Asymetrically contoured elastomeric disk

Information

  • Patent Grant
  • 6776079
  • Patent Number
    6,776,079
  • Date Filed
    Friday, July 25, 2003
    20 years ago
  • Date Issued
    Tuesday, August 17, 2004
    19 years ago
Abstract
An elastomeric disk for use in an elastomeric ejection system in which a thickened curvature protrudes from both sides of a central plane of the disk. Integral to each curvature is an annulet which dovetails from the curvatures to a periphery of the disk. The thickness of the annulet in regard to the central plane is greater on the fluid pressure side of the disk thereby shifting material strain to the center of the disk during expanding deformation. The annulet shape is attachable to the elastomeric ejection system by a clamp of the system.
Description




BACKGROUND OF THE INVENTION




(1) Field of the Invention




The present invention relates to a device for use in an elastomeric vehicle launching system, and more particularly to an elastomeric disk for the storage of elastic energy convertible to impulse fluid energy with the impulse fluid capable of ejecting or launching vehicles from the system into a liquid medium.




(2) Description of the Prior Art




Impulse fluid flows are used to launch vehicles from submarine platforms. Elastomeric ejection systems have been developed which store impulse fluid in a charged elastomeric bladder or against the pressure surface of a distended elastomeric disk. In the operation of an ejection system with an elastomeric disk, a recharge pump of the system draws water from the ocean such that the inflow of water has a pressure that distends or expands the disk. The elastic deformation of the disk by expansion results in a storage of energy by the disk. Once a predetermined amount of energy is stored, the recharge pump is shut off.




In order to launch a vehicle, a slide valve for the designated torpedo tube is opened. The opening action of the slide valve allows instantaneous porting water from the expanded disk to the torpedo tube with the porting water pressure capable of launching weapons from the tube.




Typical disks used for elastomeric ejection systems have a flat, ellipsoidal, spherical, or other symmetrically contoured shape. The purpose of a symmetrical contoured shape is to distribute strain energy across the disk during expansion. For example, the prior art disk


2


shown in FIG.


1


and shown in the cross-sectional view of

FIG. 2

has a symmetrical contour about a central plane


4


. When the prior art disk


2


expands, as shown in

FIG. 3

, the expansion of the disk


2


outward is the greatest at the center axis


6


of the disk


2


. The disk


2


must be clamped or attached at its edges


8


,


10


to the supporting structure


12


in order to expand outward.




The problem with the clamping of the disk


2


to the supporting structure


12


is that the expansion of the disk consequently puts a significant material strain at the periphery of the disk


2


. While there is a contact strain with the supporting structure


12


, the material strain is greater on the pressure surface


14


of the disk


2


specifically at the point


16


where the disk


2


bends toward deformation of the disk. This material strain at the bend of the disk


2


significantly increases the risk of disk failure during operation and interferes with the distribution of material strain across the disk


2


. In addition, the variation in the clamping strength of the supporting structure


12


and the loss of material strength of disk


2


at the structure


12


makes it difficult to predict how many cycles of operation the disk


2


can safely withstand.




SUMMARY OF THE INVENTION




Accordingly, it is a general purpose and primary object of the present invention to provide an elastomeric disk resistant to cyclic material failure at its periphery.




It is a further object of the present invention to provide an elastomeric disk in which the peak material strain levels of the disk are located proximate to the center of the disk such that the cycles of operation for the disk can be adequately determined.




It is a still further object of the present invention to provide an elastomeric disk which securely attaches to the structure of an elastomeric ejection system.




To attain the objects described there is provided an elastomeric disk with a thickened curvature protruding from both sides of a central plane of the disk. Integral to each curvature of the disk is an annulet which dovetails from the curvatures to a periphery of the disk. The annulet allows secure attachment of the disk to the ejection system preferably by a clamp of the supporting structure of the ejection system.




In contrast to the prior art, the contour of the disk is asymmetrical at the periphery of the disk. Specifically, the thickness of the annulet in regard to the central plane is greater on the pressure side of the disk. By increasing the thickness of the annulet on the pressure side of the disk, the bending strain and resultant material strain on the disk caused by expansion is compensated for while the holding action of the clamp is maintained. The strengthening of the disk thereby lengthens the material cyclic life of the ejection system since fatigue problems associated with the material strain at the periphery bend are minimized. In addition, the reduction of material strain at the periphery has the result of relocating the higher material strain away from the clamp and towards the center axis of the disk. At the center portion of the disk, incidence of fatigue failure is generally expected and thus a fatigue failure becomes more predictable for maintenance scheduling.




The above and other features of the invention, including various and 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 devices embodying the invention are shown by way of illustration only and not as the limitations 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




A more complete understanding of the invention and many of the attendant advantages thereto will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:





FIG. 1

depicts a plan view of a prior art elastomeric disk;





FIG. 2

depicts a cross-sectional view of the prior art elastomeric disk in which the disk is clamped to the support structure of an elastomeric ejection system with the view of the disk taken from reference line


2





2


of

FIG. 1

;





FIG. 3

depicts a cross-sectional view of the prior art disk of

FIG. 1

in which the disk is in an expanded state;





FIG. 4

depicts a plan view of an elastomeric disk of the present invention;





FIG. 5

depicts a cross-sectional view of the disk of the present invention with the view taken from reference line


5





5


of

FIG. 4

;





FIG. 6

depicts a cross-sectional view of the disk of the present invention in which the disk is clamped to the support structure of an elastomeric ejection system; and





FIG. 7

depicts a cross-sectional view of the disk of the present invention in which the disk is in an expanded state.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring now to the drawings including those drawings provided in the prior art portion of this specification wherein like numerals refer to like elements throughout the several is views, one sees that

FIG. 4

depicts the elastomeric disk


20


of the present invention. As shown in the cross-sectional view of

FIG. 5

, the elastomeric disk


20


is formed with a first curvature


22


protruding from a first side of a central plane


24


and a second curvature


26


protruding from a second side of the central plane


24


. Integral to the curvatures


22


and


26


is an annulet


28


which dovetails from the taper of the curvatures


22


,


26


to a periphery


30


of the disk


20


.




As further shown in the figure, the contour of the disk


20


is asymmetrical to the central plane


24


at the annulet


28


of the disk


20


. In order to compensate for bending strain associated with attachment to the structure of an ejection system, the thickness of the annulet


28


on the pressure surface


32


is increased. The portion of the annulet


28


on the pressure side


32


originates at a point


33


with the point


33


located a distance “A” from a center axis


34


of the disk


20


. The distance “A” is approximately eighty percent of the distance “B” for the point


35


upon which the annulet


28


originates on the non-pressure surface


36


of the disk


20


. By originating at the shorter distance of “A”, the annulet


28


incorporates a thicker area of the first curvature


22


.




In order to reduce the amount of material used while maintaining an increased thickness of the annulet


28


, the pressure surface


32


of the annulet


28


indents toward the central plane


24


without indenting the thickness of the annulet


28


between the origination points


33


and


35


. The indent


37


is preferably positioned at a majority of the distance to the periphery


30


from the origination point


33


. For the remaining distance to the periphery


30


, the pressure surface


32


extends away from the central plane


24


to form the widened base


38


of the annulet


28


.




As shown in

FIG. 6

, the dovetailed shape of the annulet


28


still permits clamping by a clamp


39


at the contact area


40


while an arc of clamping by the clamp


39


is maintained on the non-pressure surface


36


at the contact area


42


. The result of the increased thickness of the annulet


28


is that the bend area


44


shown in

FIG. 7

diverts to the center axis


34


and the annulet


28


is also retained with minimal movement in the clamp


39


. As such, a shift of material strain continues to the central axis


34


of the disk


20


.




Accordingly, the shift of material strain to the center of the disk


20


, also shifts the strain to where a fatigue failure is generally expected and thus a fatigue failure becomes more predictable for maintenance scheduling.




Thus by the present invention its objects and advantages are realized and although preferred embodiments have been disclosed and described in detail herein, its scope should be determined by that of the appended claims.



Claims
  • 1. An expandable elastomeric disk for retaining and discharging a fluid under pressure, said elastomeric disk comprising:first and second curvatures protruding opposite to each other from a central plane of said elastomeric disk wherein a surface of said first curvature is contactable to said fluid; and an annulet capable of attachment to a support structure for said elastomeric disk, said annulet including an interior circumference dovetailing to an exterior circumference with said interior circumference integrating to the surface of said first curvature at a first point and integrating to a surface of said second curvature at a second point; and wherein a distance of said first point from a central axis of said elastomeric disk is less than a distance of said second point from said central axis of said said elastomeric disk thereby providing a thickness combining said annulet and said first curvature in relation to said central plane greater than a thickness combining said annulet and said second curvature in relation to said central plane such that said thickness at said annulet and said first curvature reduces material strain at said thickness of said annulet and said first curvature during the expansion of said elastomeric disk with the effect of relocating the material strain to said central axis; wherein said central axis is perpendicular to said central plane.
  • 2. The elastomeric disk in accordance with claim 1 wherein a surface of said annulet includes an indent originating from said first point toward a thickness of said annulet, said indent providing a reduction in material used for said elastomeric disk.
  • 3. The elastomeric disk in accordance with claim 2 wherein said indent is less than a plane collinear with the protrusion of said first curvature.
  • 4. The elastomeric disk in accordance with claim 3 wherein said indent is positioned at a majority of a distance from said first point to said periphery.
  • 5. The elastomeric disk in accordance with claim 4 wherein said exterior circumference is positioned at a periphery of said elastomeric disk.
  • 6. The elastomeric disk in accordance with claim 5 wherein the distance of said first point from the central axis is at most eighty percent of the distance of said second point from the central axis of said elastomeric disk.
  • 7. The elastomeric disk in accordance with claim 6 wherein said first curvature is contactable to said fluid under pressure as a pressure side of said elastomeric disk and said second curvature protruding opposite to said first curvature as a non-pressure side of said elastomeric disk.
STATEMENT OF GOVERNMENT INTEREST

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

US Referenced Citations (20)
Number Name Date Kind
3962951 Schenk Jun 1976 A
4632035 Maillet Dec 1986 A
4848210 Bissonnette Jul 1989 A
5074187 Vollersen et al. Dec 1991 A
5099745 Hubbell Mar 1992 A
5125318 Purser Jun 1992 A
5200572 Bissonnette et al. Apr 1993 A
5231241 Bissonnette Jul 1993 A
5410978 Waclawik et al. May 1995 A
5438948 Moody Aug 1995 A
5546839 Gardiner Aug 1996 A
5562065 Duarte Oct 1996 A
5568782 Moody Oct 1996 A
5645006 Moody Jul 1997 A
5898125 Mangolds Apr 1999 A
5988036 Mangolds Nov 1999 A
6079347 Lieb Jun 2000 A
6216626 Curtis Apr 2001 B1
6220196 Escarrat Apr 2001 B1
6595098 Wray Jul 2003 B1
Foreign Referenced Citations (1)
Number Date Country
0638398 Jul 1995 EP