Marine countermeasures launch assembly

Information

  • Patent Grant
  • 6484618
  • Patent Number
    6,484,618
  • Date Filed
    Monday, October 1, 2001
    22 years ago
  • Date Issued
    Tuesday, November 26, 2002
    21 years ago
  • Inventors
  • Original Assignees
  • Examiners
    • Carone; Michael J.
    • Sukman; Gabriel S.
    Agents
    • McGowan; Michael J.
    • Oglo; Michael F.
    • Kasischke; James M.
Abstract
A marine countermeasures launch assembly includes a cylindrical body including first and second members having, respectively, first and second surfaces engageable with each other to form the body, the first surface having first and second recesses therein, the second surface having first and second recesses therein opposed to the recesses of the first member when the members are engaged, to form a first chamber for retaining a first countermeasure and a second chamber for retaining a second countermeasure. The first and second surfaces have opposed bores therein. A spring is disposed in each pair of the opposed bores and urges the members to separate from each other to release the countermeasures after the assembly is launched.
Description




CROSS REFERENCE TO OTHER PATENT APPLICATIONS




Not applicable.




BACKGROUND OF THE INVENTION




1. Field of the Invention




The invention relates to the development of electronic countermeasures and is directed more particularly to an assembly for launching undersea warfare countermeasures which serve as decoys and to jam and confuse sonar systems of submarines and torpedoes.




2. Description of the Prior Art




Acoustic countermeasure devices have become an integral part of undersea warfare. Such devices are used to confuse hostile sonar systems and thereby protect own force assets. Typical countermeasures are launched from a submarine and transmit acoustic signals. The signals are transmitted at a selected depth in the ocean and the devices are maintained at the selected depth by an active compensation system which maintains buoyancy. In practice, the devices typically are slightly negatively buoyant, requiring means for providing upward force to maintain depth.




Referring to

FIG. 1

, it will be seen that a known prior art countermeasure assembly


10


includes a cylindrical tube


12


in which are disposed a buoyancy maintenance system and countermeasures electronics (not shown). Fixed to the tube


12


is a transducer


14


which transmits signals from the countermeasure assembly


10


. A protective sabot


16


fits over the transducer


14


and is of a configuration which continues the cylindrical configuration of the tube


12


.




Submarines are provided with launch tubes


20


having therein a ram plate


22


, and a muzzle cap


26


disposed in a discharge end


28


of the tube


20


and held therein by shear pins


30


. The launch tubes


20


typically are mounted outside the pressure hull of the submarine. The launch tube


20


, ram plate


22


, and muzzle cap


26


define a compartment


32


complementary in shape and size to the countermeasure assembly


10


and sabot


16


.




Mounted in the tube


20


adjacent the ram plate


22


is a gas generator


34


. From within the submarine the gas generator


34


is activated to release gas under pressure. The gas forces the ram plate forwardly, to the right as viewed in FIG.


1


. The ram plate


22


and countermeasure


10


, including the transducer


14


and sabot


16


, move forwardly in the tube


12


, shearing the muzzle cap shear pins


30


and blowing away the muzzle cap


26


. The counter measure


10


, transducer


14


, and sabot


16


exit the tube


12


, with the transducer


14


protected during transit by the sabot


16


.




In due course, the sabot


16


drops away and the countermeasure


10


, including the transducer


14


, seeks a pre-selected depth from which to operate.




Recent advances in the buoyancy maintenance and transducer structure areas have resulted in reduced space requirements for countermeasures. It is now feasible from a size standpoint to launch two or more countermeasures from the prior art launch tube shown in FIG.


1


.




SUMMARY OF THE INVENTION




Accordingly, an object of the invention is to provide a marine countermeasures launch assembly which facilitates the launch of a plurality of countermeasures from a single prior art launch tube.




With the above and other objects in view, as will hereinafter appear, a feature of the present invention is the provision of a marine countermeasures launch assembly comprising a cylindrical body comprising first and second members having, respectively, first and second surfaces engageable with each other to form the body. The first surface is provided with first and second recesses therein and the second surface is provided with first and second recesses opposed to the recesses of the first member when the members are engaged, to form a first chamber for retaining a first countermeasure and a second chamber for retaining a second countermeasure. The first and second surfaces have opposed bores therein. A spring is disposed in each pair of the opposed bores and urges the members to separate from each other to release the countermeasures after the assembly is launched.




The above and other features of the invention, including various novel details of construction and combinations of parts, will now be more particularly described with reference to the accompanying drawings and pointed out in the claims. It will be understood that the particular assembly embodying the invention is shown by way of illustration only and not as a limitation of the invention. The principles and features of this invention may be employed in various and numerous embodiments without departing from the scope of the invention.











BRIEF DESCRIPTION OF THE DRAWINGS




Reference is made to the accompanying drawings in which is shown an illustrative embodiment of the invention, from which its novel features and advantages will be apparent, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:





FIG. 1

is a diagrammatic, in part sectional view of a prior art countermeasures launch assembly disposed in a launch tube;





FIG. 2

is a diagrammatic, in part sectional view of one form of countermeasures launch assembly illustrative of an embodiment of the invention;





FIG. 3

is an exploded perspective view of the assembly of

FIG. 2

; and





FIG. 4

is a diagrammatic in part sectional view of the assembly of

FIGS. 2 and 3

disposed in the assembly of FIG.


1


.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIGS. 2-4

, it will be seen that a preferred embodiment of the invention includes a cylindrical body


40


comprising a first member


42


having a first surface


44


. First and second recesses


46


,


48


are disposed in the surface


44


. The cylindrical body


40


further comprises a second member


50


having a second surface


52


having first and second recesses


54


,


56


therein. The recesses


46


,


48


are opposed to the recesses


54


,


56


when the members


42


,


50


are engaged, as shown in

FIG. 2

, to form a first chamber


60


for retaining a first countermeasure


62


, and a second chamber


64


for retaining a second countermeasure


66


. The countermeasures


62


,


66


each include transducers


58


in the body of the countermeasure.




The surfaces


44


,


52


are complementary to each other so as to fully engage one another and, for ease of manufacture and interchangeability, preferably are planar. The surfaces


44


,


52


are provided with opposed bores


68


. A spring


70


is disposed in each pair of opposed bores


68


. The springs


70


urge separation of the members


42


,


50


to release the countermeasures


62


,


66


.




In operation, the cylindrical body


40


is housed in the launch compartment


32


of the launch tube


20


(FIG.


4


). The body


40


houses the countermeasures


62


,


66


. The body


40


is launched in the same manner as the countermeasure assembly


10


, as described above with reference to FIG.


1


. When the body


40


clears the launch tube


20


, the springs


70


(

FIG. 3

) urge the members


42


,


50


apart, releasing the countermeasures


62


,


66


. Each countermeasure is provided with its own pressure sensor


72


and depth regulator


74


, and individually seeks its pre-selected depth and transmits signals, as previously programmed, by way of the transducers


58


.




There is thus provided a marine countermeasures launch assembly which facilitates launch of a plurality of countermeasures from a single launch tube.




It will be understood that many additional changes in the details, materials, steps and arrangement of parts, which have been herein described and illustrated in order to explain the nature of the invention, may be made by those skilled in the art within the principles and scope of the invention as expressed in the appended claims. For example, it will be apparent that the maximum number of chambers defined by the cylindrical body depends upon the size of the counter-measures to be contained. While two chambers are shown for illustrative purposes, the invention contemplates additional chambers.



Claims
  • 1. A marine countermeasures launch assembly comprising:a cylindrical body comprising first and second members having, respectively, first and second surfaces engageable with each other to form said body, the first surface having first and second recesses therein, the second surface having first and second recesses therein opposed to the recesses of said first member when said members are engaged, to form a first chamber for retaining a first countermeasure and a second chamber for retaining a second countermeasure, the first and second surfaces having opposed bores therein; and a spring disposed in each pair of the opposed bores and urging said members to separate from each other to release the countermeasures after the assembly is launched.
  • 2. The assembly in accordance with claim 1 wherein the first and second surfaces are planar surfaces.
  • 3. The assembly in accordance with claim 1 wherein said springs are coil springs.
  • 4. A countermeasures assembly comprising:a launch tube having a compartment therein; a cylindrical countermeasures body for disposition in said launch tube, said body comprising first and second members having, respectively, first and second surfaces engageable with each other to form said body, the first surface having first and second recesses therein, the second surface having first and second recesses therein opposed to the recesses of said first member when said members are engaged, to form a first chamber for retaining a first countermeasure and a second chamber for retaining a second countermeasure, the first and second surfaces having opposed bores therein, and a spring disposed in each pair of the opposed bores and urging said members to separate from each other to release the countermeasures after the assembly is launched; and a gas generator disposed in said launch tube and adapted to provide sufficient gas pressure in said tube to blow said cylindrical countermeasures body out of said tube.
  • 5. The assembly in accordance with claim 4 wherein the first and second surfaces of the first and second members are planar surfaces.
  • 6. The assembly in accordance with claim 4 wherein said springs are coil springs.
  • 7. The assembly in accordance with claim 4 and further comprising:a ram plate disposed in said tube; a muzzle cap disposed in said tube; and said tube, ram plate and muzzle cap defining the compartment; and wherein the sufficient gas pressure is operable to move said ram plate to push said countermeasures body from said launch tube.
STATEMENT OF GOVERNMENT INTEREST

The invention described herein may be manufactured and used by and for the Government of the United States of America for Governmental purposes without the payment of any royalties thereon or therefor.

US Referenced Citations (5)
Number Name Date Kind
2779282 Raffel Jan 1957 A
4676167 Huber et al. Jun 1987 A
5666900 Carroll et al. Sep 1997 A
6336641 Williams Jan 2002 B1
20020073831 MacLeon Jun 2002 A1
Foreign Referenced Citations (1)
Number Date Country
123598 Mar 1919 GB