Patent US4177692A successfully refreshed from Google Patents.
US4177692A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Shaft balancing
Assignee: Rolls Royce Corp
•
Filing: 1977-11-25
•
Granted: 1979-12-11
•
Expires: 1997-11-25
Abstract
Abstract A gas turbine engine has an internal drive shaft including one end connected to a driven load and an opposite end connected to a turbine wheel and wherein the shaft has an in situ adjustable balance system near the critical center of a bearing span for the shaft including two 360° rings piloted on the outer diameter of the shaft at a point accessible through an internal engine panel; each of the rings has a small amount of material removed from its periphery whereby both of the rings are precisely unbalanced an equivalent amount; the rings are locked circumferentially together by radial serrations thereon; numbered tangs on the outside diameter of each ring identify the circumferential location of unbalance once the rings are locked together; an aft ring of the pair of rings has a spline on its inside diameter that mates with a like spline on the shaft to lock the entire assembly together.
Inventors
- 👤 John A. Irwin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 23:11
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/027; F16; F16F; F16F15/00; F16F15/22; F16F15/32; F16F15/322
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
388 words
A gas turbine engine rotor shaft balancing assembly comprising: a shaft having first and second segments each having an outer peripheral surface thereon spaced from one another, a coupling joining said shaft segments, one of said shaft segments including a plurality of external splines at one end thereof, a first balance ring having a first precise unbalance located thereon, said first balance ring having a first smooth inner bore at one end thereof supportably received on the peripheral surface of the other of said shaft segments and internal splines at the opposite end thereof and for axial adjustment into and out of interlocked engagement with said external splines, a second balance ring having a second smooth inner bore throughout its axial length slidably supported on the peripheral surface of the other of said shaft segments and having a second precise unbalance thereon, coacting serration means on said first and second balance rings for axially joining and separating said first and second balance rings for rotatable adjustment relative to one another to circumferentially locate said first and second unbalances at a relatively fixed rotatable joined position therebetween, said first and second balance rings when in their joined position having their smooth inner bores rotatable on said other of said shaft segments when said first balance ring is out of interlocked engagement with said external splines thereby to circumferentially position said relatively fixed joined first and second balance rings with respect to said shaft for correcting shaft unbalance, means for shifting said first and second balance rings axially on said shaft when said relatively fixed first and second precise unbalances are rotatably adjusted with respect to the shaft to balance said shaft, a housing surrounding said shaft and said first and second balance rings thereon accessible from exteriorly of said engine and including an access port therein overlying said shaft and said first and second balance rings thereon, a removable panel on said housing covering said access port to prevent the entrance of foreign matter interiorly of said housing, said panel being removable whereby said first and second balance rings can be adjusted both axially and rotatably both with respect to one another and with respect to said shaft to produce in situ balancing of the shaft without disassembly from an axially fixed running location within a gas turbine engine.
Claim 2
Dependent Claim
388 words
A gas turbine engine rotor shaft balancing assembly comprising: a shaft having first and second segments each having an outer peripheral surface thereon spaced from one another, a coupling joining said shaft segments, one of said shaft segments including a plurality of external splines at one end thereof, a first balance ring having a first precise unbalance located thereon, said first balance ring having a first smooth inner bore at one end thereof supportably received on the peripheral surface of the other of said shaft segments and internal splines at the opposite end thereof and for axial adjustment into and out of interlocked engagement with said external splines, a second balance ring having a second smooth inner bore throughout its axial length slidably supported on the peripheral surface of the other of said shaft segments and having a second precise unbalance thereon, coacting serration means on said first and second balance rings for axially joining and separating said first and second balance rings for rotatable adjustment relative to one another to circumferentially locate said first and second unbalances at a relatively fixed rotatable joined position therebetween, said first and second balance rings when in their joined position having their smooth inner bores rotatable on said other of said shaft segments when said first balance ring is out of interlocked engagement with said external splines thereby to circumferentially position said relatively fixed joined first and second balance rings with respect to said shaft for correcting shaft unbalance, means for shifting said first and second balance rings axially on said shaft when said relatively fixed first and second precise unbalances are rotatably adjusted with respect to the shaft to balance said shaft, a housing surrounding said shaft and said first and second balance rings thereon accessible from exteriorly of said engine and including an access port therein overlying said shaft and said first and second balance rings thereon, a removable panel on said housing covering said access port to prevent the entrance of foreign matter interiorly of said housing, said panel being removable whereby said first and second balance rings can be adjusted both axially and rotatably both with respect to one another and with respect to said shaft to produce in situ balancing of the shaft without disassembly from an axially fixed running location within a gas turbine engine.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-12-10 | 1983-06-11 | 1983-12-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-12-10 | 1987-06-11 | 1987-12-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-12-10 | 1991-06-11 | 1991-12-11 | $7700.00 | Window Closed / Lapsed |