US2004200344A1PendingUtilityA1
Radar comouflaged launcher for deploying ammunition
Assignee: HDW HOWALDTSWERKE DEUTSCHE WERPriority: Dec 5, 2002Filed: Dec 5, 2003Published: Oct 14, 2004
Est. expiryDec 5, 2022(expired)· nominal 20-yr term from priority
B63G 2013/027F41A 23/34B63G 13/02F41F 3/077F41F 1/08
40
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Claims
Abstract
The present invention relates to a device for deploying ammunition, wherein a recess ( 2 ) provided in the body shell ( 1 ) of a vehicle, in particular of a ship, is covered by cover means ( 4 ), whereby a heightening of the radar signature caused by this recess ( 2 ) and having a negative effect is diminished.
Claims
exact text as granted — not AI-modified1 . A device for deploying ammunition, wherein a recess ( 2 ) in the body shell ( 1 ) of a mobile object provided for ammunition depoyment is covered by a cover arrangement ( 4 ), that reduces a radar signature caused by this recess ( 2 ) and having a negative effect is diminished.
2 . The device according to claim 1 , wherein the ammunition is deployed with the aid of a launcher located on the inside of the body shell of the object.
3 The device according to claim 2 , wherein the launcher has at least one discharge tube (3).
4 . The device according to claim 2 , wherein the launcher terminates flush with the body sheet (1) of the object.
5 . The device according to claim 3 , wherein the launcher is located at a distance of 0-20 cm from the body shell of the object.
6 . The device according to claim 3 , wherein the discharge tube ( 3 ) is arranged on the inside of the body shell ( 1 ), so that loading of the launcher tube ( 3 ) is possible from the inside.
7 . The device according to claim 3 , wherein the discharge tube ( 3 ) is accommodated in a launcher housing ( 6 ).
8 . The device according to claim 7 , wherein the launcher housing ( 6 ) is fixedly connected with the inside of the body shell ( 1 ).
9 . The device according to claim 6 , wherein the launcher housing ( 6 ) includes at least one closable hatch in the interior range of the object, through which loading of the launcher tube(s) ( 3 ) takes place.
10 . The device according to claim 9 , wherein the hatch is a squeeze lock ( 7 ).
11 . The device according to claim 8 , wherein a gas-tight seal is provided at least either between launcher housing opening and body shell ( 1 ) or between loading hatch ( 8 ) and loading opening of the launcher housing ( 6 ).
12 . The device according to claim 11 , wherein the launcher housing ( 6 ) is provided with a blow-off valve ( 10 ).
13 . The device according to claim 7 , wherein the launcher housing ( 6 ) is provided with outlet means ( 9 ).
14 . The device according to claim 7 , wherein the launcher housing ( 6 ) is provided with a connection facility ( 12 ) for control with the aid of ignition means.
15 . The device according to claim 14 , wherein the ignition means are electrical ignition means.
16 . The device according to claim 15 , wherein the launcher housing ( 6 ) includes grounding means ( 11 ).
17 . The device according to claim 1 , wherein the angle of deployment of the discharge means is adjustable in lateral pointing and elevation with the ad of adapters ( 13 ).
18 . The device according to claim 1 , wherein the object is selected from the group consisting of land vehicles, aircraft and water craft.
19 . The device according to claim 1 , wherein the cover arrangement ( 4 ) comprises a radar camouflage coating.
20 . The device according to claim 1 , wherein the cover arrangement ( 4 ) covers the recess ( 2 ) such that a radar camouflaged structure of the body shell ( 1 ) is preserved.
21 . The device according to claim 1 , wherein the cover earrangement ( 4 ) is opened by the penetrating body to then close again.
22 . The device according to claim 21 , wherein the cover arrangement ( 4 ) includes at least one camouflage hatch.
23 . The device according to claim 22 , wherein the at least one camouflage hatche is arranged as a single hatch, as a wing hatch, or as an annular or polygonal hatch segment.
24 . The device according to claim 21 , wherein the cover arrangement ( 4 ) includes at least one elastic, material.
25 . The device according to claim 24 , wherein the elastic material is provided with a radar-scattering coating.
26 . The device according to claim 25 , wherein the radar-scattering coating is made of metal.
27 . The device according to claim 1 , further comprising a splash-proof protective cover ( 5 ) which is removed by a first discharge of ammunition.
28 . The device according to claim 27 , wherein the protective cover (5) is a radar-reflecting type.
29 . The device according to claim 27 , wherein the protective cover ( 5 ) terminates flush with the body shell ( 1 ).
30 . The device according to claim 27 , wherein the protective cover (5) is retained by a snap-in device.
31 . Method for enhancing the radar camouflage of a mobile object, wherein all of the recesses ( 2 ) in the body shell ( 1 ) of the object for the deployment of ammunition are covered by reversible covers ( 4 ), reducing a negative effect of the radar signature caused by the recesses ( 2 ).
32 . The device according to claim 5 , wherein the distance is 0.5-1.5 cm.
33 . The device according to claim 32 , wherein the distance is 1-5 cm.
34 . The device according to claim 24 , wherein the elastic material is a rubber material.
35 . The method according to claim 31 , wherein the mobile object is a ship.Cited by (0)
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