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US3757424A Expired / Lapsed US ⏱️ 0.0 years remaining

Classification gage for turbine vanes

Assignee: Chromalloy American Corp
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Filing: 1970-11-05
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Granted: 1973-09-11
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Expires: 1990-11-05
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Abstract

Abstract The invention contemplates a gage for vane-class measurement, in which the vane is oriented in space, and in which class is determined by a single angular measurement. The angular measurement is taken about a longitudinal axis which may be considered to be substantially the trailing-edge gage line, and said measurement is made between (a) a radial strobe through substantially the mid-point of the airfoil gage line (along the convex surface of the blade of the vane) and (b) a radial strobe parallel to the orientation of one of the abutment edges of a buttress forming part of the vane. Various structural features enable simple and rapid one-handed manipulation of each successive vane into gaging position, so that the angular (classindicating) measurement is fully repeatable for a given vane, and so that small and minor local anomalies in surface fidelity are substantially eliminated, i.e., they are not effective in degrading the reliability of the measurement.

Inventors

  • 👤 E Palmenberg

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 04:40
CPC Classifications
G; G01; G01B; G01B5/00; G01B5/20; G01B5/205

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 427 words
Gage means for observing class in a turbine vane which comprises an airfoil blade having a span extending longitudinally between fixed outer and inner buttresses, said blade having a convex surface referenced to an airfoil gage line extending between said buttresses and having a concave surface referenced at its trailing edge to a trailing-edge gage line, one of said buttresses including a wall extending generally transverely of said blade at juncture thereto and having opposed substantially flat elongated abutment surfaces for nested abutment with corresponding adjacent surfaces of the next adjacent vane when in shrouded assembly about a turbine axis; said gage means comprising a rigid frame, trailing-edge support means carried by said frame at longitudinally spaced locations for stabilized support of the trailing edge of the vane, said support means at each of said locations comprising first and second elongated abutments that are generally transversely oriented with respect to each other and with respect to the axis of longitudinal spacing, the first abutments at said locations being substantially parallel to each other and the second abutments at said locations being substantially parallel to each other, whereby said trailing-edge support means affords an applied blade a limited region of angularly rockable displacement of the blade about a rocking axis substantially coincident with the trailingedge gage line; a fixed stop longitudinally offset in a first direction from said support means and projecting from a part of said frame to intercept part of the inner wall of one buttress and thus determine a lateral location for rockable trailing-edge support; second stop means including blade-contacting means movably carried by said frame and offset from the rocking axis for contact with the convex blade surface, said second stop means also including a buttress contact movably mounted on said frame for engaging the inner wall of the other buttress, said bladecontacting means and said movable buttress contact being mechanically coupled for cooperative displacement so that the displaced position of one determines the displaced position of the other, and said offset being such as to position said bladecontacting means for localized contact with the convex blade surface substantially at the airfoil gage line thereof; and means for measuring with respect to a predetermined reference on said frame the angular orientation of one of the abutment surfaces of one of the buttresses, when the blade is limited in said rocking displacement, upon contact by the movable buttress contact with the inner wall of the other buttress; whereby the measured angle may be substantially indicative of class of vanes successively observed by aid gage means.
Claim 2
Dependent Claim 427 words
Gage means for observing class in a turbine vane which comprises an airfoil blade having a span extending longitudinally between fixed outer and inner buttresses, said blade having a convex surface referenced to an airfoil gage line extending between said buttresses and having a concave surface referenced at its trailing edge to a trailing-edge gage line, one of said buttresses including a wall extending generally transverely of said blade at juncture thereto and having opposed substantially flat elongated abutment surfaces for nested abutment with corresponding adjacent surfaces of the next adjacent vane when in shrouded assembly about a turbine axis; said gage means comprising a rigid frame, trailing-edge support means carried by said frame at longitudinally spaced locations for stabilized support of the trailing edge of the vane, said support means at each of said locations comprising first and second elongated abutments that are generally transversely oriented with respect to each other and with respect to the axis of longitudinal spacing, the first abutments at said locations being substantially parallel to each other and the second abutments at said locations being substantially parallel to each other, whereby said trailing-edge support means affords an applied blade a limited region of angularly rockable displacement of the blade about a rocking axis substantially coincident with the trailingedge gage line; a fixed stop longitudinally offset in a first direction from said support means and projecting from a part of said frame to intercept part of the inner wall of one buttress and thus determine a lateral location for rockable trailing-edge support; second stop means including blade-contacting means movably carried by said frame and offset from the rocking axis for contact with the convex blade surface, said second stop means also including a buttress contact movably mounted on said frame for engaging the inner wall of the other buttress, said bladecontacting means and said movable buttress contact being mechanically coupled for cooperative displacement so that the displaced position of one determines the displaced position of the other, and said offset being such as to position said bladecontacting means for localized contact with the convex blade surface substantially at the airfoil gage line thereof; and means for measuring with respect to a predetermined reference on said frame the angular orientation of one of the abutment surfaces of one of the buttresses, when the blade is limited in said rocking displacement, upon contact by the movable buttress contact with the inner wall of the other buttress; whereby the measured angle may be substantially indicative of class of vanes successively observed by aid gage means.
Claim 3
Dependent Claim 54 words
Gage means according to claim 1, in which said trailing-edge support means comprises spaced upwardly extending parallel abutment bars and spaced horizontally extending parallel abutment bars, all said bars extending generally transverse to the trailing edge, whereby a limited region of angular rocking displacement of the blade is afforeded by said trailing-edge support means.
Claim 4
Dependent Claim 26 words
Gage means according to claim 1, in which said movable buttress contact is mounted for displacement substantially normal to the inner wall of said other buttress.
Claim 5
Dependent Claim 29 words
Gage means according to claim 3, in which said second stop means includes a frame-pivoted linkage in the mechanical coupling of said blade-contacting means to said movable buttress contact.
Claim 6
Dependent Claim 61 words
Gage means according to claim 1, in which said blade-contacting means comprises rocker-arm means having two spaced blade-contacting elements which are aligned for localized engagement with the convex blade surface at points substantially along the airfoil gage line thereof, said mechanical coupling being from said movable buttress contact and including a movable member with a pivot connection to said rocker-arm means.
Claim 7
Dependent Claim 50 words
Gage means according to claim 5, in which a trailing-edge support means comprises rocker-arm means wherein the first elongated abutments at each of the longitudinally spaced locations of stabilized support are at spaced locations along said last-mentioned rocker-arm means, the pivot axes of both said rocker-arm means being substantially parallel.
Claim 8
Dependent Claim 47 words
Gage means according to claim 6, in which the rocker-arm means of said trailing-edge support means comprises two laterally spaced rocker arms, the spaced first elongated abutments at each of the longitudinally spaced locations of stabilized support being at the outer ends of each of said arms.
Claim 9
Dependent Claim 51 words
Gage means according to claim 7, in which said second elongated abutments are spaced parallel horizontal frame-based rods to provide a vertical component of trailing-edge support, said first elongated abutments being vertical pins carried at the respective ends of said two rocker arms to provide a horizontal component of trailing-edge support.
Claim 10
Dependent Claim 74 words
Gage means according to claim 5, in which said blade-contacting means comprises two laterally spaced rocker arms each having two spaced blade-contacting elements which are aligned for localized engagement with the convex blade surface at points substantially along the airfoil gage line thereof, said mechanical coupling including a third rocker arm having spaced pivotal connections to said first two rocker arms, and said movable member having a pivot connection to said third rocker arm.
Claim 11
Dependent Claim 43 words
Gage means according to claim 1, in which said means for measuring includes a buttress contacting bar having two spaced buttress-contacting elements, the direction of the effective spacing of said spaced buttress-contacting elements being in substantially a radial plane about the pivot axis.
Claim 12
Dependent Claim 29 words
Gage means according to claim 10, in which said buttress-contacting bar is part of an element of a quadrilateral four-bar linkage pivoted at one corner thereof to said frame.
Claim 13
Dependent Claim 40 words
Gage means according to claim 11, in which an angle indicator carried by said frame includes a probe tracking the instantaneous position of that element of said four-bar linkage which is opposite said bar elemenT with said buttress contacting feature.
Claim 14
Dependent Claim 34 words
Gage means according to claim 1, in which said means for measuring includes buttress-contacting pivoted means on a frame-fixed pivot axis for self-adapting angular positioning by said one abutment surface of said one buttress.

References Cited (Backward Citations)

US3464119A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-09-10 1977-03-12 1977-09-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-09-10 1981-03-12 1981-09-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-09-10 1985-03-12 1985-09-11 $7700.00 Window Closed / Lapsed

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