Variable camber vane and method therefor

• US 4,619,580 A
• Filed: 09/08/1983
• Issued: 10/28/1986
• Est. Priority Date: 09/08/1983
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Snyder, Howard E.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US06/530,985
• Time in Patent Office: 1,146 Days
• Field of Search: 415/12, 415/48, 416/39, 416/229 R, 416/229 A, 416/38
• US Class Current: 415/12
• CPC Class Codes: F01D 5/148 Blades with variable camber, e.g. by ejection of fluid
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

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.

Claims

1. 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.

2. 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.

3. 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.

4. 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.