US1714989A - Method of making bourdon tubes - Google Patents
Method of making bourdon tubes Download PDFInfo
- Publication number
- US1714989A US1714989A US188318A US18831827A US1714989A US 1714989 A US1714989 A US 1714989A US 188318 A US188318 A US 188318A US 18831827 A US18831827 A US 18831827A US 1714989 A US1714989 A US 1714989A
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- US
- United States
- Prior art keywords
- coil
- making
- tube
- bourdon
- rib
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/06—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
- B21C37/15—Making tubes of special shape; Making tube fittings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/06—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
- B21C37/15—Making tubes of special shape; Making tube fittings
- B21C37/155—Making tubes with non circular section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D11/00—Bending not restricted to forms of material mentioned in only one of groups B21D5/00, B21D7/00, B21D9/00; Bending not provided for in groups B21D5/00 - B21D9/00; Twisting
- B21D11/06—Bending into helical or spiral form; Forming a succession of return bends, e.g. serpentine form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D11/00—Component parts of measuring arrangements not specially adapted for a specific variable
- G01D11/16—Elements for restraining, or preventing the movement of, parts, e.g. for zeroising
- G01D11/18—Springs
Definitions
- This invention relates to the manufacture of pressure responsive instruments, and more particularly to a'method of making a.
- Bour- 'don tube of the type for example, disclosed in my pending application Serial No. 726,231, filed *July 15, 1924, for Bourdon tubes.
- the present application is a division of said pending application.
- Certain instruments such, for example, as distance type thermometers, utilize a Bourdon tube to actuate an indicator in response to the variations of pressure produced by the expansion and contraction of an expansible liquid ina remotely located bulb.
- the invention of my co-pending application has to do with the provision of a Bourdon coil having stiffening means in the parts of larger radius so that the inner parts may be rendered more elficient for the intended purpose.
- the present invention has to do with the method whereby a Bourdon coil of this character is produced.
- Fig. 1 is a cross section of a fiat piece of pulping suitable for making into a Bourdon Fig. 2 shows a spiral coil made up in accordance with the present invention; Flg. 3 shows the end of the tubing shaped to form theouter part of the coil;
- Fig. 4 is a longitudinal section through suitable dies showing the formation of the part shown in Fig. 3;
- F ig. 5 is a cross section on the line 55 of Fig. 4;
- Fig. 6 illus'tratesa double helical coil to -which the present invention has been applied.
- Figs. 4 and 5 One end of the flattened tubing is placed between a pair of cooperative dies 14 so and 15 one of which is provided with a longitudinal depression 16 which is opposite a longitudinal rib 17 on the other die.
- a longitudinal rib is produced in the end portion of the strip of flattened tubing.
- Such a ridge is shown at 18.
- the strip. of tubing is to be used in making a spiral coil (such as shown 1n Fig. 2) I prefer to gradually taper, the depression 16 and rib 17 in the dies, as more clearly shown in Fig.
- a tapering longitudinal rib or ridge along the tu mg is then wound into a coil 20 of t e predetermined diameter.
- a coil 20 of t e predetermined diameter is illustrated in Fig. 2.
- the outer end 21 of the coil is mounted in a fixed sup ort 22 while the inner end 23 is adapted or connection with an indicating hand, not shown.
- the tapering ridge or rib 18 extends from the support around the outer convolutions of the co1l, thereby rendering these convolutions somewhat more ri 'd than the inner ones.
- the rigidity of the convolutions varies inversely with the distance from the outer or supported end of the omplete coil.
- coils made up as above described provide a very open and uniform scale, and that all parts of the coil may be made to function in the intended manner by varying the stiffness by means of the rib or ridge which is formed in the tubing before the tubing is wound into the coil.
- Fig. 6 shows a double helical coil form of pressure responsive element- 30.
- one provides the length of strip which is to go into the outer convolutions 31 with a long ridge or rib 32 which extends from the end convolution 33 down to the other end 34 of the coil where it is suitably supported in the instrument.
- the end convolution is spirally wound and has a decreasing diameter to reach to the inner convolutions 35.
- This convolution is preferably provided with a rib 36 of varying height so that there will be a gradual variation in the rigidity of this con volution as its radius of curvature changes.
- this form of coil one may, however. omit the tapering feature in the end coil 33 and rely upon the diflerence in rigidity in the inner and outer coils which would be produced .by uniform ridge or rib 32.
- the method of making a Boudon coil which comprises providing a straight, flattened, metallictube, stamping, a stiffening rib of gradually diminishing height in said tube at a single operation, and forming the tube into a coil of variable diameter with the portion including the highest part of the rib at the outside of the coil.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Fluid Pressure (AREA)
Description
METHOD OF MAKING BOURDON TUBES Original Filed July 15, 1924 Patented May 28, 1929.
UNITED STATES PATENT- OFFICE.
HERMIAN SCHLAICH, OF LONG ISLAND CITY, YORK.
METHOD OF MAKING BOURDON TUBES.
Original application filed July 15, 1924, Serial No. 726,231, and in Germany March 12, 1925. Divided and this application filed my 2, 1927. Serial No. 188,318.
This invention relates to the manufacture of pressure responsive instruments, and more particularly to a'method of making a. Bour- 'don tube of the type, for example, disclosed in my pending application Serial No. 726,231, filed *July 15, 1924, for Bourdon tubes. The present application is a division of said pending application.
Certain instruments, such, for example, as distance type thermometers, utilize a Bourdon tube to actuate an indicator in response to the variations of pressure produced by the expansion and contraction of an expansible liquid ina remotely located bulb.
In order to obtain a wide, open, uniform scale and accurate and dependable readings, it has been found necessary to eliminate as many parts which might contribute,errors as by lost motion-as possible. This has resulted in the use of a longer pressure responsive element which has been wound into such forms'as a double helix having inner and outer coils or a spiral coil, These forms of pressure responsive element have parts at 2 different diameters. Inasmuch as the flexibility of the Bourdon tube is a function of the radius of curvature, it is notuniform throughout the length of the coil. I have found that this lack of uniformity is quite appreciable and that it results in compelling the outer coils to assume more than their share of the distortion due to pressure changes. The inner coils, on account of the stifiness inherent in the smaller diameter of coil, operate at a much reduced efliciency.
The invention of my co-pending application has to do with the provision of a Bourdon coil having stiffening means in the parts of larger radius so that the inner parts may be rendered more elficient for the intended purpose.
The present invention has to do with the method whereby a Bourdon coil of this character is produced.
In the accompanying drawings, two forms of Bourdon coils made in accordance with the present method are illustrated in detail, and the steps whereby such Bourdon coils are produced are illustrated.
In the drawings-forming a part of this specification Fig. 1 is a cross section of a fiat piece of pulping suitable for making into a Bourdon Fig. 2 shows a spiral coil made up in accordance with the present invention; Flg. 3 shows the end of the tubing shaped to form theouter part of the coil;
Fig. 4 is a longitudinal section through suitable dies showing the formation of the part shown in Fig. 3;
F ig. 5 is a cross section on the line 55 of Fig. 4; and
Fig. 6 illus'tratesa double helical coil to -which the present invention has been applied.
In making up pressure responsive elements m accordance with the present invention one may utilize a flattened tube of the proper material and size for the. particular instrument in which the Bourdon tube is to be used- A cross-section of such a flattened tube is illustrated at 10 in- Fig. 1, where it will be noted that the flattened tube is opened slightlyat 11 and 12.
It has heretofore been the practice to wind such flattened tubing directly into the coil, but the present invention contemplates an intermediate step which is illustrated in Figs. 4 and 5. One end of the flattened tubing is placed between a pair of cooperative dies 14 so and 15 one of which is provided with a longitudinal depression 16 which is opposite a longitudinal rib 17 on the other die. When pressure is applied to the dies, a longitudinal rib is produced in the end portion of the strip of flattened tubing. Such a ridge is shown at 18. Where the strip. of tubing is to be used in making a spiral coil (such as shown 1n Fig. 2) I prefer to gradually taper, the depression 16 and rib 17 in the dies, as more clearly shown in Fig. 4, so as to produce a tapering longitudinal rib or ridge along the tu mg. The proper length of tubing is then wound into a coil 20 of t e predetermined diameter. Such a coil is illustrated in Fig. 2. Here the outer end 21 of the coil is mounted in a fixed sup ort 22 while the inner end 23 is adapted or connection with an indicating hand, not shown. The tapering ridge or rib 18 extends from the support around the outer convolutions of the co1l, thereby rendering these convolutions somewhat more ri 'd than the inner ones. When the rib is ma e tapering the rigidity of the convolutions varies inversely with the distance from the outer or supported end of the omplete coil.
I have found that coils made up as above described provide a very open and uniform scale, and that all parts of the coil may be made to function in the intended manner by varying the stiffness by means of the rib or ridge which is formed in the tubing before the tubing is wound into the coil.
If desired, one may provide the dies 14 and 15 with opposed depressions 24 and 25 and, in conjunction with other dies (not shown),- form enlargements 26 and 27 having enlarged openings therein which lare adapted to receive the pressure tubing 28 and the sealing tube 29.
Fig. 6 shows a double helical coil form of pressure responsive element- 30. In mak ng up such a coil according to the present invention, one provides the length of strip which is to go into the outer convolutions 31 with a long ridge or rib 32 which extends from the end convolution 33 down to the other end 34 of the coil where it is suitably supported in the instrument. The end convolution is spirally wound and has a decreasing diameter to reach to the inner convolutions 35. This convolution is preferably provided with a rib 36 of varying height so that there will be a gradual variation in the rigidity of this con volution as its radius of curvature changes. In this form of coil one may, however. omit the tapering feature in the end coil 33 and rely upon the diflerence in rigidity in the inner and outer coils which would be produced .by uniform ridge or rib 32.
It is obvious that the invention may be practiced with reference to may forms and constructions, and I wish it to be understood that the particular forms shown are but a few of the many forms. Various modifications and changes being possible, I do not limit myself in any way with respect thereto, except as indicated in the following claims.
I claim:
1. The method of making a Bourdon tube which comprises providing a flattened tube,
forming a longitudinal rib extending from one end of the flattened tube part way to the other end, and winding the flattened tube intoa coil with the rib portion in the outer convolutions of the coil.
2. The method of making a Bourdon tube which comprises providing a flattened tube,
forming a longitudinal rib extending from one end of the flattened tube toward the other one end of the flattened tube part way to the other end. and winding the flattened tube into a coil with the rib portion in the outer convolutions of the coil, the rib being outwardly disposed on the outer convolutions.
4. The method of making a Bourdon tube which comprises providing a flattened tube,
forming in both sides thereof a centrally dis posed longitudinal stiffening rib extending from one end of the flattened tube part way to the other end, and winding said tube into a coil with said other end at the inside of the coil so as to bring the ribbed portion to the outside of the coil. 1
5. The method of making a Bourdon tube which comprises providing a flattened tube,
simultaneously forming in both sides of the flattened tube centrally disposed longitudinal stiffening ribs extending from one end of the flattened tube toward the other. end, the heights of the ribs varying inversely as the distance from said first end. and winding said tube into a coil with said other end at the inside of the coil so as to bring the highest ribbed portion to the outside of the coil.
6. The method of making a Boudon coil, which comprises providing a straight, flattened, metallictube, stamping, a stiffening rib of gradually diminishing height in said tube at a single operation, and forming the tube into a coil of variable diameter with the portion including the highest part of the rib at the outside of the coil.
' In testimony whereof I have aflixed my sig-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US188318A US1714989A (en) | 1924-07-15 | 1927-05-02 | Method of making bourdon tubes |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US726231A US1714988A (en) | 1924-07-15 | 1924-07-15 | Bourdon tube |
US188318A US1714989A (en) | 1924-07-15 | 1927-05-02 | Method of making bourdon tubes |
Publications (1)
Publication Number | Publication Date |
---|---|
US1714989A true US1714989A (en) | 1929-05-28 |
Family
ID=26883955
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US188318A Expired - Lifetime US1714989A (en) | 1924-07-15 | 1927-05-02 | Method of making bourdon tubes |
Country Status (1)
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US (1) | US1714989A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2453165A (en) * | 1943-12-03 | 1948-11-09 | American Can Co | Method of preparing tubing for transportation |
US2748455A (en) * | 1951-01-05 | 1956-06-05 | Boosey & Hawkes Ltd | Method of forming a bend in ductile metal tubing |
US2857657A (en) * | 1956-01-16 | 1958-10-28 | California Inst Res Found | Method of constructing a porous wall |
US3232116A (en) * | 1962-08-06 | 1966-02-01 | Robertshaw Controls Co | Bourdon spiral assembly |
US3258955A (en) * | 1962-01-22 | 1966-07-05 | American Standard Controls Div | Method of manufacturing a pressure sensing element |
-
1927
- 1927-05-02 US US188318A patent/US1714989A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2453165A (en) * | 1943-12-03 | 1948-11-09 | American Can Co | Method of preparing tubing for transportation |
US2748455A (en) * | 1951-01-05 | 1956-06-05 | Boosey & Hawkes Ltd | Method of forming a bend in ductile metal tubing |
US2857657A (en) * | 1956-01-16 | 1958-10-28 | California Inst Res Found | Method of constructing a porous wall |
US3258955A (en) * | 1962-01-22 | 1966-07-05 | American Standard Controls Div | Method of manufacturing a pressure sensing element |
US3232116A (en) * | 1962-08-06 | 1966-02-01 | Robertshaw Controls Co | Bourdon spiral assembly |
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