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US4619580A Expired / Lapsed US ⏱️ 0.0 years remaining

Variable camber vane and method therefor

Assignee: Boeing Co
•
Filing: 1983-09-08
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Granted: 1986-10-28
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Expires: 2003-09-08
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Abstract

Abstract A variable camber vane particularly suitable for use as a variable stator vane (20) has a secured root (22), a free tip (24) and a working face (26) disposed within and diverting flow of a working fluid, exhibiting temperature-responsive deflection of the tip as respects the root correllative to the temperature of the working fluid, is comprised of a sintered, generally laminar composite of a first amorphous metallic composition as a first vane element (32) and a second amorphous metallic composition as a second vane element (34), wherein the coefficients of thermal expansion for each of the compositions differ; whereby the camber of the vane varies in response to thermal variations of the working fluid.

Inventors

  • 👤 Howard E. Snyder

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 17:50
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/148; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 172 words
A variable camber vane having a first portion adapted to be secured to a mounting means, a second free tip portion spaced from said first secured portion, and a working face disposed within and diverting flow of a working fluid, for temperature-responsive deflection of said tip portion as respects said root coorelative to the temperature of said working fluid, said vane comprising: a. a sintered, generally laminar composite of a first amorphous metallic composition as a first vane element; b. a second amorphous metallic composition as a second vane element; c. said vane elements being characterized in that the coefficients of thermal expansion for each of said first and second compositions differ in a manner that the camber of said vane varies in response to thermal variations of said working fluid; d. each of said amorphous metallic compositions being an RSR amorphous metallic composition; e. each of said first and second vane elements being formed with an array of lateral surface grooves disposed generally along a flow path of said working fluid.
Claim 2
Dependent Claim 172 words
A variable camber vane having a first portion adapted to be secured to a mounting means, a second free tip portion spaced from said first secured portion, and a working face disposed within and diverting flow of a working fluid, for temperature-responsive deflection of said tip portion as respects said root coorelative to the temperature of said working fluid, said vane comprising: a. a sintered, generally laminar composite of a first amorphous metallic composition as a first vane element; b. a second amorphous metallic composition as a second vane element; c. said vane elements being characterized in that the coefficients of thermal expansion for each of said first and second compositions differ in a manner that the camber of said vane varies in response to thermal variations of said working fluid; d. each of said amorphous metallic compositions being an RSR amorphous metallic composition; e. each of said first and second vane elements being formed with an array of lateral surface grooves disposed generally along a flow path of said working fluid.
Claim 3
Dependent Claim 24 words
The variable camber vane of claim 1, wherein at least one of said amorphous metallic compositions further includes a coating of an environmentally-protective composition.
Claim 4
Dependent Claim 239 words
A vane assembly particularly adapted for use in an air breathing turbine engine, said vane assembly comprising: a. a first outer ring mounting member; b. a second inner ring mounting member disposed within said first member; c. a plurality of vane members mounted in an area between said first and second ring mounting members, each vane member being a variable camber vane, having a first secured portion by which it is mounted to said first and second ring mounting members, a second freetip portion spaced from said first secured portion, and a working face disposed within and diverting flow of a working fluid, for temperature responsive deflection of said tip portion as respects said root correlative to the temperature of said working fluid, each of said vane members comprising: i. a sintered, generally laminar composite of a first amorphous metallic composition as a first vane element; ii. a second amorphous metallic composition as a second vane element; iii. said vane elements being characterized in that the coefficients of thermal expansion for each of said first and second compositions differ in a manner that the camber of said vane varies in response to thermal variations of said working fluid; iv. each of said amorphous metallic compositions being an RSR amorphous metallic composition; v. each of said first and second vane elements being formed with an array of lateral surface grooves disposed generally along the flow path of said working fluid.
Claim 5
Dependent Claim 239 words
A vane assembly particularly adapted for use in an air breathing turbine engine, said vane assembly comprising: a. a first outer ring mounting member; b. a second inner ring mounting member disposed within said first member; c. a plurality of vane members mounted in an area between said first and second ring mounting members, each vane member being a variable camber vane, having a first secured portion by which it is mounted to said first and second ring mounting members, a second freetip portion spaced from said first secured portion, and a working face disposed within and diverting flow of a working fluid, for temperature responsive deflection of said tip portion as respects said root correlative to the temperature of said working fluid, each of said vane members comprising: i. a sintered, generally laminar composite of a first amorphous metallic composition as a first vane element; ii. a second amorphous metallic composition as a second vane element; iii. said vane elements being characterized in that the coefficients of thermal expansion for each of said first and second compositions differ in a manner that the camber of said vane varies in response to thermal variations of said working fluid; iv. each of said amorphous metallic compositions being an RSR amorphous metallic composition; v. each of said first and second vane elements being formed with an array of lateral surface grooves disposed generally along the flow path of said working fluid.
Claim 6
Dependent Claim 25 words
The vane assembly as recited in claim 3, wherein at least one of said amorphous metallic compositions further includes a coating of an environmentally-protective composition.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-10-27 1990-04-28 1990-10-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-10-27 1994-04-28 1994-10-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-10-27 1998-04-28 1998-10-28 $7700.00 Window Closed / Lapsed

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