US2751935A - Diaphragm elements - Google Patents

Diaphragm elements Download PDF

Info

Publication number
US2751935A
US2751935A US474952A US47495254A US2751935A US 2751935 A US2751935 A US 2751935A US 474952 A US474952 A US 474952A US 47495254 A US47495254 A US 47495254A US 2751935 A US2751935 A US 2751935A
Authority
US
United States
Prior art keywords
diaphragm
corrugations
points
pressure
successive
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
Application number
US474952A
Inventor
Charles R Smith
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cutler Hammer Inc
Original Assignee
Cutler Hammer Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Cutler Hammer Inc filed Critical Cutler Hammer Inc
Priority to US474952A priority Critical patent/US2751935A/en
Application granted granted Critical
Publication of US2751935A publication Critical patent/US2751935A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J3/00Diaphragms; Bellows; Bellows pistons
    • F16J3/02Diaphragms

Definitions

  • a primary object of the invention is to provide a diaphragm the expansion of which is substantially linear over a wide range of pressures uniformly applied thereto.
  • Another object is to provide a diaphragm which is pressure-linear over a wide range of applied pressures, which expands relatively greatly in respect to its diameter and which will withstand a large number of expansions without breaking.
  • a more specific object is to provide a self-loaded diaphragm which is pressure-linear over the range of domestic refrigerator power element operation and, in addition, is a size, durability, and cost commensurate with the requirement of domestic refrigeration service.
  • the refrigerator, and its power element may be transported and stored in places where temperature differentials are greater than those which the power element will experience during normal service. Accordingly self-loaded diaphragms which form a part of those power elements must be able to withstand greater pressure differentials than those to which they are subjected during normal service.
  • Another object of the invention is to provide a diaphragm which can withstand such extreme pressure variations without loss of calibration in its normal operating range.
  • Figure 1 is a top plan view of a diaphragm embodying the invention
  • Fig. 2 is an enlarged sectional view taken on line 22 of Fig. l, and
  • Fig. 3 is a chart of certain of the structural features of the corrugations of the diaphragm greatiy exaggerated.
  • the diaphragm there shown comprises a circular cup 16 the bottom wall of which is provided with a series of concentric corrugations and a central boss 12.
  • corrugation 14 extends from point 17 to point 18
  • corrugation 15 extends from point 18 to point 19
  • corrugation 16 extends from point 19 to point 20.
  • the uppermost or top points of corrugations 14, 15 and 16 are designated 21, 22 and 23, respectively.
  • the outer side walls of corrugations 14, 15 and 16 are numbered 24, 25 and 26,
  • the upper surface of the diaphragm When assembled in a power element, the upper surface of the diaphragm is normally subjected to atmospheric pressure and the bottom surface is subjected to a pressure which is a function of some quantity to be measured.
  • the spacing between corresponding points of successive inner corrugations tends to decrease.
  • the distance between points 22 and 23 is less than the distance between points 21 and 22.
  • the distance between points 18 and 1 is less than the distance between points 17 and 18 and is greater than the distance between points 1*) and 20.
  • the height of the outer sides of the corrugations tends to increase in successive outer corrugations whereas the height of the inner sides of the corrugations tends to increase in successive inner corrugations.
  • the spacing, in a direction parallel to axis 30, between points 13 and 22 is less than that between points 17 and 21 and greater than that between points 19 and 23.
  • the spacing, thu measured, between points 22 and 19 is lessthan that between points 21 and 18 and is greater than that between points 23 and 2h.
  • the slope of the outer sides of the corrugations tends to decrease in successive inner corrugations but the slope of the inner sides of the corrugations tends to increase in successive inner corrugations.
  • Fig. 3 the numerals 17' through 30' correspond to numerals 17 through 39 in Fig. 2.
  • This chart does not iilustrate a diaphragm but is intended to show, in exaggerated form, the relationships between the sides and the top and bottom points of a diaphragm embodying the invention.
  • Pressurelinearity is defined as the characteristic of expansion of the diaphragm along its axis as a linear function of the differential of pressure uniformly applied on opposite sides of the diaphragm.
  • the diaphragm is pressure-linear for a given diaphragm sensitivity. Conversely, in a diaphragm of given sensitivity, substantial pressure-linearity is provided over a given range with less variation in corrugation slope and height if the change in width is increased.
  • Substantial pressure-linearity over a specified range may be achieved by various combinations of the degree in which particular ones of these structural features are present in the diaphragm shape.
  • the dominant feature may diifer in different combinations.
  • the number of corrugations in a diaphragm and the thickness and resilience of the diaphragm material are major factors in determining its sensitivity or ratio of incremental expansion to incremental change in pressure differential.
  • a pressure responsive diaphragm having formed therein a series of concentric corrugations, the slopes of the inner sides of which increase and the slopes of the outer sides of which decrease in successive inner corru gations for substantially linear expansion of said diaphragm in response to equal increments of pressure change over a given range of pressure uniformly applied thereto.
  • a pressure responsive diaphragm having formed therein a series of concentric corrugations the slopes of the inner sides of which increase in successive inner corrugations and the slopes of the outer sides of which decrease in successive inner corrugations and in which the cross-sectional width of successive inner corrugations is decreased for substantially linear expansion of said diaphragm in response to equal increments of change over a given range of pressure uniformly applied thereto.
  • a pressure responsive diaphragm having formed therein a series of concentric corrugations the slopes and the heights of the inner sides of which increase in successive inner corrugations and the slopes and the heights of the outer sides of which decrease in successive inner corrugations for substantially linear expansion of said diaphragm in response to equal increments of change over a given range of pressure uniformly applied thereto.

Description

June 26, 1956 c. R. SMiTH 2,751,935
DIAPHRAGM ELEMENTS Filed Dec. 13, 1954 United States Patent F DIAPi-BZAGM ELEDEENTS Charles R. Smith, Mequon, Wis., assignor to Cutler, er, Inc., Milwaukee, Wis, a corporation of Dela= ware Application December 13, 1954, Serial No. 474,952
9 Claims. (Cl. 137--795) This invention relates to pressure responsive diaphragm elements.
A primary object of the invention is to provide a diaphragm the expansion of which is substantially linear over a wide range of pressures uniformly applied thereto.
Another object is to provide a diaphragm which is pressure-linear over a wide range of applied pressures, which expands relatively greatly in respect to its diameter and which will withstand a large number of expansions without breaking.
A more specific object is to provide a self-loaded diaphragm which is pressure-linear over the range of domestic refrigerator power element operation and, in addition, is a size, durability, and cost commensurate with the requirement of domestic refrigeration service.
In the interval between manufacture of a refrigerator and the time when it is placed in service, the refrigerator, and its power element, may be transported and stored in places where temperature differentials are greater than those which the power element will experience during normal service. Accordingly self-loaded diaphragms which form a part of those power elements must be able to withstand greater pressure differentials than those to which they are subjected during normal service. Another object of the invention is to provide a diaphragm which can withstand such extreme pressure variations without loss of calibration in its normal operating range.
Other objects and advantages of the invention will hereinafter appear.
One embodiment of the invention is shown in the accompanying drawing, it being understood that certain modifications may be made in the embodiment illustrated and that other modifications are possible to be made without departing from the spirit of the invention or the scope of the appended claims.
In the drawings, Figure 1 is a top plan view of a diaphragm embodying the invention,
Fig. 2 is an enlarged sectional view taken on line 22 of Fig. l, and
Fig. 3 is a chart of certain of the structural features of the corrugations of the diaphragm greatiy exaggerated.
Referring to Figs. 1 and 2, the diaphragm there shown comprises a circular cup 16 the bottom wall of which is provided with a series of concentric corrugations and a central boss 12.
To facilitate description, that face of the diaphragm which is seen in Fig. 1 and which is seen from the top in Fig. 2 will be referred to as the top or upper side. The opposite side will be referred to as the bottom or lower side. Each corrugation will be considered as including that portion of the bottom of the cup which extends between successive low points. Thus, in Fig. 2, corrugation 14 extends from point 17 to point 18, corrugation 15 extends from point 18 to point 19 and corrugation 16 extends from point 19 to point 20. The uppermost or top points of corrugations 14, 15 and 16 are designated 21, 22 and 23, respectively. The outer side walls of corrugations 14, 15 and 16 are numbered 24, 25 and 26,
2,751,935 Patented June 26, 1956 ice respectively, and their inner side walls are numbered 27, 28 and 29, respectively. The construction line 30 lies in the axis of the diaphragm. Other unnumbered construction lines indicate the slopes of the sides of the corrugations. The numeral 31 designates the outer side wall of the diaphragm.
When assembled in a power element, the upper surface of the diaphragm is normally subjected to atmospheric pressure and the bottom surface is subjected to a pressure which is a function of some quantity to be measured.
The spacing between corresponding points of successive inner corrugations tends to decrease. Thus the distance between points 22 and 23 is less than the distance between points 21 and 22. Also, the distance between points 18 and 1 is less than the distance between points 17 and 18 and is greater than the distance between points 1*) and 20.
The amplitude or the height of the respective sides of any corrugation, measured in a direction parallel to the axis of the diaphragm from the bottom points to the top point, need not be the same. The height of the outer sides of the corrugations tends to increase in successive outer corrugations whereas the height of the inner sides of the corrugations tends to increase in successive inner corrugations. Thus the spacing, in a direction parallel to axis 30, between points 13 and 22 is less than that between points 17 and 21 and greater than that between points 19 and 23. Similarly the spacing, thu measured, between points 22 and 19 is lessthan that between points 21 and 18 and is greater than that between points 23 and 2h. The slope of the outer sides of the corrugations tends to decrease in successive inner corrugations but the slope of the inner sides of the corrugations tends to increase in successive inner corrugations.
In addition, successive inner corrugations tend to be positioned downwardly so that the corrugated portion of the diaphragm, when relaxed, is funnel shaped or bell shaped as indicated by construction line a and [9V drawn through the mid-points of the corrugations in Figs. 2 and 3, respectively. It will be apparent that at different ambient pressure differentials on opposite sides of the diaphragm that the diaphragm may or may not be funnel or bell shaped.
In the chart, Fig. 3, the numerals 17' through 30' correspond to numerals 17 through 39 in Fig. 2. This chart does not iilustrate a diaphragm but is intended to show, in exaggerated form, the relationships between the sides and the top and bottom points of a diaphragm embodying the invention.
The various structural features hereinbefore described contribute to make the diaphragm substantially pressurelinear over a wide range of applied pressures. Pressurelinearity is defined as the characteristic of expansion of the diaphragm along its axis as a linear function of the differential of pressure uniformly applied on opposite sides of the diaphragm.
It is apparent that certain of these structural features determine others of them so that the shape of the diaphragm may be defined as various combinations of these features. Accordingly, description of the effects of the various structural features on diaphragm performance, which efiects are themselves complex, is complicated by the fact that the features may be described in different combinations.
in general, substantial pressure-linearity is achieved by varying the heights of the inner and outer sides of the corrugations as described or by varying the slopes of said sides as described. The change in corrugation width and amplitude, as described, has the eflfect of increasing, to higher applied pressures, the range of pressures over relatively small.
which the diaphragm is pressure-linear for a given diaphragm sensitivity. Conversely, in a diaphragm of given sensitivity, substantial pressure-linearity is provided over a given range with less variation in corrugation slope and height if the change in width is increased.
Shaping the diaphragm to be somewhat funnel or bell shaped'in its relaxed condition permits increased diaphragm expansion with a of expansion and stress in the individual corrugations.
Substantial pressure-linearity over a specified range may be achieved by various combinations of the degree in which particular ones of these structural features are present in the diaphragm shape. The dominant feature may diifer in different combinations.
The number of corrugations in a diaphragm and the thickness and resilience of the diaphragm material are major factors in determining its sensitivity or ratio of incremental expansion to incremental change in pressure differential.
The dimensional changes in successive corrugations are small in small diaphragms of'the type described. Accordingly, tools for making such diaphragms must be accurately made. However, it is a feature of the invention that the amplitude of the corrugations may be made This reduces the need for accuracy in the tools and simplifies problems attendant upon deep drawing of the diaphragm material. It has been found that minor deviations in individual corrugations from the 7 crease in successive inner corrugations.
2. The diaphragm defined in claim 1 in which the crosssectional width decreases in successive inner corrugations.
3. The diaphragm defined in claim 2 in which corresponding points of successive inner corrugations define a funnel or bell shape when said diaphragm is relaxed.
4. A pressure responsive diaphragm having formed therein a series of concentric corrugations, the slopes of the inner sides of which increase and the slopes of the outer sides of which decrease in successive inner corru gations for substantially linear expansion of said diaphragm in response to equal increments of pressure change over a given range of pressure uniformly applied thereto.
5. A pressure responsive diaphragm having formed therein a series of concentric corrugations the slopes of the inner sides of which increase in successive inner corrugations and the slopes of the outer sides of which decrease in successive inner corrugations and in which the cross-sectional width of successive inner corrugations is decreased for substantially linear expansion of said diaphragm in response to equal increments of change over a given range of pressure uniformly applied thereto.
6. The diaphragm defined in claim 5 in which the amplitude of the inner side of said corrugations increases in successive inner corrugations for substantially linear expansion of said diaphragm over an increased range of pressures.
7. The diaphragm defined in claim 5 in which corresponding points of successive inner corrugations define a funnel or bell shape when said diaphragm is relaxed.
8. A pressure responsive diaphragm having formed therein a series of concentric corrugations the slopes and the heights of the inner sides of which increase in successive inner corrugations and the slopes and the heights of the outer sides of which decrease in successive inner corrugations for substantially linear expansion of said diaphragm in response to equal increments of change over a given range of pressure uniformly applied thereto.
9. The diaphragm defined in claim 8 in which the crosssectional width of the corrugations decreases in succes sive inner corrugations for substantially linear expansion of said diaphragm over an increased range of pressures.
References Cited in the file of this patent UNITED STATES PATENTS 1,927,617 Schmidt Sept. 19, 1933 2,111,168 Chansor Mar. 15, 1938 FOREIGN PATENTS 847,073 Germany Aug. 27, 1952
US474952A 1954-12-13 1954-12-13 Diaphragm elements Expired - Lifetime US2751935A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US474952A US2751935A (en) 1954-12-13 1954-12-13 Diaphragm elements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US474952A US2751935A (en) 1954-12-13 1954-12-13 Diaphragm elements

Publications (1)

Publication Number Publication Date
US2751935A true US2751935A (en) 1956-06-26

Family

ID=23885645

Family Applications (1)

Application Number Title Priority Date Filing Date
US474952A Expired - Lifetime US2751935A (en) 1954-12-13 1954-12-13 Diaphragm elements

Country Status (1)

Country Link
US (1) US2751935A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4314480A (en) * 1980-07-14 1982-02-09 Baxter Travenol Laboratories, Inc. Venous pressure isolator
US4867653A (en) * 1988-01-20 1989-09-19 Grace Inc. Diaphragm pump
US20040261860A1 (en) * 2003-06-24 2004-12-30 Kirchner Mark W. Flow control valves
US20070289640A1 (en) * 2006-04-27 2007-12-20 Sko Flo Industries, Inc. Flow control valve
US20100077852A1 (en) * 2008-09-30 2010-04-01 M&Fc Holding, Llc Gas metering diaphragm

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1927617A (en) * 1930-01-15 1933-09-19 Schmidt Rudolf Piston engine or piston pump
US2111168A (en) * 1935-03-04 1938-03-15 Chansor John Flexible corrugated diaphragm
DE847073C (en) * 1950-12-02 1952-08-21 J C Eckardt A G Diaphragm pressure gauge with a diaphragm spring that is corrugated or bent out in several circular shapes around its center

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1927617A (en) * 1930-01-15 1933-09-19 Schmidt Rudolf Piston engine or piston pump
US2111168A (en) * 1935-03-04 1938-03-15 Chansor John Flexible corrugated diaphragm
DE847073C (en) * 1950-12-02 1952-08-21 J C Eckardt A G Diaphragm pressure gauge with a diaphragm spring that is corrugated or bent out in several circular shapes around its center

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4314480A (en) * 1980-07-14 1982-02-09 Baxter Travenol Laboratories, Inc. Venous pressure isolator
US4867653A (en) * 1988-01-20 1989-09-19 Grace Inc. Diaphragm pump
US20040261860A1 (en) * 2003-06-24 2004-12-30 Kirchner Mark W. Flow control valves
US6932107B2 (en) 2003-06-24 2005-08-23 Flow Control Industries, Inc. Flow control valves
US20050211305A1 (en) * 2003-06-24 2005-09-29 Flow Control Industries, Inc. Flow control valves
US7128086B2 (en) 2003-06-24 2006-10-31 Flow Control Industries, Inc. Flow control valves
US20070289640A1 (en) * 2006-04-27 2007-12-20 Sko Flo Industries, Inc. Flow control valve
US7770595B2 (en) 2006-04-27 2010-08-10 Sko Flo Industries, Inc. Flow control valve
US8469053B2 (en) 2006-04-27 2013-06-25 SKO FLO Industries, Inc Flow control valve
US9383035B2 (en) 2006-04-27 2016-07-05 Sko Flo Industries, Inc. Flow control valve
US20100077852A1 (en) * 2008-09-30 2010-04-01 M&Fc Holding, Llc Gas metering diaphragm
US8104397B2 (en) 2008-09-30 2012-01-31 M&Fc Holding, Llc Gas metering diaphragm

Similar Documents

Publication Publication Date Title
US2283439A (en) Accumulator diaphragm
US2751935A (en) Diaphragm elements
US4157835A (en) Strip seal for stuffing box packing
KR880701372A (en) Differential pressure sensor and diaphragm
US3046788A (en) Fluid pressure electrical transducer
US4119123A (en) Flexible hose with wear indicator
US2261307A (en) Thermal insulating material
US2267164A (en) Snap acting condition responsive device
US848238A (en) Metallic hose.
US4018356A (en) Floating deck for liquid storage tank
US2761411A (en) Pressure indicating device
US3244227A (en) Plate type heat exchangers
US3187641A (en) Diaphragm
US3277718A (en) Electrical pressure transducer
US2888286A (en) Turbine apparatus
US2489322A (en) Liner for centrifugal casting molds
US2925829A (en) Bellows
US2879802A (en) Differential pressure-responsive device
US3782077A (en) Diffusion cell
US1813099A (en) Edible container
US2080429A (en) Aneroid condenser
US2015817A (en) Heat insulation for wall structures
US1698164A (en) Method of producing expansible collapsible elements
US1484141A (en) Expansible collapsible element
US1921312A (en) Thermostat