1995-04-11 | 1996-04-10 | Bottom plate member |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9501344A SE506253C2 (sv) | 1995-04-11 | 1995-04-11 | Anordning vid bottenbricka |
SE9501344-7 | 1995-04-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1996032610A1 true WO1996032610A1 (en) | 1996-10-17 |
Family
ID=20397927
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1996/000469 WO1996032610A1 (en) | 1995-04-11 | 1996-04-10 | Bottom plate member |
Country Status (6)
Country | Link |
---|---|
US (1) | US5900575A (sv) |
EP (1) | EP0870165B1 (sv) |
CA (1) | CA2217528C (sv) |
DE (1) | DE69622586D1 (sv) |
SE (1) | SE506253C2 (sv) |
WO (1) | WO1996032610A1 (sv) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1923656A1 (en) * | 2006-11-17 | 2008-05-21 | Saab Ab | Arrangement for weapon |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7019822B1 (en) * | 1999-04-29 | 2006-03-28 | Mss, Inc. | Multi-grade object sorting system and method |
SE524912C2 (sv) * | 2003-06-05 | 2004-10-19 | Saab Ab | Runt vapen trycksänkande motmassa i motmassebehållare innefattande styrande vikstöd för symmetriskt öppningsförlopp |
SE525137C2 (sv) * | 2003-06-05 | 2004-12-07 | Saab Ab | Anordning vid vapen innefattande en motmassa för att sänka trycket kring vapnet, varvid motmassans huvudbeståndsdel är vätska som binds och hålls kvar av kapillärkrafter |
EP1584883B1 (en) * | 2004-04-05 | 2006-11-08 | Saab Ab | Weapon of countermass type and means for sealing countermass |
ATE344914T1 (de) * | 2004-04-05 | 2006-11-15 | Saab Ab | Waffe mit gegengewicht und vorrichtung zur dichtung des gegengewichtes |
US8322264B1 (en) * | 2007-02-13 | 2012-12-04 | The United States Of America As Represented By The Secretary Of The Army | Controlled plastic venting for low-recoil gun systems |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2791961A (en) * | 1952-02-11 | 1957-05-14 | Musser C Walton | Recoilless type ammunition having self-contained venturi |
SE406805B (sv) * | 1975-02-06 | 1979-02-26 | Dynamit Nobel Ag | Drivladdningstendare |
DE3012382A1 (de) * | 1979-03-29 | 1980-10-02 | Katsuo Oana | Sicherheitsgaspatrone |
DE3208032A1 (de) * | 1981-04-10 | 1982-10-28 | Miyata Industry Co., Ltd., Chigasaki, Kanagawa | Druckfluid-patrone und dafuer vorgesehener sicherheitsverschluss |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NO118837B (sv) * | 1966-10-04 | 1970-02-16 | Foersvarets Fabriksverk | |
US4902043A (en) * | 1985-09-17 | 1990-02-20 | John T. Hoskins | Fluid coupling and seal assembly |
US4739799A (en) * | 1986-10-20 | 1988-04-26 | Carney Joseph H | Plumbing test plug |
CA2019946C (en) * | 1990-06-27 | 1996-11-12 | Donald D. Savard | Temporary disintegratable plug for an open-ended oil pipeline |
US5216194A (en) * | 1991-05-15 | 1993-06-01 | Alliant Techsystems Inc. | Lightweight molded cartridge case and nozzle assembly for recoilless launch systems |
-
1995
- 1995-04-11 SE SE9501344A patent/SE506253C2/sv not_active IP Right Cessation
-
1996
- 1996-04-10 CA CA002217528A patent/CA2217528C/en not_active Expired - Fee Related
- 1996-04-10 EP EP96910281A patent/EP0870165B1/en not_active Expired - Lifetime
- 1996-04-10 DE DE69622586T patent/DE69622586D1/de not_active Expired - Lifetime
- 1996-04-10 US US08/930,591 patent/US5900575A/en not_active Expired - Fee Related
- 1996-04-10 WO PCT/SE1996/000469 patent/WO1996032610A1/en active IP Right Grant
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2791961A (en) * | 1952-02-11 | 1957-05-14 | Musser C Walton | Recoilless type ammunition having self-contained venturi |
SE406805B (sv) * | 1975-02-06 | 1979-02-26 | Dynamit Nobel Ag | Drivladdningstendare |
DE3012382A1 (de) * | 1979-03-29 | 1980-10-02 | Katsuo Oana | Sicherheitsgaspatrone |
DE3208032A1 (de) * | 1981-04-10 | 1982-10-28 | Miyata Industry Co., Ltd., Chigasaki, Kanagawa | Druckfluid-patrone und dafuer vorgesehener sicherheitsverschluss |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1923656A1 (en) * | 2006-11-17 | 2008-05-21 | Saab Ab | Arrangement for weapon |
Also Published As
Publication number | Publication date |
---|---|
US5900575A (en) | 1999-05-04 |
DE69622586D1 (de) | 2002-08-29 |
CA2217528C (en) | 2004-03-23 |
CA2217528A1 (en) | 1996-10-17 |
SE506253C2 (sv) | 1997-11-24 |
SE9501344L (sv) | 1996-10-12 |
EP0870165B1 (en) | 2002-07-24 |
SE9501344D0 (sv) | 1995-04-11 |
EP0870165A2 (en) | 1998-10-14 |
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