Rotating assembly including a dynamic balancing system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F16F-015/14
G01M-003/08
B64C-011/00
출원번호
US-0650298
(2012-10-12)
등록번호
US-8955409
(2015-02-17)
발명자
/ 주소
Carvalho, Paul A.
출원인 / 주소
Hamilton Sundstrand Corporation
대리인 / 주소
Cantor Colburn LLP
인용정보
피인용 횟수 :
1인용 특허 :
15
초록▼
A rotating assembly includes a shaft having a driven end and a driving end. At least one rotating member coupled to the driven end. A support member is operatively connected to the at least one rotating member. A dynamic balancing system is operatively coupled to the support member. The dynamic bala
A rotating assembly includes a shaft having a driven end and a driving end. At least one rotating member coupled to the driven end. A support member is operatively connected to the at least one rotating member. A dynamic balancing system is operatively coupled to the support member. The dynamic balancing system includes a first balancing weight rotatably mounted to the support member. The first balancing weight is operatively connected to a first motor. A second balancing weight is rotatably mounted to the support member. The second balancing weight is operatively connected to a second motor. A controller is operatively connected to the first and second motors. The controller is configured and disposed to signal each of the first and second motors to rotate and to establish a desired position of the first balancing weight and the second balancing weight relative to at least one rotating member.
대표청구항▼
1. A propeller system comprising: a shaft including a driven end and a driving end;at least one propeller operatively coupled to the driven end, and a support member operatively connected to the at least one propeller; anda dynamic balancing system operatively connected to the support member, the dy
1. A propeller system comprising: a shaft including a driven end and a driving end;at least one propeller operatively coupled to the driven end, and a support member operatively connected to the at least one propeller; anda dynamic balancing system operatively connected to the support member, the dynamic balancing system comprising: a first balancing weight member rotatably mounted to the support member, the first balancing weight member being operatively connected to a first motor arranged on a motor support, the first balancing weight member being arranged between the at least one propeller and the first motor;a first ring gear extending through the motor support and operatively engaging the first balancing weight member;a second balancing weight member rotatably mounted to the support member, the second balancing weight member being operatively connected to a second motor arranged on the motor support, the second balancing weight member being arranged between the at least one propeller and the second motor;a second ring gear extending through the motor support and operatively engaging the second balancing weight member; anda controller operatively connected to the first and second motors, the controller being configured and disposed to signal each of the first and second motors to rotate and to establish a desired position of the first balancing weight member and the second balancing weight member relative to the at least one propeller to reduce system vibration. 2. The propeller system according to claim 1, further comprising: a sensor configured and disposed to sense vibrations at the shaft, the controller being configured and disposed to rotate and establish the desired position of the first balancing weight member and second balancing weight member relative to the at least one propeller to reduce vibrations perceived at the sensor. 3. The propeller system according to claim 1, wherein each of the first and second motors rotate with the at least one propeller. 4. The propeller system according to claim 1, wherein the first and second balancing weight members and first and second motors are co-located with the at least one propeller. 5. The propeller system according to claim 4, further comprising: a hub member extending across the support member and portions of the at least one propeller, the first and second motors and the first and second balancing weight members being housed within the hub member. 6. The propeller system according to claim 1, wherein the first balancing weight member includes a first base portion, a first arm portion extending from the first base portion, and a first balancing weight being coupled to the first arm portion. 7. The propeller system according to claim 6, wherein the first base portion is rotatably mounted to the support member. 8. The propeller system according to claim 6, wherein the first base portion is drivingly connected to the first motor through the first ring gear. 9. The propeller system according to claim 8, further comprising: a first driving member operatively coupled between the first motor and the first base portion, the first ring gear being carried by the first driving member. 10. The propeller system according to claim 6, wherein the second balancing weight member includes a second base portion, a second arm portion extending from the second base portion, and a second balancing weight being coupled to the second arm portion. 11. The propeller system according to claim 10, wherein the second base portion is rotatably mounted to the first base portion. 12. The propeller system according to claim 10, wherein the second base portion is drivingly connected to the second motor through the second ring gear. 13. The propeller system according to claim 12, further comprising: a second driving member operatively coupled between the second motor and the second base portion, the second ring gear being carried by the second driving member. 14. The propeller system according to claim 1, wherein each of the first and second motors and first and second balancing weight members are arranged axially outboard of the at least one propeller. 15. The propeller system according to claim 1, wherein the motor support being mounted to the support member, and the second motor being coupled to the motor support. 16. The propeller system according to claim 1, wherein each of the first and second motors are arranged axially outwardly of the first and second balancing weight members. 17. A method of balancing a propeller system including at least one propeller, the method comprising: imparting a driving force to a shaft operatively coupled to the at least one propeller;rotating a first balancing weight member with a first motor mounted to a motor support, the first balancing weight member being operatively coupled to a support member arranged axially outboard of, and connected with, the at least one propeller, the first balancing weight member being arranged between the first motor and the at least one propeller;driving the first balancing weight member with a first ring gear extending through the motor support;rotating a second balancing weight member with a second motor mounted to the motor support, he second balancing weight member being operatively coupled to the support member independently of the first balancing weight member, the second balancing weight member being arranged between the second motor and the at least one propeller;driving the second balancing weight member with a second ring gear extending through the motor support; andcontrolling a position of the first balancing weight member relative to the second balancing weight member. 18. The method of claim 17, further comprising: sensing vibration in the shaft; andcontrolling the position of the first balancing weight member relative to the second balancing weight member to reduce the sensed vibration. 19. The method of claim 17, further comprising: rotating the first and second motors with the at least one propeller. 20. The method of claim 17, further comprising: rotating the first and second balancing weight members within a hub member that covers, at least in part, a portion of the at least one propeller. 21. The method of claim 17, wherein operating the first and second motors includes activating the first and second motors arranged axially outwardly of the first and second balancing weight members.
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이 특허에 인용된 특허 (15)
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