[0001] The present invention relates to a torpedo recovery device.
[0002] In the so-called drill configuration, used for performance testing and practice,
torpedoes have negative buoyancy and so tend to sink at the end of the mission, thus
making them difficult to recover for the next mission.
[0003] It is an object of the present invention to provide a recovery device that can be
housed inside the torpedo, without affecting the streamline contour of the torpedo,
and which provides for positive buoyancy of the torpedo at the end of the mission
or, at any rate, in predetermined activation conditions.
[0004] According to the present invention, there is provided a device as claimed in Claim
1.
[0005] A preferred, non-limiting embodiment of the present invention will be described by
way of example with reference to the accompanying drawings, in which:
Figure 1 shows a side view of a torpedo featuring a recovery device in accordance
with the present invention;
Figure 2 shows a view in perspective of the torpedo in the recovery position, after
the device according to the invention is activated;
Figure 3 shows an axial section of the recovery device;
Figure 4 shows a view in perspective of the device at one assembly stage.
[0006] With reference to Figures 1 and 3, number 1 indicates as a whole a torpedo.
[0007] According to the present invention, torpedo 1 comprises a recovery device 2 housed
inside the torpedo, preferably at the front, close to the head 3.
[0008] Recovery device 2 comprises a substantially cylindrical supporting structure 4 forming
a section of the overall structure of torpedo 1. Structure 4 substantially comprises
two tubular end portions 5, 6, of the same outside diameter as the torpedo and connected
to the adjacent sections of the torpedo; and an intermediate portion 7 smaller in
outside diameter and integral with one (6) of the tubular portions. The intermediate
portion of device 2 is defined externally by a frangible cylindrical housing 8 flush
with the outer surface of tubular portions 5, 6. It should be pointed out that "frangible"
is used here in its widest sense, and applies equally to a housing made of a number
of detachable parts, as well as to a one-piece housing that can be broken off or detached
from structure 4. In a preferred embodiment, housing 8 preferably comprises three
120° segments 9 fixed releasably to tubular portions 5, 6 by respective dove-tail
joints 10, 11, and defining, with intermediate portion 7, an annular chamber 12 housing
an inflatable bag 13.
[0009] Bag 13 comprises an annular sheet of high-pressure-resistant, rubber-coated canvas
fixed hermetically along its lateral edges 17, 18 to the axial ends 15, 16 of intermediate
portion 7 of structure 4 to form an air chamber 19 with intermediate portion 7.
[0010] More specifically, each lateral edge 17, 18 of bag 13 is thicker than the rest of
the sheet to form a raised toroidal rib 20, and is gripped between a first ring 21
fitted hermetically to the respective end 15, 16 of intermediate portion 7 and defining
a shoulder 22 for the lateral edge, and a second ring 23 which slides onto the first
and is locked in the grip position by a ring nut 24. Shoulder 22 and second ring 23
are shaped to mate with lateral edge 17, 18, and in particular with relative rib 20.
[0011] At rest, bag 13 is folded accordion-fashion inside annular chamber 12, and is kept
in this position by a rip-off retaining belt 25 (Figure 4) surrounding bag 13, and
which comprises two fabric portions 26 laced together by laces 27 (only one shown)
made of string with a predetermined break strength.
[0012] At rest, bag 13 therefore exerts no pressure on housing 8.
[0013] Bag 13 has three compensating valves 28 located 120° apart and offset, with respect
to the centre line of the bag, towards lateral edge 17 (i.e. in use, towards head
3 of torpedo 1). Each compensating valve 28 comprises a casing 29 fixed hermetically
to an opening 30 in bag 13 and defining a cavity 31 communicating with air chamber
19 and the outside through respective openings 32, 33. A shutter 34 associated with
opening 32 is held in a normally closed position by a spring 35, and opens when the
difference in pressure between air chamber 19 and the outside exceeds a predetermined
threshold value defined by the setting of spring 35.
[0014] Structure 4 of the device houses a cylinder 36 of high-pressure, e.g. 300-bar, compressed
air, which is fixed rigidly to structure 4 by three supports 37 (only one shown in
Figure 3), each fixed to an inner flange 38 of structure 4 by screws 39.
[0015] Cylinder 36 is connected to air chamber 19 by a pneumatic circuit comprising a fitting
40, an explosive-actuated valve 41, a pipe 42, and a diffuser 43.
[0016] More specifically, valve 41 comprises a breakable partition 44 associated with an
electrically-activated explosive actuating device (squib) 45, which receives an activating
signal S resulting from an AND operation between a control signal C1 and a consent
signal C2.
[0017] Control signal C1 is in turn the result of an OR operation between three signals
: a signal S1 from a first pressure sensor P1; a signal S2 from a second pressure
sensor P2; and an activation control signal S3.
[0018] Sensors P1 and P2 are set to define the minimum and maximum pressure respectively
to which device 2 can be subjected during the mission, i.e. the compulsory operating
depth range of the device.
[0019] Consent signal C2 is generated by a salinity sensor SS designed to only permit activation
of device 2 in seawater, and so prevent accidental activation during transport or
storage.
[0020] Device 2 operates as follows.
[0021] Device 2 is activated at the end of the torpedo 1 mission, either by activation control
signal S3 (end of mission) or, in the event of a malfunction causing the torpedo to
stray from the predetermined depth range, by pressure sensor P1 or P2 generating respective
signal S1 or S2.
[0022] In the presence of signal C2 from salinity sensor SS and one of signals S1, S2 and
S3, activating signal S is active, so squib 45 breaks partition 44 to allow compressed-air
flow from cylinder 36 through fitting 40, valve 41, pipe 42, and diffuser 43 into
air chamber 19.
[0023] Diffuser 43 prevents high-pressure airflow from striking bag 13 directly and so damaging
the material.
[0024] Bag 13 is thus inflated and, in so doing, snaps laces 27 and rips off retaining belt
25; and the outward mechanical thrust exerted by bag 13 also detaches segments 9.
[0025] Bag 13 is now free to expand and inflate fully into a toroidal shape about torpedo
1 to achieve positive buoyancy of torpedo 1.
[0026] As torpedo 1 floats to the surface, compensating valves 28 maintain a constant pressure
difference between air chamber 19 and the outside, to prevent bag 13 from expanding
to breaking point as a result of the reduction in external pressure as torpedo 1 rises.
[0027] By locating device 2 at the front, the torpedo emerges in the substantially vertical
recovery position shown in Figure 1, with head 3 above water.
[0028] It should be noted that valves 28 are so located as to face upwards, and so be freely
accessible, in the above recovery position.
[0029] One of the three compensating valves 28 is conveniently fitted with a line 46 fixed
to shutter 34, and which is operated manually to deflate bag 13 and so assist recovery
of torpedo 1.
[0030] The advantages of device 2 according to the present invention will be clear from
the above description.
[0031] In particular, device 2 provides for surfacing torpedo 1 at the end of the mission
or in the event of a malfunction, thus simplifying recovery.
[0032] Moreover, in the preferred embodiment described, the structure of the device complies
with the dimensional requirements, dictated by the geometry of the torpedo, of in
no way affecting the streamline profile of the torpedo either before or during the
mission, and of ensuring maximum safety during handling and use.
[0033] Clearly, changes may be made to device 2 as described herein without, however, departing
from the scope defined in the accompanying Claims.
1. A recovery device (2) for a torpedo (1), the device comprising a housing (8) designed
to be incorporated in the torpedo (1); buoying means (13) housed in said housing (8);
pressurized-gas supply means (36); and valve means (41) for connecting said supply
means (36) to said buoying means (13) and inflating said buoying means (13) in response
to at least one activating signal.
2. A device as claimed in Claim 1, characterized in that said housing (8) is breakable by said buoying means (13) when these are inflated.
3. A device as claimed in Claim 1 or 2,
characterized by comprising a supporting structure (4); said housing (8) being connected to said structure
(4) to define a continuous outer profile with respect to the profile of the torpedo
(1).
4. A device as claimed in Claim 3, characterized in that said housing (8) comprises a number of segments (9) connected to said structure (4)
by connecting means (10, 11) releasable by said buoying means (13).
5. A device as claimed in Claim 3 or 4,
characterized in that said structure (4) comprises two tubular end portions (5, 6) connected to adjacent
sections of said torpedo (1); and a smaller-diameter intermediate portion (7) defining,
with said housing (8), an annular cavity (12) housing said buoying means (13).
6. A device as claimed in Claim 5, characterized in that said buoying means comprise an annular bag (13) housed in said annular cavity (12).
7. A device as claimed in Claim 6, characterized in that said bag (13) comprises an annular sheet having lateral edges (17, 18) connected
hermetically to said structure (4) and forming, with said structure, an air chamber
(19).
8. A device as claimed in Claim 6 or 7,
characterized by comprising a rip-off retaining belt (25) for holding said bag (13) in a folded position.
9. A device as claimed in Claim 8, characterized in that said retaining belt (25) comprises a number of fabric portions (26) joined by laces
(27) of a string of a predetermined break strength.
10. A device as claimed in any one of the foregoing Claims, characterized in that said pressurized-gas supply means comprise a cylinder (36) of compressed air.
11. A device as claimed in any one of the foregoing Claims, characterized in that said valve means comprise an explosive-actuated valve (41).
12. A device as claimed in Claim 11, characterized in that said explosive-actuated valve (41) comprises a breakable partition (44); and an explosive
actuating device (45) for breaking said partition (44).
13. A device as claimed in any one of the foregoing Claims, characterized by comprising pressure sensors (P1, P2) which generate activating signals to activate
said valve means (41) in the event the torpedo (1) exceeds predetermined depth thresholds.
14. A device as claimed in any one of the foregoing Claims, characterized by comprising a salinity sensor (SS) which generates a consent signal for said valve
means (41).
15. A device as claimed in any one of Claims 6 to 14, characterized in that said valve means (41) are connected to said air chamber (19) by a diffuser (43).
16. A device as claimed in any one of Claims 5 to 15, characterized in that said bag (13) has at least one compensating valve (28) for regulating the pressure
difference between said air chamber (19) and the outside.
17. A torpedo, characterized by comprising a recovery device (2) as claimed in any one of the foregoing Claims.
18. A torpedo as claimed in Claim 17, characterized in that said housing (8) of said device is flush with adjacent sections of the torpedo (1),
so as not to affect the streamline profile of the torpedo (1).
19. A torpedo as claimed in Claim 17 or 18,
characterized in that said recovery device is located close to a head of said torpedo (1).
20. A torpedo comprising a recovery device (2) as claimed in Claim 16, characterized in that said bag (13) has a number of compensating valves (28) arranged along the bag (13)
and so located as to face, in use, the head (3) of the torpedo (1).
21. A torpedo as claimed in Claim 20, characterized in that at least one of said compensating valves (28) comprises hand-operated means (46)
for deflating said bag (13).