| (19) |
 |
|
(11) |
EP 1 936 317 B1 |
| (12) |
EUROPEAN PATENT SPECIFICATION |
| (45) |
Mention of the grant of the patent: |
|
11.11.2009 Bulletin 2009/46 |
| (22) |
Date of filing: 22.12.2006 |
|
| (51) |
International Patent Classification (IPC):
|
|
| (84) |
Designated Contracting States: |
|
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE
SI SK TR |
| (43) |
Date of publication of application: |
|
25.06.2008 Bulletin 2008/26 |
| (73) |
Proprietor: SAAB AB |
|
581 88 Linköping (SE) |
|
| (72) |
Inventors: |
|
- Malmlöf, Andreas
SE-70224, Örebro (SE)
- Dugalic', Mili
SE-653 45, Karlstad (SE)
|
| (74) |
Representative: Herbjörnsen, Rut |
|
Albihns AB
P.O. Box 5581 114 85 Stockholm 114 85 Stockholm (SE) |
| (56) |
References cited: :
EP-A- 1 484 572 GB-A- 1 213 711 US-A- 2 557 151
|
DE-A1- 1 678 189 NL-A- 6 509 893 US-A- 2 598 256
|
|
| |
|
|
|
|
| |
|
| Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
|
[0001] The present invention relates to a nozzle for a weapon comprising a launcher which
constitutes a guide for a projectile or missile; the nozzle comprises a wall, a first
opening connected to the launcher and a second opening. The area of the first opening
is smaller than the area of the second opening.
[0002] Weapons such as handheld weapons from which a projectile or missiles are shot are
in some cases provided with a launcher without a nozzle. The nozzle is arranged in
the rear end of a launcher which constitutes a guide for the projectile. When the
weapon is fired the projectile is guided by the launcher and leaves the front end
of the launcher towards a target. Also a flame is created by the projectile when the
weapon is fired. The flame creates gases of high temperature which expands at the
rear end of the launcher of the weapon, through the nozzle. In this connection also
a high pressure being created behind the launcher.
[0003] In order to decrease the recoil and thus make possible an increase in weight of the
projectile without excessively high pressure being created behind the launcher, it
has been known for many years to introduce what is known as a countermass. The countermass
may be a liquid enclosed in a container arranged in the launcher behind the projectile.
The countermass in form of liquid leaves the rear end of the weapon when the weapon
is fired and thereby produces a pressure-reducing effect adjacent to the weapon when
the countermass expands and disintegrates. Documents
SE 0301626-8 and
SE 0301627-6 discloses examples of such countermass containers for weapons.
[0004] Document
DE-A1-1578050 discloses a weapon that forms the basis for the preamble of claim 1.
[0005] However, one drawback is that when the countermass is a liquid, a cloud is formed
around the weapon, which makes it difficult to rapidly achieve a clear view of the
target for firing the weapon again. Another drawback of using a countermass is that
an asymmetrical flow may be created in the countermass container, which can produce
great shear forces on the weapon. Also, pieces from the container may come away from
the container and constitute a risk behind the weapon.
[0006] The objective problem to be solved by the present invention is to avoid that a liquid
cloud is formed around the weapon when the weapon is fired.
[0007] Another objective problem to be solved by the present invention is to reduce the
pressure behind a weapon
[0008] Yet another objective problem to be solved by the present invention is to eliminate
the need of a countermass in a weapon.
[0009] Yet another objective problem to be solved by the present invention is to reduce
the recoil in the forward direction.
[0010] This is achieved by a nozzle according to claim 1.
[0011] Ambient air is used to reduce the temperature of the hot gases which leaves the rear
end of the weapon through the nozzle. When ambient air is introduced in the hot gases,
energy is transformed which reduces also the pressure inside the hot gases. Since
the pressure is reduced also the recoil on the weapon is reduced. The ambient air
is introduced in the hot gases by the means provided at the nozzle.
[0012] According to are embodiment said means is a spoiler is arranged substantially inside
the nozzle in the area of the second opening. When the weapon is fired the gases from
the projectile passes through the nozzle with high velocity. The spoiler creates a
low pressure on one of its surfaces when the gases pass the spoiler. The low pressure
reduces the temperature of the gases. Also, the low pressure created by the spoiler
leads to that ambient air is sucked in through the second opening of the nozzle and
thereby reduces the temperature of the gases from the projectile. According to this
embodiment the gases within the nozzle are under expanded.
[0013] According to yet another embodiment of the invention a circumferential element is
arranged at the first opening of the nozzle. The circumferential element has an opening
area which is less than the area of the first opening of the nozzle. The effect achieved
by this element is that recoil in the forward direction is reduced when the weapon
is fired.
[0014] When a nozzle provided with said means is used in a weapon a liquid cloud is not
formed around the weapon when the weapon is fired since there is no need for a countermass.
Therefore it is possible to rapidly firing the weapon again since no liquid cloud
restricts the view of the target.
[0015] Also, a weapon with such a nozzle is easy to handle, cost effective when manufacturing
and have no problems with shear forces which may occur when using a countermass.
[0016] Other advantages and features of the invention can be derived from the following
detailed description of exemplary embodiments of the invention, with reference to
the drawings.
Fig. 1 shows a section view of a nozzle according to an embodiment of the invention,
Fig. 2 shows a view in perspective of the nozzle according to an embodiment, and
Fig.53 shows a section view of a nozzle according to an embodiment of the invention
with a reduced pressure area indicated.
[0017] According to an embodiment of the invention disclosed in fig. 1 said means 18 is
a spoiler 18' arranged substantially inside the nozzle 1 in the area of the second
opening 12. The spoiler 18' is so arranged inside the nozzle 1 that an opening gap
22 is created between the wall 8 of the nozzle 1 and the spoiler 18'.
[0018] Fig. 2 shows a perspective view of the second embodiment. The spoiler 18' has a form
which is substantial circular and is connected to the wall 8 by distance elements
24. Preferably, the distance elements 24 have an aerodynamic form that not disturbs
the flow of the gases 16.
[0019] When the weapon 2 is fired the gases 16 from the projectile 6 passes through the
nozzle 1 with high velocity. The spoiler 18' creates a low pressure on one of its
surfaces when the gases 16 pass the spoiler 18', which is indicated in fig 5. The
low pressure reduces the temperature of the gases 16 and the low pressure LP created
by the spoiler 18' also leads to that ambient air is sucked in through the second
opening 12 of the nozzle 1 and thereby reduces the temperature of the gases 16 from
the projectile 6.
[0020] According to a second embodiment of the invention 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 nozzle 1. Hence, a circumferential
abutment 30 or edge is created by the element 26. When the weapon 2 is fired a pressure
from the gases 16 created by the projectile 6 is exerted on the element 26. Therefore,
recoil in the forward direction of the weapon 2 is reduced.
1. Nozzle 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); characterized in that the area of the first opening (10) is smaller than the area of the second opening
(12); the nozzle (1) has the form of a funnel; 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); said means is a spoiler (18') arranged
substantially inside the nozzle (1) in the area of the second opening (12) and the
spoiler (18') is so arranged inside the nozzle (1) that an opening gap (22) is created
between the wall (8) of the nozzle (1) and the spoiler (18').
2. Nozzle according to claim 1, characterized in that said means (18;18') is arranged at the second opening of the nozzle.
3. Nozzle according to any of the preceding claims, characterized in that the first and second openings (10,12) are substantially cylindrical.
4. Nozzle according to any of the preceding claims, characterized in that the first and second openings (10,12) are arranged substantially concentric with
each others.
5. Nozzle according to any of the preceding claims, characterized in that a gas generator (14) is arranged in the area of the first opening (10).
6. Nozzle according to claim 1, characterized in that the spoiler (18') has a form which is substantial circular.
7. Nozzle according to claim 1 or 6, characterized in that the spoiler (18') is connected to the wall (8) by distance elements (24).
8. Nozzle according to any of the preceding claims, characterized in that a circumferential element (26) is arranged at the first opening (10) of the nozzle
(1) and in that an opening area (28) of the circumferential element (26) is less than the area of
the first opening (10) of the nozzle (1).
1. Düse für eine Waffe (2), die eine Abschusseinrichtung (4) umfasst, die eine Führung
für ein Projektil oder ein Geschoss (6) bildet, wobei die Düse (1) eine Wand (8),
eine mit der Abschusseinrichtung (4) verbundene erste Öffnung (10) und eine zweite
Öffnung (12) umfasst, dadurch gekennzeichnet, dass die Fläche der ersten Öffnung (10) kleiner als die Fläche der zweiten Öffnung (12)
ist; die Düse (1) die Form eines Trichters aufweist; die Düse (1) mit einem Mittel
(18; 18') zum Verringern des Drucks von Gasen (16) von dem Projektil (6) innerhalb
und hinter der Düse (1), wenn die Waffe (2) abgefeuert wird, versehen ist; das Mittel
ein Spoiler (18') ist, der im Wesentlichen innerhalb der Düse (1) in der Fläche der
zweiten Öffnung (12) angeordnet ist, und der Spoiler (18') so innerhalb der Düse (1)
angeordnet ist, dass eine Öffnungslücke (22) zwischen der Wand (8) der Düse (1) und
dem Spoiler (18') gebildet ist.
2. Düse nach Anspruch 1, dadurch gekennzeichnet, dass das Mittel (18, 18') an der zweiten Öffnung der Düse angeordnet ist.
3. Düse nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die erste und die zweite Öffnung (10, 12) im Wesentlichen zylindrisch sind.
4. Düse nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die erste und die zweite Öffnung (10, 12) im Wesentlichen konzentrisch zueinander
angeordnet sind.
5. Düse nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass ein Gaserzeuger (14) in der Fläche der ersten Öffnung (10) angeordnet ist.
6. Düse nach Anspruch 1, dadurch gekennzeichnet, dass der - Spoiler (18') eine Form aufweist, die im Wesentlichen kreisförmig ist.
7. Düse nach Anspruch 1 oder 6, dadurch gekennzeichnet, dass der Spoiler (18') durch Abstandselemente (24) mit der Wand (8) verbunden ist.
8. Düse nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass ein Umfangselement (26) an der ersten Öffnung (10) der Düse (1) angeordnet ist und
dass eine Öffnungsfläche (28) des Umfangselements (26) kleiner als die Fläche der
ersten Öffnung (10) der Düse (1) ist.
1. Tuyère pour une arme (2) comprenant un lanceur (4) qui constitue un guide pour un
projectile ou missile (6) ; la buse (1) comprend une paroi (8), une première ouverture
(10) raccordée au lanceur (4) et une seconde ouverture (12) ; caractérisée en ce que la surface de la première ouverture (10) est plus petite que la surface de la seconde
ouverture (12) ; la tuyère (1) a la forme d'un entonnoir ; la tuyère (1) est prévue
avec des moyens (18, 18') pour réduire la pression des gaz (16) du projectile (6)
à l'intérieur et derrière la tuyère (1) lors de la mise à feu de l'arme (2), lesdits
moyens sont un réducteur de portance (18') agencé sensiblement à l'intérieur de la
tuyère (1) dans la zone de la seconde ouverture (12) et le réducteur de portance (18')
est agencé à l'intérieur de la tuyère (1) de sorte qu'un espace d'ouverture (22) est
créé entre la paroi (8) de la tuyère (1) et le réducteur de portance (18').
2. Tuyère selon la revendication 1, caractérisée en ce que lesdits moyens (18, 18') sont agencés au niveau de la seconde ouverture de la tuyère.
3. Tuyère selon l'une quelconque des revendications précédentes, caractérisée en ce que les première et seconde ouvertures (10, 12) sont sensiblement cylindriques.
4. Tuyère selon l'une quelconque des revendications précédentes, caractérisée en ce que les première et seconde ouvertures (10, 12) sont agencées de manière sensiblement
concentriques les unes par rapport aux autres.
5. Tuyère selon l'une quelconque des revendications précédentes, caractérisée en ce qu'un générateur de gaz (14) est agencé dans la zone de la première ouverture (10).
6. Tuyère selon la revendication 1, caractérisée en ce que le réducteur de portance (18') a une forme qui est sensiblement circulaire.
7. Tuyère selon la revendication 1 ou 6, caractérisée en ce que le réducteur de portance (18') est raccordé à la paroi (8) par des éléments de distance
(24).
8. Tuyère selon l'une quelconque des revendications précédentes, caractérisée en ce qu'un élément circonférentiel (26) est agencé au niveau de la première ouverture (10)
de la tuyère (1) et en ce qu'une surface d'ouverture (28) de l'élément circonférentiel (26) est inférieure à la
surface de la première ouverture (10) de la tuyère (1).


REFERENCES CITED IN THE DESCRIPTION
This list of references cited by the applicant is for the reader's convenience only.
It does not form part of the European patent document. Even though great care has
been taken in compiling the references, errors or omissions cannot be excluded and
the EPO disclaims all liability in this regard.
Patent documents cited in the description