|Publication number||US3032462 A|
|Publication date||May 1, 1962|
|Filing date||Nov 4, 1955|
|Priority date||Nov 4, 1955|
|Publication number||US 3032462 A, US 3032462A, US-A-3032462, US3032462 A, US3032462A|
|Inventors||Roy J Saporito|
|Original Assignee||Scott Aviation Corp|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (12), Referenced by (10), Classifications (6)|
|External Links: USPTO, USPTO Assignment, Espacenet|
y 1962 R. -1. SAPORITO 3,032,462
PROCESS OF MAKING A DIAPHRAGM United States This invention relates to a process for making diaphragms and more particularly to the making of that type of diaphragm which in its operation displaces a considerable volume of fluid. More especially the invention relates to a diaphragm comprising one component of a miniature regulator for a high altitude breathing apparatus employing oxygen as the breathing fluid.
The principal object of the invention is to provide a diaphragm which is very thin and sensitive and yet is able to function properly even when subjected to excessive pressures. Other collateral objects of the invention and practical attainments thereof are described in the following description and illustrated in the appended drawing, wherein:
FIG. 1 is a perspective view of the completed diaphragm.
FIG. 2 is a transverse medial section thereof, taken on line 22 FIG. 1.
FIG. 3 is an enlarged, schematic, fragmentary, transverse section illustrating the calendering of the rubberlike sheet which constitutes the chief component of the diaphragm.
FIG. 4 is an enlarged, fragmentary, transverse section thru a piece of fabric.
FIG. 5 is an enlarged, schematic, fragmentary, transverse section illustrating the calendering of the sheet and the fabric to form a sandwich.
FIG. 6 is a somewhat enlarged, transverse, medial section thru the completed diaphragm.
For convenience and succinctness, this invention will be described exactly as illustrated but it is to be understood that the scope of the invention is to be measured by the rational interpretation of the claims.
The first step in the making of this diaphragm is to take a blob 10 of some such rubber-like material as silicone rubber and pass it between the rotating rolls 11 and 12 of a rubber calendering machine to form a silicone sheet 13. The blob of silicone rubber used in this calendering operation may be defined as hydrated magnesium silicate, H Mg (SiO The sheet 13 is approximately .030 thick and to obtain this thickness the rolls 11 and 12 are spaced approximately .010 apart.
This sheet 13 of silicone rubber is then overlaid by a strip of fabric 14 (as shown at the left side of FIG. 5) and this combination of silicone sheet 13 and superimposed fabric strip 14 is then fed thru rotating calendering rolls 15 and 16, which are spaced approximately .006 apart. The fabric is approximately .005" thick and the sandwic 17 that results from this second calendering operation is approximately .017 thick.
A conical, metal backing plate 18 now has its upper or convex side mechanically roughened by sandpaper or by sand blasting or the like and this surface then cleaned with acetone and a layer of silicone primer such as a silicone derivative primer applied. The sandwich 17 is then laid over said plate 18 and the whole laminated combination placed in a mold Which is dusted with talcum powder to prevent the mold from sticking to the diaphragm. The mold is then compressed so as to shape the sandwich 17 to the diaphragm shape shown in FIG.
6 which shape includes the concentric annular convolutions or corrugations 20 and 21 and also the internal, annular, concentric rib 23. The mold is now heated to 240-260 F. for 5 minutes. The mold is then opened 5 atent "ice i 2 and the diaphragm removed and its jagged peripheral edge trimmed off to form the finished diaphragm 22 of FIGS. 6, 1 and 2.
It should be noted that the metal plate 18 is bonded to that face of the sandwich 17 which is furthest from its fabric 14. This is to ensure maximum bonding strength between said plate 18 and the sandwich 17.
In some cases it is desirable to employ a fabric 14 which, while pliable, is not stretchable to any great extent, and in such cases it is desirable to use a fabric in which either the warp or the woof or of both the warp and the woof of the fabric, are of the tension-resisting type, as in ordinary woven cloth. In other cases, however, the volume of fluid displaced by the diaphragm and the fluid pressures involved are such that a certain amount of stretch of the diaphragm is desirable. In such cases it is preferable to use a fabric in which either the warp or the woof or of both the warp and the woof of the fabric are of the knitted type, i.e., of the type where there is a certain amount of give before the threads become straightened out. These threads may be of nylon, Orlon, Dacron or the like and in any certain application to be sufficiently strong to withstand fluid pressures which are sufiiciently high to rupture the silicone if it were not reinforced by the fabric.
1. The process of making an annular diaphragm consisting of producing a sheet of silicone rubber by calendering a quantity of silicone rubber between power-driven rolls; overlaying said sheet with a strip of raw fabric to form a sandwich; calendering said sheet-strip sandwich between a second pair of power-driven rolls which are spaced apart a considerably smaller distance than the thickness of said sheet-strip sandwich, and operate to very forceably imbed said strip in said sheet; mechanically pressing said sheet-strip sandwich in a two'part, rigid, formed, diaphragm mold in a direction parallel to its axis; and then heating said sheet-strip sandwich to a temperature between 240 and 260 F.
2. As in claim 1 with a roughened backing-plate placed in the mold against one face of the sheet-strip sandwich, prior to the pressing and heating operations.
3. As in claim 1 with a roughened backing-plate placed in the mold against that particular face of the sheet-strip sandwich which is located the farthest from its strip, this latter placement being effected prior to the pressing and heating operations.
4. As in claim 1 with a silicone derivative primer applied to a backing-plate which latter is placed in the mold prior to the pressing and heating operations.
5. As in claim 1 with both the warp and woof of the fabric being of the knitted type.
6. As in claim 1 with the sheet of silicone rubber being approximately thirty thousandths of an inch thick.
7. As in claim 1 with the sheet of silicone rubber being approximately thirty thousandths thick and produced by the first calendering operation with the rolls spaced approximately ten thousandths of an inch apart.
8. As in claim 1 with the rolls of the first calendering operation being approximately thirty thousandths of an inch apart and the rolls of the second calendering operation being approximately six thousandths of an inch apart.
References Cited in the file of this patent UNITED STATES PATENTS 1,594,048 Colbert et al. July 27, 1926 1,952,468 Smith Mar. 27, 1934 2,017,071 Minor Oct. 15, 1935 (Other references on following page) 3 UNITED STATES PATENTS Coffey Feb. 22, 1938 Jennings July 30, 1946 Hosking Oct. 22, 1946 Arnold June 29, 1948 5 4 Palumbo Nov. 21, 1950 Nagel et a1. Dec. 19, 1950 Smith-Johannsen June 24, 1952 Kay Sept, 2, 1952 Cofiey Feb. 7, 1956
|Cited Patent||Filing date||Publication date||Applicant||Title|
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|US1952468 *||Oct 15, 1931||Mar 27, 1934||Alfred J Smith||Automobile trim material and its method of manufacture|
|US2017071 *||Mar 10, 1934||Oct 15, 1935||Ind Process Corp||Method of securing adhesion of rubber to metal|
|US2109190 *||Aug 26, 1935||Feb 22, 1938||Coffey Joseph Herbert||Method and apparatus for making rubber articles|
|US2405038 *||Dec 24, 1943||Jul 30, 1946||Du Pont||Carburetor diaphragm|
|US2409759 *||Sep 13, 1941||Oct 22, 1946||Composite Rubber Products Corp||Direct bonding of rubber to metal|
|US2444394 *||Mar 11, 1943||Jun 29, 1948||Lane Wells Co||Method of molding diaphragms|
|US2530906 *||Jun 28, 1947||Nov 21, 1950||Johns Manville||Sheet packing and method of manufacture|
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|Citing Patent||Filing date||Publication date||Applicant||Title|
|US3186552 *||Dec 12, 1962||Jun 1, 1965||Filters Inc||Filter element end cap|
|US3332479 *||Jan 2, 1964||Jul 25, 1967||Carrier Corp||Heat exchanger with expansible tube seal|
|US3372073 *||Jul 15, 1966||Mar 5, 1968||Filters Inc||Process for making a molded filter assembly|
|US3389035 *||Aug 16, 1966||Jun 18, 1968||Reeves Bros Inc||System, apparatus and process for the manufacture of metering diaphragms|
|US3523857 *||Apr 21, 1967||Aug 11, 1970||Chem Rubber Products Inc||Diaphragm assembly|
|US4048280 *||Sep 17, 1971||Sep 13, 1977||Jury Gordeevich Borzyak||Method of manufacturing electrotechnical articles|
|US4390584 *||Jan 21, 1981||Jun 28, 1983||Societe Nationale Industrielle Aerospatiale||Process for making a perforated rigid sheet material for sound absorbing composite cellular structure|
|US5068074 *||Oct 20, 1988||Nov 26, 1991||Schlumberger Industries, S.A.||Method for making synthetic membranes for a gas meter|
|US5093067 *||Jun 21, 1989||Mar 3, 1992||Allied-Signal Inc.||Injection molding of fabric reinforced elastomeric diaphragms|
|US5487861 *||Feb 16, 1995||Jan 30, 1996||Walbro Corporation||Method of making synthetic composite fuel metering membrane|
|U.S. Classification||156/242, 264/273, 264/257|