Torsion spring internal damper

Patent metadata

Field	Value
Publication number	US-9926851-B2
Application number	US-201514639220-A
Country	US
Kind code	B2
Filing date	Mar 5, 2015
Priority date	Apr 10, 2014
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A spring assembly has a spring end for engagement with a component to bias the component in a first direction. The spring end is connected to a plurality of coils, which have an inner peripheral surface, and are mounted about a pivot pin. A damper is positioned between an outer peripheral surface on the pivot pin and the inner peripheral surface of the spring coils. The damper is engaged by the spring coils, if the spring end is driven in a direction opposed to the first direction. A one-way drive assembly and a gas turbine engine are also disclosed.

First claim

The invention claimed is:

1. A one-way drive assembly comprising:
at least one pawl with a counterweight on one side of a pivot pin and an engaging pawl end on an opposed side of said pivot pin;
said at least one pawl rotating with a shaft, a housing having a ratchet to receive said pawl end, and prevent rotation of said shaft in an undesired direction;
a spring end for engagement with said at least one pawl to bias said at least one pawl in a first direction and said spring end being connected to a plurality of coils, said coils having an inner peripheral surface, and said coils being mounted about said pivot pin;
a damper positioned between an outer peripheral surface on said pivot pin and said inner peripheral surface of said spring coils, with said damper being engaged by said spring coils, if said spring end is driven in a direction opposed to said first direction; and
when said spring end is driven in a direction opposed to said first direction, said plurality of coils is compressed, and an inner diameter of said plurality of coils shrinks and said damper is squeezed between said plurality of coils and said pin, to dampen motion of said plurality of coils.

2. The drive assembly as set forth in claim 1 , wherein said damper has a plurality of damper coils.

3. The drive assembly as set forth in claim 2 , wherein said damper coils are generally cylindrical in cross-section.

4. The drive assembly as set forth in claim 2 , wherein said damper coils have a part-circular portion shape.

5. The drive assembly as set forth in claim 2 , wherein said damper coils have a generally diamond shape in cross-section.

6. The drive assembly as set forth in claim 1 , wherein said damper is formed of at least one of a polymer or an elastomer.

7. The drive assembly as set forth in claim 1 , wherein said damper coils are closely received between said outer periphery of said pivot pin and said inner periphery of said spring coils.

8. The drive assembly as set forth in claim 1 , wherein said damper is a cylindrical sleeve.

9. A gas turbine engine comprising:
a turbine driving a fan and a bearing for mounting a turbine shaft, said turbine having a one-way drive to prevent reverse rotation of a shaft leading into said turbine by said fan;
at least one pawl with a counterweight on one side of a pivot pin and an engaging pawl end on an opposed side of said pivot pin;
said at least one pawl rotating with said shaft, a housing having a ratchet to receive said pawl end, and prevent rotation of said shaft in an undesired direction;
a spring end for engagement with said at least one pawl to bias said at least one pawl in a first direction and said spring end being connected to a plurality of coils, said coils having an inner peripheral surface, and said coils being mounted about said pivot pin;
a damper positioned between an outer peripheral surface on said pivot pin and said inner peripheral surface of said spring coils, with said damper being engaged by said spring coils, if said spring end is driven in a direction opposed to said first direction; and
when said spring end is driven in a direction opposed to said first direction, said plurality of coils is compressed, and an inner diameter of said plurality of coils shrinks and said damper is squeezed between said plurality of coils and said pin, to dampen motion of said plurality of coils.

10. The gas turbine engine as set forth in claim 9 , wherein said damper has a plurality of damper coils.

11. The gas turbine engine as set forth in claim 10 , wherein said damper coils are generally cylindrical in cross-section.

12. The gas turbine engine as set forth in claim 10 , wherein said damper coils have a part-circular portion shape.

13. The gas turbine engine as set forth in claim 10 , wherein said damper coils have a generally diamond shape in cross-section.

14. The gas turbine engine as set forth in claim 9 , wherein said damper is closely received between said outer periphery of said pivot pin and said inner periphery of said spring coils.

15. The gas turbine engine as set forth in claim 9 , wherein said damper is formed of at least one of a polymer or an elastomer.

16. The gas turbine engine as set forth in claim 9 , wherein said damper is a cylindrical sleeve.

Assignees

• United Technologies Corp

Inventors

• Anglin Christopher T
• Kurz Leslie Charles

Classifications

• F16F1/042

  characterised by the cross-section of the wire · CPC title

• F01D25/04

  Antivibration arrangements · CPC title

• F05D2260/403

  through the shape of the drive components · CPC title

• F16D41/12

  with hinged pawl co-operating with teeth, cogs, or the like (F16D41/02, F16D41/24 take precedence) · CPC title

• F02C3/04

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title