Electromechanical rotary actuator and method

Patent metadata

Field	Value
Publication number	US-9407121-B2
Application number	US-201213484689-A
Country	US
Kind code	B2
Filing date	May 31, 2012
Priority date	May 31, 2012
Publication date	Aug 2, 2016
Grant date	Aug 2, 2016

Abstract

An electromechanical rotary actuator including a housing including first end that extends to a second end through an intermediate portion that defines a longitudinal axis, and an internal cavity. An electric motor is arranged within the internal cavity. The electric motor includes a shaft having first shaft end and a second shaft end. A drive member is arranged within the housing along the longitudinal axis. The drive member includes an input shaft operatively coupled to the first shaft end and an output shaft. An output shaft member is coupled to the output shaft of the drive member. At least one bearing assembly supports one of the output shaft member and the first shaft end, and a preload member is arranged within the housing and configured to apply a compressive axial force to the at least one bearing, the drive member and the electric motor.

First claim

What is claimed is:

1. An electromechanical rotary actuator comprising:
a housing including a first end that extends to a second end through an intermediate portion that defines a longitudinal axis, the housing defining an internal cavity;
an electric motor arranged within the internal cavity, the electric motor including a stator and a rotor, the rotor surrounding a shaft having a first shaft end and a second shaft end;
a drive member arranged within the housing along the longitudinal axis, the drive member including an input shaft operatively coupled to the first shaft end and an output shaft;
an output shaft member coupled to the output shaft of the drive member, the output shaft member extending out from the first end of the housing and being configured and disposed to rotate about the longitudinal axis;
at least one bearing assembly supporting one of the output shaft and the first shaft end; and
a preload member arranged within the housing and configured to apply a compressive axial force to the at least one bearing, the drive member and the electric motor, the preload member accommodating thermal expansion of the electromechanical rotary actuator along the longitudinal axis; and
a resolver operatively coupled to the one of the input shaft and the output shaft of the drive member;
wherein the at least one bearing assembly includes a first bearing assembly supporting the first shaft end and a second bearing assembly supporting the output shaft member, and an end bearing assembly arranged to support the second shaft end, the first and second bearing assemblies being subjected to the compressive axial force.

2. The electromechanical rotary actuator according to claim 1 , wherein the preload member comprises a spring arranged adjacent the first bearing assembly.

3. The electromechanical rotary actuator according to claim 2 , further comprising: a spring housing extending about the spring and abutting an outer race of the first bearing assembly, the spring housing being subjected to the compressive axial force.

4. The electromechanical rotary actuator according to claim 3 , further comprising an end cap provided at the first end of the housing, the end cap including an opening that receives the output shaft member.

5. The electromechanical rotary actuator according to claim 4 , further comprising: a seal ring arranged between the end cap and the spring, the seal ring being subjected to the compressive axial force.

6. The electromechanical rotary actuator according to claim 1 , further comprising: a first bearing housing extending about the first bearing assembly and abutting the stator of the electric motor, the first bearing housing being subjected to the compressive axial force.

7. The electromechanical rotary actuator according to claim 1 , further comprising: a spacer arranged between the first bearing assembly and the drive member, the spacer being subjected to the compressive axial force.

8. The electromechanical rotary actuator according to claim 1 , further comprising: a second bearing housing extending about the second bearing assembly and abutting the drive member, the second bearing housing being subjected to the compressive axial force.

9. The electromechanical rotary actuator according to claim 1 , further comprising: an end bearing housing extending about the end bearing assembly and abutting the resolver, the end bearing housing being subjected to the compressive axial force.

10. The electromechanical rotary actuator according to claim 1 , wherein the drive member comprises a harmonic drive gear box.

11. The electromechanical rotary actuator according to claim 1 , wherein the electric motor comprises a brushless electric motor.

12. The electromechanical rotary actuator according to claim 1 , wherein the housing is arranged within a rotor blade of a rotary aircraft and the output shaft is coupled to a trailing edge effector.

Assignees

• Matalanis Claude G
• Kuczek Andrzej Ernest
• Jonsson Ulf J
• Wake Brian E
• Chaudhry Zaffir A
• Brewer Paul
• Hamilton Sundstrand Corp

Inventors

• Matalanis Claude G
• Kuczek Andrzej Ernest
• Jonsson Ulf J
• Wake Brian E
• Chaudhry Zaffir A
• Brewer Paul

Classifications

• H02K5/1732 Primary

  radially supporting the rotary shaft at both ends of the rotor (H02K5/1737 takes precedence) · CPC title

• H02K7/14 Primary

  Structural association with mechanical loads, e.g. with hand-held machine tools or fans (with fan or impeller for cooling the machine H02K9/06) · CPC title

• Y10T29/49009

  Dynamoelectric machine · CPC title

• Y02T50/30

  Wing lift efficiency · CPC title

• B64C27/615 Primary

  including flaps mounted on blades · CPC title