DE602006010422D1 - jet - Google Patents
jetInfo
- Publication number
- DE602006010422D1 DE602006010422D1 DE602006010422T DE602006010422T DE602006010422D1 DE 602006010422 D1 DE602006010422 D1 DE 602006010422D1 DE 602006010422 T DE602006010422 T DE 602006010422T DE 602006010422 T DE602006010422 T DE 602006010422T DE 602006010422 D1 DE602006010422 D1 DE 602006010422D1
- Authority
- DE
- Germany
- Prior art keywords
- opening
- nozzle
- area
- launcher
- projectile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000010304 firing Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
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
Abstract
The invention relates to a nozzle (1) for a weapon (2) comprising a launcher (4) which constitutes a guide for a projectile or missile (6). The nozzle (1) comprises a wall (8), a first opening (10) connected to the launcher (4) and a second opening (12). The area of the first opening (10) is smaller than the area of the second opening (12). The nozzle (1) is provided with means (18; 18') for reducing the pressure of gases (16) from the projectile (6) inside and behind the nozzle (1) when firing the weapon (2). A circumferential element (26) is arranged at the first opening (10) of the nozzle (1). An opening area (28) of the circumferential element (26) is less than the area of the first opening (10) of the nozzle (1).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP06126990A EP1936317B1 (en) | 2006-12-22 | 2006-12-22 | Nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602006010422D1 true DE602006010422D1 (en) | 2009-12-24 |
Family
ID=38038731
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602006010422T Active DE602006010422D1 (en) | 2006-12-22 | 2006-12-22 | jet |
Country Status (5)
Country | Link |
---|---|
US (1) | US20100275763A1 (en) |
EP (1) | EP1936317B1 (en) |
AT (1) | ATE448459T1 (en) |
DE (1) | DE602006010422D1 (en) |
ES (1) | ES2333666T3 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2933499T3 (en) * | 2017-05-17 | 2023-02-09 | Saab Ab | Chamber and procedure for noise reduction |
US10788284B1 (en) * | 2019-05-09 | 2020-09-29 | The United States Of America As Represented By The Secretary Of The Army | Grounded and vehicular mounted weapons with improved recoil stability |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2557151A (en) * | 1944-08-24 | 1951-06-19 | Leslie A Skinner | Spring actuated generator for rocket launchers |
US2598256A (en) * | 1945-04-21 | 1952-05-27 | Us Sec War | Recoilless gun |
BE560119A (en) * | 1956-09-13 | |||
US2956479A (en) * | 1958-02-28 | 1960-10-18 | Musser C Walton | Cascaded gun barrel |
US3035494A (en) * | 1960-01-26 | 1962-05-22 | Musser C Walton | Recoil adjusting device |
US3251552A (en) * | 1963-03-07 | 1966-05-17 | Douglas M Ford | Exhaust nozzle for jet or rocket motors |
DE977818C (en) * | 1963-06-22 | 1970-12-17 | Messerschmitt Boelkow Blohm | Propellant charge arrangement for tubular launchers |
US3208384A (en) * | 1964-01-21 | 1965-09-28 | Fountain Gilbert | Rocket thrust neutralizer |
DE1428637C1 (en) * | 1964-02-26 | 1975-02-20 | Messerschmitt Boelkow Blohm | Tubular launcher for projectiles, especially for missiles |
FR1410375A (en) * | 1964-07-30 | 1965-09-10 | Tech De Rech S Eindustrielles | Small footprint weapon |
NL132545C (en) * | 1967-03-16 | |||
DE1678189A1 (en) * | 1968-03-12 | 1972-01-13 | Ludwig Bucklisch | Recoil-free weapon |
SE416230B (en) * | 1976-05-17 | 1980-12-08 | Bofors Ab | DEVICE FOR RECYCLING EXPLOITATION OF A MISSILE |
US4043248A (en) * | 1976-06-10 | 1977-08-23 | General Electric Company | Liquid propellant gun (recoilless regenerative piston) |
US4091709A (en) * | 1976-07-26 | 1978-05-30 | The United States Of America As Represented By The Secretary Of The Army | Recoilless rifle nozzle |
US4203347A (en) * | 1978-04-10 | 1980-05-20 | The Boeing Company | Shock suppressing apparatus and method for a rocket launcher |
US4404887A (en) * | 1980-06-23 | 1983-09-20 | General Dynamics, Pomona Division | Recoil reducer |
SE525137C2 (en) | 2003-06-05 | 2004-12-07 | Saab Ab | Apparatus for weapons comprising a countermass to lower the pressure around the weapon, the main component of the countermass being fluid which is bound and retained by capillary forces |
SE524912C2 (en) * | 2003-06-05 | 2004-10-19 | Saab Ab | Round weapon pressure lowering countermass in countermass container including guiding fold support for symmetrical opening process |
-
2006
- 2006-12-22 ES ES06126990T patent/ES2333666T3/en active Active
- 2006-12-22 DE DE602006010422T patent/DE602006010422D1/en active Active
- 2006-12-22 EP EP06126990A patent/EP1936317B1/en active Active
- 2006-12-22 AT AT06126990T patent/ATE448459T1/en not_active IP Right Cessation
-
2007
- 2007-12-21 US US12/003,319 patent/US20100275763A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
ES2333666T3 (en) | 2010-02-25 |
EP1936317B1 (en) | 2009-11-11 |
ATE448459T1 (en) | 2009-11-15 |
EP1936317A1 (en) | 2008-06-25 |
US20100275763A1 (en) | 2010-11-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |