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US4468620A Expired / Lapsed US ⏱️ 0.0 years remaining

System for in situ checking of turbine engine blades with eddy current probe guidance apparatus

Assignee: Safran Aircraft Engines SAS
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Filing: 1981-10-16
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Granted: 1984-08-28
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Expires: 2001-10-16
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Abstract

Abstract A system for in situ checking of turbine engine blades consists of a frame bearing on its two opposite large sides two hooks and a stop that can cooperate with the edges of the airfoil portion. Parallel to these sides, the system is provided with two elements serving to guide a carriage which is driven by means of a notched belt and two pinions, of which one is connected to a motor. The carriage supports an elastic element at the end of which is attached a shoe housing the probe. On the side of the shoe is an inclined plane cooperating with an identical inclined plane formed in one of the hooks. The motor is reversible and is controlled by end-of-stroke contacts in the carriage.

Inventors

  • 👤 Jean F. Vaerman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 17:08
CPC Classifications
G; G01; G01N; G01N27/00; G01N27/72; G01N27/82; G01N27/90; G01N27/9013; G01N27/902

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 153 words
A system for the in situ checking of turbine engine blades by eddy currents, said system comprising: a frame including a first set of two parallel sides; positioning means on at least one of said sides for holding at least one of the edges of one of said blades; a detection probe; means connected to said frame and supporting said probe for rectilinear guidance of said probe parallel to said positioning means; and means connected to said frame for displacement of said probe along said means for rectilinear guidance, wherein said positioning means comprises: two C-shaped hook portions on one of said sides of said frame, a line extending between said hook portion being parallel to said one of said sides; and a stop attached to the other of said two sides, wherein the distance between said hook portions and said stop is substantially equal to the width of one of said blades.
Claim 2
Independent Claim 153 words
A system for the in situ checking of turbine engine blades by eddy currents, said system comprising: a frame including a first set of two parallel sides; positioning means on at least one of said sides for holding at least one of the edges of one of said blades; a detection probe; means connected to said frame and supporting said probe for rectilinear guidance of said probe parallel to said positioning means; and means connected to said frame for displacement of said probe along said means for rectilinear guidance, wherein said positioning means comprises: two C-shaped hook portions on one of said sides of said frame, a line extending between said hook portion being parallel to said one of said sides; and a stop attached to the other of said two sides, wherein the distance between said hook portions and said stop is substantially equal to the width of one of said blades.
Claim 3
Dependent Claim 14 words
The system of claim 1 wherein said means for displacement include a drive motor.
Claim 4
Dependent Claim 63 words
The system of claim 1 wherein said frame includes a second set of two parallel sides, and wherein said means for guidance further comprise two parallel elements, each having one end attached to one of said sides of said second set of parallel sides of said frame, said first portion of said means for rectilinear guidance being movable on said two parallel elements.
Claim 5
Dependent Claim 67 words
The system of claim 3 wherein said first portion of said means for rectilinear guidance comprises: a carriage movably cooperating with said two parallel elements; an elastic element having one end cooperating with said carriage; and a shoe holding said probe, said shoe being attached to the other end of said elastic element such that it is able to contact a blade mounted in said positioning means.
Claim 6
Dependent Claim 46 words
The system of claim 4 wherein said means for displacement comprises: a coupling element fixed to said first portion of said means for rectilinear guidance; a rectilinear movement transmission system connected between said frame and said coupling element; and a drive motor for said transmission system.
Claim 7
Dependent Claim 57 words
The system of claim 5 wherein said transmission system comprises: two pinions, one of said two pinions being mounted on each end of one of said sides of said first set of parallel sides; a notched belt mounted on said pinions and cooperating with said coupling element; and a two directional motor driving one of said pinions.
Claim 8
Dependent Claim 54 words
The system of claim 4 wherein said shoe includes an inclined plane portion and one of said hook portions includes a mating inclined plane portion, whereby said shoe is held by said one of said hook portions and away from said plane when said carriage is adjacent an end of said two parallel elements.
Claim 9
Dependent Claim 20 words
The system of claim 6 including: stopping means for the end positions of said carriage; and motor direction control means.

References Cited (Backward Citations)

US2937522A Cited
US3588683A Cited
US3537300A Cited
FR2051987A5 Cited
US3570304A Cited
US3739262A Cited
DE2603336A1 Cited
US4142154A Cited
US4270089A Cited
US4304133A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-08-28 1988-02-27 1988-08-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-08-28 1992-02-27 1992-08-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-08-28 1996-02-27 1996-08-28 $7700.00 Window Closed / Lapsed

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