Diaphragm

• US 4,434,203 A
• Filed: 10/27/1980
• Issued: 02/28/1984
• Est. Priority Date: 10/27/1980
• Status: Expired due to Term

• Current Assignee: Setra Systems Incorporated (Fortive Corp.)
• Original Assignee: Setra Systems Incorporated (Fortive Corp.)
• Inventors: Briefer, Dennis K.
• Primary Examiner(s): Thibodeau, Paul J.
• Application Number:
  US06/200,790
• Time in Patent Office: 1,219 Days
• Field of Search: 428/152, 428/192, 428/179, 428/174, 428/64, 428/66, 179/181 R, 181/157, 181/165, 181/168, 181/167, 181/173, 181/174
• US Class Current: 428/152
• CPC Class Codes: G01L 9/0044 Constructional details of non-semiconductive diaphragms
• CPC Class Codes: Y10T 428/216 Ornamental, decorative, pattern, or indicia
• CPC Class Codes: Y10T 428/24446 Wrinkled, creased, crinkled or creped
• CPC Class Codes: Y10T 428/24628 Nonplanar uniform thickness material
• CPC Class Codes: Y10T 428/24777 Edge feature
• CPC Class Codes: Y10T 428/31678 Of metal

Abstract

A diaphragm having a pattern of wrinkles adapted so that the diaphragm is both radially and tangentially expandable with respect to a reference point in that central portion.

Claims

1. A diaphragm that flexes in a direction generally normal to said diaphragm in response to a pressure differential across the diaphragm, comprising:

a generally thin diaphragm member formed of a structural material that is substantially inelastic, said diaphragm member including a low energy collapse pattern of wrinkles that extend over a substantial portion of the diaphragm, each of said wrinkles being elongated over a short length in any one direction and having an amplitude greater than the thickness of the diaphragm but not projecting substantially from the plane of said diaphragm, said low energy collapse pattern also being such that the angular orientation of said elongated wrinkles varies over said diaphragm member and any axis lying in the plane of said diaphragm intersects at least one wrinkle to thereby relieve stresses induced in said diaphragm member by said pressure differential, whereby said diaphragm is both radially and tangentially expandable with respect to any reference point in the central portion thereof.

2. A diaphragm according to claim 1 wherein said central portion has an electrically conductive surface and wherein said conductive surface extends to the periphery of said diaphragm.

3. A diaphragm according to claim 1 wherein said diaphragm member includes a peripheral region adapted for supporting said diaphragm so that said central portion is substantially planar.

4. A diaphragm according to claim 1 wherein said wrinkle pattern of diaphragm includes a nominally planar portion and a plurality of wrinkle portions extending from at least one side of said planar portion.

5. A diaphragm according to claim 4 wherein said wrinkle portions extend from both sides of said planar portion.

6. A diaphragm according to claim 1 wherein the principal axes of said wrinkles are aligned substantially with one of three axes on the surface of said central portion, said axes being sixty degrees offset from each other.

7. A diaphragm according to claim 1 wherein the principal axes of said wrinkles are aligned substantially with one of two axes on the surface of the said central portion, said axes being ninety degrees offset from each other.

8. A diaphragm that flexes in a direction generally normal to said diaphragm in respnse to a pressure differential across the diaphragm, comprising:

a generally thin diaphragm member formed of a structural material that is substantially inelastic, said diaphragm member including a low energy collapse pattern of wrinkles that extend over a substantial portion of the diaphragm, each of said wrinkles being elongated over a short length in any one direction and having an amplitude greater than the thickness of the diaphragm but not projecting substantially from the plane of said diaphragm, said low energy collapse pattern being such that the angular orientation of said elongated wrinkles varies over said diaphragm member in a random manner and any axis lying in the plane of said diaphragm intersects at least one wrinkle to thereby relieve stresses induced in said diaphragm member by said pressure differential, whereby said diaphragm is both radially and tangentially expandable with respect to any reference point in the central portion thereof.

9. The diaphragm of claim 8 wherein said wrinkles are discontinuous.

10. The diaphragm according to claim 9 wherein said wrinkles are straight.

11. The diaphragm according to claim 9 wherein said wrinkles are each curved.

12. The diaphragm according to claim 11 wherein some of said wrinkles are continuous.

13. A diaphragm that flexes in a direction generally normal to said diaphragm in response to a pressure differential across the diaphragm, comprising:

a generally thin diaphragm member formed of a structural material that is substantially inelastic, said diaphragm member including a low energy collapse pattern of wrinkles that extend over a substantial portion of the diaphragm, each of said wrinkles being elongated over a short length in any one direction, straight and discontinuous, and having an amplitude greater than the thickness of the diaphragm but not projecting substantially from the plane of said diaphragm, said low energy collapse pattern being such that the angular orientation of said elongated wrinkles varies over said diaphragm member with the principal axes of said wrinkles being aligned generally with one of a plurality axes in the plane of said diaphragm such that any axis lying in the plane intersects at least one wrinkle to thereby relieve stresses induced in said diaphragm member by said pressure differential, whereby said diaphragm is both radially and tangentially expandable with respect to any reference point in the central portion thereof.

14. The diaphragm of claim 13 wherein said plurality is three and said axes are offset from one another by sixty degrees.

15. The diaphragm of claim 13 wherein said plurality is two and said axes are offset from one another by ninety degrees.

16. A diaphragm that flexes in a direction generally normal to said diaphragm in response to a pressure differential across the diaphragm, comprising:

a generally thin diaphragm member formed of a structural material that is substantially inelastic, said diaphragm member including a low energy collapse pattern of wrinkles that extend over a substantial portion of the diaphragm, each of said wrinkles being elongated over a short length in any one direction and having an amplitude greater than the thickness of the diaphragm but not projecting substantially from the plane of said diaphragm, said low energy collapse pattern being such that the angular orientation of said elongated wrinkles varies over said diaphragm member in a plurality of concentric zig-zag ring patterns where each of said wrinkles is a short, straight portion of one of said rings such that any axis lying in the plane of said diaphragm intersects at least one wrinkle to thereby relieve stresses induced in said diaphragm member by said pressure differential, whereby said diaphragm is both radially and tangentially expandable with respect to any reference point in the central portion thereof.

17. The diaphragm according to claim 16 wherein each of said rings of wrinkles is continuous.

18. The diaphragm according to claim 16 wherein at least some of said ring patterns are formed of wrinkles that are discontinuous.

19. The diaphragm according to claim 17 wherein interior angles of each of said ring patterns are 90 degrees.

20. The diaphragm according to claim 17 wherein interior angles of each of said ring patterns are 120 degrees.

21. The diaphragm according to claim 17 wherein inter-ring pattern separation is substantially constant.

22. A diaphragm that flexes in a direction generally normal to said diaphragm in response to a pressure differential across the diaphragm, comprising:

a generally thin diaphragm member formed of a structural material that is substantially inelastic, said diaphragm member including a low energy collapse pattern of wrinkles that extend over a substantial portion of the diaphragm, each of said wrinkles being elongated over a short length in any one direction, straight and having an amplitude greater than the thickness of the diaphragm but not projecting substantially from the plane of said diaphragm, said low energy collapse pattern being such that the angular orientation of said elongated wrinkles varies over said diaphragm member with the principal axes of said wrinkles being aligned generally with one of a plurality axes in the plane of said diaphragm such that any axis lying in the plane intersects at least one wrinkle to thereby relieve stresses induced in said diaphragm member by said pressure differential, whereby said diaphragm is both radially and tangentially expandable with respect to any reference point in the central portion thereof.

23. The diaphragm according to claim 22 wherein groups of said wrinkle are linear to form a wrinkle pattern that is a plurality of linear zig-zag patterns.

24. The diaphragm according to claim 23 wherein said linear zig-zag patterns are substantially parallel.

25. The diaphragm according to claim 23 wherein said linear zig-zag patterns are continuous.

26. The diaphragm according to claim 23 wherein said linear zig-zag patterns are discontinuous.