Gap measurement device

• US 5,760,593 A
• Filed: 02/14/1996
• Issued: 06/02/1998
• Est. Priority Date: 02/14/1996
• Status: Expired due to Term

• Current Assignee: nVent Solutions (UK) Ltd. (nVent Electric Plc)
• Original Assignee: BICC Public Limited Company
• Inventors: Sheard, Anthony Geoffrey, Lawrence, David Charles
• Primary Examiner(s): Ryan, Patrick
• Assistant Examiner(s): LAM, CATHY FONG FONG
• Application Number:
  US08/615,372
• Time in Patent Office: 839 Days
• Field of Search: 342/661, 342/662, 342/220, 342/207.15, 342/207.16, 33/544.4, 33/613, 33/656, 73/117.3, 73/660, 73/661, 250/559.31, 348/135, 376/245, 376/258
• US Class Current: 324/662
• CPC Class Codes: G01B 7/14 for measuring distance or clearance between spaced objects or spaced apertures G01B7/30 takes precedence

Abstract

This invention provides a device for capacitively measuring the distance to an object, which comprises an electrode that will couple capacitively with the object, a shield that surrounds the electrode and is electrically isolated from the electrode by means of insulation, and a layer of insulation that surrounds the shield, wherein the insulation between the electrode and the shield, and the insulation that surrounds the shield, are formed by deposition.

This invention further provides a method for measuring the distance to a solid object, which comprises forming an electrode that will capacitively couple with the object, depositing a layer of insulation over at least part of the electrode so that the insulation surrounds the electrode, depositing a layer of metal over the insulation to form a shield, and depositing a second layer of insulation over the shield.

Claims

1. A device for capacitively measuring the distance between a turbine blade in a turbine and another part of the turbine which comprises

an electrode that will couple capacitively with the turbine blade, said electrode having a part which faces the turbine blade,

a deposited electrically conductive layer on said part which faces the turbine blade,

a shield that surrounds the electrode except where the electrically conductive layer is located,

a deposited ceramic coating of insulation between said electrode and said shield such that said shield is electrically isolated from the electrode by means of said insulation, and

a deposited ceramic layer of insulation that surrounds the shield.

2. A device as claimed in claim 1, which contains the shield as a preformed part, and the insulation between the electrode and the shield, and the insulation that surrounds the shield, have both been formed on the shield by deposition.

3. A device as claimed in claim 1, wherein the insulation located between the electrode and the shield has been deposited on the electrode.

4. A device as claimed in claim 3, wherein the shield has been formed on the insulation deposited on the electrode by deposition.

5. A device as claimed in claim 4, wherein the insulation that surrounds the shield has been formed on the shield by deposition.

6. A device as claimed in claim 5, wherein the electrode is formed as a solid body of metal.

7. A device as claimed in claim 5, wherein the electrode comprises a solid body of a ceramic on which an electrically conductive layer has been deposited.

8. A device as claimed in claim 7, wherein the deposited electrically conductive layer on that part of the electrode that faces the turbine blades has a thickness of at least 0.5 mm.

9. A device as claimed in claim 8, wherein the deposited layer of insulation comprises an oxide or nitride of a metal or metalloid.

10. A device as claimed in claim 9, wherein any deposited layer has been deposited by a vacuum deposition method.

11. A device as claimed in claim 10, wherein any deposited layer has been formed by a chemical vapour deposition method, a sputtering method or a plasma deposition method.

12. A device as claimed in claim 1, wherein the deposited electrically conductive layer of that part of the electrode that faces the turbine blades is of a relatively low density, porous metal that is relatively soft so that said conductive layer can be abraded by the turbine blades, thereby forming a small and controllable gap therebetween.

13. A device as claimed in claim 12, wherein the deposited electrically conductive layer on that part of the electrode that faces the turbine blades is about 1 mm.

14. A device as claimed in claim 1, wherein the deposited electrically conductive layer on that part of the electrode that faces the turbine blades is of a metal/ceramic composite that is relatively soft so that said conductive layer can be abraded by the turbine blades, thereby forming a small and controllable gap therebetween.

15. A device as claimed in claim 1, wherein the deposited electrically conductive layer on that part of the electrode that faces the turbine blades is about 1 mm.