Eddy current sensor, eddy current sensor assembly, and polishing apparatus
US-2024399536-A1 · Dec 5, 2024 · US
US9103801B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9103801-B2 |
| Application number | US-200813124092-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 14, 2008 |
| Priority date | Oct 14, 2008 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
In a defect detection device for a turbine rotor blade, a recess is provided in a side surface of a web provided to the inner circumferential side of a stationary blade diaphragm where stationary blades are annularly arranged adjacent to turbine rotor blades. An eddy current probe is movably installed in the recess, and a rod provided with a signal line for transmitting a signal detected by the eddy current probe, connected to the eddy current prove, is set up to be movable through a hole in a turbine casing and an air gap formed in the stationary blade diaphragm. The eddy current probe is moved toward or away from the turbine rotor blade implanting portion, and a data analyzer determines the condition of a defect occurred in the turbine rotor blade implanting portion based on the signals detected by the eddy current probe.
Opening claim text (preview).
The invention claimed is: 1. A defect detection device for a turbine rotor blade having a turbine rotor blade implanting portion constructed by fitting a set of rotor grooves formed on a rotor disc portion of a turbine rotor and a set of blade grooves formed on a root portion of the turbine rotor blade, wherein the turbine rotor is rotatably installed inside a turbine casing, and around an outer circumference of the turbine rotor, a plurality of turbine rotor blades are annularly a…
Physics · mapped topic
Physics · mapped topic
Physics · mapped topic
Related publications grouped by family.
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Answers are generated from the same data shown on this page.