[특허]Passive dynamic inertial rotor balance system for turbomachinery

Passive dynamic inertial rotor balance system for turbomachinery 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G01M-001/16 F16F-015/36
출원번호	US-0438922 (2012-04-04)
등록번호	US-8984940 (2015-03-24)
발명자 / 주소	Josefczyk, Ronald John
출원인 / 주소	Elliot Company
대리인 / 주소	The Webb Law Firm
인용정보	피인용 횟수 : 0 인용 특허 : 46

초록 ▼

A passive dynamic inertial rotor balance system including a plurality of balancing members fitted onto a rotor shaft at locations of predicted maximum shaft modal deflection. Each of the balancing members has at least one chamber and located within the at least one chamber is a plurality of movable weights and a viscous fluid. As the shaft accelerates toward an unbalance point, the weights move within the at least one chamber to a location which is opposite from the unbalance point. The viscous fluid provides damping for the movable weights to prevent excess movement within the chamber and to provide lubrication thereof. A system for self-correcting an unbalance of a turbomachinery rotor during rotation of the rotor and a method for balancing a rotor in a turbomachinery is also provided.

대표청구항 ▼

1. A passive dynamic inertial rotor balance system comprising: at least three balancing members fitted onto a rotor shaft at locations of predicted maximum shaft modal deflection, each of said balancing members including at least one chamber, said at least one chamber of each of said balancing members including:a plurality of movable weights; anda viscous fluid located therein, wherein as the shaft accelerates toward an unbalance point, the weights move within the at least one chamber to a location which is opposite from the unbalance point,wherein at least one balancing member is located near a center portion for a first mode bending and at least two balancing members are located at approximately quarter spans for a second mode bending. 2. The system of claim 1, wherein the weights comprise ball bearings formed from a heavy metal material. 3. The system of claim 2, wherein the heavy metal material comprises a tungsten alloy. 4. The system of claim 1, wherein the viscous fluid comprises a non-corrosive fluid material. 5. The system of claim 4, wherein the viscous fluid comprises a petroleum or glycol based substance. 6. The system of claim 1, wherein the balancing member is a ring defining a central open portion configured for placement about the rotor shaft and the at least one chamber comprises an annular hollow portion extending about the central open portion and defined by walls of the ring. 7. The system of claim 6, wherein up to one half of a circumference of the hollow portion of the ring is covered by the ball bearings and the hollow portion is fully filled with the viscous fluid. 8. A system for self-correcting an unbalance of a turbomachinery rotor during rotation of said rotor, said system comprising: at least three rings mounted at predetermined locations along a shaft of the rotor, each of said rings including an enclosed chamber;a plurality of movable weights located within said chamber of each of said rings; anda fluid located within said chamber of each of said rings and surrounding said movable weights, wherein upon the presence of an unbalance during rotation, the weights located within the chambers move in a direction which is opposite from the location of the unbalance,wherein a first ring is located near a center portion for a first mode bending, a second ring is located to one side of said first ring, and a third ring is located to an opposite side of said first ring, said second and third rings being located at approximately quarter spans for a second mode bending. 9. The system of claim 8, wherein the movable weights comprise ball bearings and the fluid comprises a viscous material capable of providing damping for the movable weights to prevent excess movement and to provide lubrication. 10. The system of claim 8, wherein the rings are located along the shaft of the rotor at locations of predicted maximum shaft modal deflection. 11. A method for balancing a rotor in a turbomachinery, said method comprising: providing a plurality of rings, each of said rings including a hollow chamber, said hollow chamber containing movable weights and a viscous fluid material; andpositioning said rings along a shaft of said rotor, said rings being positioned at predetermined locations along a longitudinal length of said shaft at locations of predicted maximum shaft modal deflection such that as the shaft accelerates toward an unbalance point, the weights move within the hollow rings in a direction that is opposite to the unbalance point,wherein at least one ring is positioned near the longitudinal center of the shaft for first mode bending and wherein additional rings are located at locations for second mode bending. 12. The method of claim 11, wherein the weights comprise ball bearings and the fluid material comprises a material capable of providing damping for the bearings to prevent excess movement thereof and to provide lubrication for the ball bearings. 13. The method of claim 12, wherein the ball bearings are formed from a heavy metal material and the fluid material comprises a non-corrosive viscous material. 14. The method of claim 11, wherein the movable weights move to a location which is approximately 180° away from the unbalance point.

이 특허에 인용된 특허 (46)

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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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연합인증

Passive dynamic inertial rotor balance system for turbomachinery 원문보기

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Passive dynamic inertial rotor balance system for turbomachinery 원문보기

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