Deformable turbine bearing mount for air turbine starter

Patent metadata

Field	Value
Publication number	US-10316756-B2
Application number	US-201615194900-A
Country	US
Kind code	B2
Filing date	Jun 28, 2016
Priority date	Jun 28, 2016
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

An air turbine starter includes a support structure and a turbine having a shaft and a rotor that extends away from the shaft in a radial direction. The air turbine starter also includes a mount structure that supports the turbine for rotation relative to the support structure. The mount structure is configured to transfer a force from the turbine to the support structure. The mount structure includes a deformable member that is configured to deform when the force exceeds a predetermined threshold.

First claim

What is claimed is:

1. An air turbine starter comprising:
a support structure;
a turbine that includes a shaft and a rotor that extends away from the shaft in a radial direction;
a mount structure that supports the turbine for rotation relative to the support structure, the mount structure configured to transfer a force from the turbine to the support structure, the mount structure including a plastically deformable member that is configured to plastically deform when the force exceeds a predetermined threshold.

2. The air turbine starter of claim 1 , wherein the deformable member is a frangible member that is configured to fracture when the force exceeds the predetermined threshold.

3. The air turbine starter of claim 2 , further comprising a cutter member that is fixed to the support structure; and
wherein the deformable member is configured to fracture and allow the turbine to move toward and impact the cutter member.

4. The air turbine starter of claim 3 , wherein the shaft of the turbine extends along a longitudinal axis;
wherein the cutter member includes a plurality of cutters that are arranged about the longitudinal axis, and wherein the plurality of cutters are spaced apart from the rotor with respect to the longitudinal axis; and
wherein the deformable member is configured to fracture and allow the turbine to move substantially along the longitudinal axis toward the cutter member so that at least one of the plurality of cutters impacts the rotor.

5. The air turbine starter of claim 4 , further comprising a containment member that is fixed relative to the support structure;
wherein the containment member is configured to contain the turbine as the turbine moves substantially along the longitudinal axis toward the cutter member.

6. The air turbine starter of claim 1 , wherein the deformable member is configured to plastically deform and allow the turbine to move substantially along the radial direction.

7. The air turbine starter of claim 1 , further comprising:
a sensor that observes a condition indicative of the plastic deformation of the deformable member and generates sensor signals based thereon;
a controller that receives and processes the sensor signals to determine the plastic deformation of the deformable member and generates a control signal based thereon; and
an output device that outputs a warning to a user indicative of the plastic deformation based on the control signal.

8. The air turbine starter of claim 1 , wherein the plastically deformable member is a crushable member that includes a plurality of voids, wherein the plastically deformable member is configured to crush when the force exceeds the predetermined threshold.

9. The air turbine starter of claim 1 , wherein the plastically deformable member includes a plurality of elongate radial members that extend in the radial direction, wherein at least one of the plurality of elongate radial members is configured to buckle when the force exceeds the predetermined threshold.

10. The air turbine starter of claim 1 , further comprising a bearing with an inner race, an outer race, and moveable bearing members disposed between the inner and outer races,
wherein the inner race is attached the shaft of the turbine, wherein the outer race is attached to the deformable member; and
wherein the deformable member is disposed between the support structure and the outer race.

11. The air turbine starter of claim 10 , further comprising a thrust member that extends from the support structure to the outer race of the bearing, the thrust member configured to support the outer race in a substantially fixed position along a longitudinal axis when the deformable member is in an undeformed configuration.

12. An air turbine starter comprising:
a support structure;
a turbine that includes a shaft and a rotor that extends away from the shaft in a radial direction;
a mount structure that supports the turbine for rotation relative to the support structure, the mount structure configured to transfer a force from the turbine to the support structure, the mount structure including a plastically deformable member that is configured to plastically deform when the force exceeds a predetermined threshold;
the deformable member including an inner member and an outer member that are separated by a plurality of transverse support members, the plurality of transverse support members extending substantially in the radial direction between the inner and outer members.

13. The air turbine starter of claim 12 , wherein at least some of the plurality of transverse support members include a frangible portion, the frangible portion configured to fracture when the force exceeds the predetermined threshold.

14. The air turbine starter of claim 13 , wherein the frangible portion of the at least some of the plurality of transverse support members are substantially aligned into an imaginary circle that extends about a longitudinal axis of the turbine.

15. A deformable member of a mount structure of an air turbine starter, the deformable member comprising:
an inner member configured to abut an outer race of a bearing, the bearing configured to support rotation of a turbine of the air turbine starter;
an outer member configured to fixedly attach to a support structure of the air turbine starter;
a transverse support member that extends between the inner member and the outer member, the transverse support member configured to transfer a force from the inner member to the outer member; and
a deformable portion configured to deform when the force exceeds a predetermined threshold.

16. The deformable member of claim 15 , wherein the deformable portion is defined on the transverse support member.

17. The deformable member of claim 16 , wherein the transverse support member is one of a plurality of transverse support members, wherein the plurality of transverse support members each extend between the inner member and the outer member;
wherein the deformable portion is one of a plurality of deformable portions, the deformable portions each included on a respective one of the plurality of transverse support members; and
wherein the plurality of deformable portions are aligned into an imaginary circle that extends about a longitudinal axis of the deformable member.

18. The deformable member of claim 15 , wherein the deformable portion is a frangible portion configured to fracture when the force exceeds the predetermined threshold.

19. The deformable member of claim 15 , wherein the deformable portion is a plastically deformable portion configured to plastically deform when the force exceeds the predetermined threshold.

Assignees

• Honeywell Int Inc

Inventors

• Gentile David P
• Zeiner Peter Kenneth

Classifications

• F05D2260/311

  of the frangible or shear type · CPC title

• F01D21/045

  special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

• F05D2220/50

  for auxiliary power units (APU's) · CPC title

• F02C7/277 Primary

  the starter being a {separate} turbine · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title