US4281942A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Lubrication system for high speed spline connection and bearing
Assignee: General Electric Co
•
Filing: 1978-11-13
•
Granted: 1981-08-04
•
Expires: 1998-11-13
Abstract
Abstract A lubrication system for the spline connection and generator bearing of a high speed aircraft generator which utilizes a split ring seal and quad o-ring is disclosed. The split ring seal retards lubricant flow so that there is an accumulation in the area of the splined connection which prevents wear of the splines. The retardation also forces oil to a bearing lubrication hole.
Inventors
- 👤 Fred J. Gaeckle
- 👤 John L. Butterfield
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 23:30
CPC Classifications
F; F16; F16N; F16N7/00; F16N7/36; F16B; F16B2200/00; F16B2200/60; F16N2210/00; F16N2210/12; F16N2210/14; Y; Y10; Y10S; Y10S277/00; Y10S277/911; Y10T; Y10T403/00; Y10T403/70; Y10T403/7026; Y10T403/7028
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
171 words
A spline and bearing lubrication system for use in high speed aircraft generator drive systems having: a stub shaft having external splines for transmitting power, a power receiving internally splined tube having a splined portion and a smooth portion, a bearing located around said power receiving internally splined tube, a splined connection formed by the stub shaft external spline and the power receiving internally splined tube, said connection having first and second ends, a source of high pressure engine lubricating oil which is supplied to said first end of said splined connection, the improvement comprising: a lubrication hole connecting said first side of said splined connection to said generator bearing for supplying said engine lubricating oil to said generator bearing and means located at said second end of said splined connection and secured to said power receiving splined tube for retarding the flow of said oil across said splined connection, for forcing a portion of said oil into said lubrication hole and for preventing fretting or corrosion of said splined connection.
Claim 2
Dependent Claim
171 words
A spline and bearing lubrication system for use in high speed aircraft generator drive systems having: a stub shaft having external splines for transmitting power, a power receiving internally splined tube having a splined portion and a smooth portion, a bearing located around said power receiving internally splined tube, a splined connection formed by the stub shaft external spline and the power receiving internally splined tube, said connection having first and second ends, a source of high pressure engine lubricating oil which is supplied to said first end of said splined connection, the improvement comprising: a lubrication hole connecting said first side of said splined connection to said generator bearing for supplying said engine lubricating oil to said generator bearing and means located at said second end of said splined connection and secured to said power receiving splined tube for retarding the flow of said oil across said splined connection, for forcing a portion of said oil into said lubrication hole and for preventing fretting or corrosion of said splined connection.
Claim 3
Dependent Claim
49 words
The apparatus of claim 1 wherein said means for retarding the flow of oil across said splined connection, comprises a split ring seal means mounted within said smooth portion of said power receiving internally splined tube, and having a radially inwardly extending annular groove around the outer circumferential surface.
Claim 4
Dependent Claim
17 words
The apparatus of claim 2 wherein a quad o-ring is mounted within said internally extending annular groove.
Claim 5
Dependent Claim
60 words
The apparatus of claim 1 or 2 wherein said split ring has a first semicircular seal member, and a second semicircular seal member, and wherein said first and second semicircular members have ends which are spaced apart by a predetermined distance when said rings are in contact with said smooth portion of said power receiving tube during high speed rotation.
Claim 6
Dependent Claim
31 words
The apparatus of claim 4 wherein said predetermined distance between the ends of said split rings is determined in accordance with the desired rate of lubricant flow across the splined connection.
Claim 7
Dependent Claim
32 words
The apparatus of claim 2 further including means mounted on said smooth portion of said power receiving internally splined tube for retaining said split ring seal means in place against axial movement.
References Cited (Backward Citations)
US2888281A
Cited
US3017230A
Cited
US3038556A
Cited
US3720418A
Cited
US4144950A
Cited
US4086759A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-08-03 | 1985-02-02 | 1985-08-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-08-03 | 1989-02-02 | 1989-08-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-08-03 | 1993-02-02 | 1993-08-04 | $7700.00 | Window Closed / Lapsed |