Spring assemblies for use in gas turbine engines and methods for their manufacture

Patent metadata

Field	Value
Publication number	US-9562616-B2
Application number	US-201313742210-A
Country	US
Kind code	B2
Filing date	Jan 15, 2013
Priority date	Jan 15, 2013
Publication date	Feb 7, 2017
Grant date	Feb 7, 2017

Abstract

In accordance with an exemplary embodiment, a method for manufacturing a bypass valve of a turbine engine control system is described. The bypass valve includes a proportional valve and an integrator valve and the integrator valve includes an integrator spring assembly. The method includes forming the integrator spring assembly using an additive manufacturing technique. The integrator spring assembly comprises first and second end portions with a spring portion disposed between the first and second end portions. The first and second end portions and the spring portion are formed as an integral unit without welding or brazing using the additive manufacturing technique. The method further includes assembling the integrator spring assembly, the integrator valve, and the proportional valve into a complete bypass valve assembly.

First claim

What is claimed is:

1. A method for manufacturing a bypass valve of a turbine engine control system, the bypass valve comprising a proportional valve and an integrator valve, the integrator valve comprising an integrator spring assembly, the method comprising the steps of:
forming the integrator spring assembly using an additive manufacturing technique, wherein the integrator spring assembly comprises first and second end portions with a spring portion disposed between the first and second end portions, and wherein the first and second end portions and the spring portion are formed as an integral unit without welding or brazing using the additive manufacturing technique, wherein the step of forming the integrator spring assembly is further defined as forming a structure that comprises:
the spring portion disposed between the first end portion and the second end portion such that the first end portion is physically connected to a first end of the spring portion and the second end portion is physically connected to a second end of the spring portion,
wherein the spring portion comprises a helical coil having at least one spring pitch, wherein the spring portion comprises both of a variable pitch and a variable cross-sectional area, wherein the helical coil rotates about a central axis of the spring portion, and wherein the helical coil terminates at the first end portion and the second end portion;
wherein the first end portion and the second end portion each comprise a spring-facing surface that extends substantially perpendicular to the central axis of the spring portion, wherein the first end of the spring portion is connected to the first end portion at the spring-facing surface of the first end portion and wherein the second end of the spring portion is connected to the second end portion at the spring-facing surface of the second end portion, wherein the first and second ends of the spring portion have zero pitch such that they are oriented parallel to the respective spring facing surfaces of the first and second ends portions,

wherein the first end portion and the second end portion are physically connected to the spring portion without any weld or braze joints between the first or second end portions and the spring portion such that the integrator spring assembly is manufactured as an integral unit without any welding or brazing of the first end portion, the second end portion, or the spring portion using the additive manufacturing technique, and
the variable cross-sectional area being defined as a cross-section taken through the helical coil in a plane that also includes the central axis being different in shape at at least two different points along the helical coil, the at least two points being between the first and second ends of the spring portion, wherein the cross-section at each of the at least two different points is independently selected from the following group of two-dimensional shapes consisting of: 1) a first shape defined as having an enclosed perimeter with two sets of parallel, planar opposing sides, connected by curved edges, 2) a second shape defined as having an enclosed perimeter with one set of parallel, planar opposing sides, connected by curved edges, and 3) a third shape defined as having one set of planar opposing sides, wherein one of the planar sides is inclined at an angle and the other one of the planar sides is declined at the angle, the one set of planar opposing sides being connected by both a planar end and a curved end; and

assembling the integrator spring assembly, the integrator valve, and the proportional valve into a complete bypass valve assembly.

2. The method of claim 1 , wherein the additive manufacturing technique comprises direct metal laser sintering.

3. The method of claim 1 , wherein the additive manufacturing technique comprises electron beam melting.

4. The method of claim 1 , wherein the spring portion of the integrator spring assembly is formed so as to comprise a variable pitch, the variable pitch being defined as forming the helical coil having at least two different spring pitches.

5. The method of claim 1 , wherein the spring portion of the integrator spring assembly is formed so as to comprise a plurality of materials such that a first part of the spring portion is formed using a first material and a second part of the spring portion is formed using a second material that is different than the first material.

6. The method of claim 1 , wherein the spring portion of the integrator spring assembly is formed so as to comprise a first material and wherein at least one of the end portions of the integrator spring assembly is formed so as to comprise a second material that is different that the first material.

7. A spring assembly, comprising:
a first end portion;
a second end portion; and
a spring portion disposed between the first end portion and the second end portion such that the first end portion is physically connected to a first end of the spring portion and the second end portion is physically connected to a second end of the spring portion,
wherein the spring portion comprises a helical coil having at least one spring pitch, wherein the spring portion comprises both of a variable pitch and a variable cross-sectional area, wherein the helical coil rotates about a central axis of the spring portion, and wherein the helical coil terminates at the first end portion and the second end portion;
wherein the first end portion and the second end portion each comprise a spring-facing surface that extends substantially perpendicular to the central axis of the spring portion, wherein the first end of the spring portion is connected to the first end portion at the spring-facing surface of the first end portion and wherein the second end of the spring portion is connected to the second end portion at the spring-facing surface of the second end portion, wherein the first and second ends of the spring portion have zero pitch such that they are oriented parallel to the respective spring facing surfaces of the first and second ends portions,
wherein the first end portion and the second end portion are physically connected to the spring portion without any weld or braze joints between the first or second end portions and the spring portion such that the spring assembly is manufactured as an integral unit without any welding or brazing of the first end portion, the second end portion, or the spring portion, and
the variable cross-sectional area being defined as a cross-section taken through the helical coil in a plane that also includes the central axis being different in shape at at least two different points along the helical coil, the at least two points being between the first and second ends of the spring portion, wherein the cross-section at each of the at least two different points is independently selected from the following group of two-dimensional shapes consisting of: 1) a first shape defined as having an enclosed perimeter with two sets of parallel, planar opposing sides, connected by curved edges, 2) a second shape defined as having an enclosed perimeter with one set of parallel, planar opposing sides, connected by curved edges, and 3) a third shape defined as having one set of planar opposing sides, wherein one of the planar sides is inclined at an angle and the other one of the planar sides is declined at the angle, the one set of planar opposing sides being connected by both a planar end and a curved end.

8. The spring assembly of claim 7 , wherein the spring assembly is manufactured as an integral unit using additive manufacturing techniques.

9. The spring assembly of claim 7 , wherein the spring portion comprises a variable pitch, the variable pitch being defined as the hel

Assignees

• Honeywell Int Inc

Inventors

• Strom Laurie
• Godfrey Donald G
• Kington Harry Lester
• Hall Douglas
• Morris Mark C

Classifications

• F16F1/043

  the cross-section varying with the wire length · CPC title

• F16F1/047

  characterised by varying pitch · CPC title

• F16K17/048 Primary

  combined with other safety valves, or with pressure control devices · CPC title

• B22F12/30

  Platforms or substrates · CPC title

• B22F10/64

  by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title