Patent US4201513A successfully refreshed from Google Patents.
US4201513A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gas turbine engines
Assignee: Rolls Royce PLC
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Filing: 1978-09-20
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Granted: 1980-05-06
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Expires: 1998-09-20
Abstract
Abstract A mounting arrangement for the fan rotor of a ducted fan engine includes a first drive which supports and rotates the fan under normal operating conditions but which includes a frangible connection which breaks when an excessive out-of-balance force is applied to the fan rotor for example after loss of one or more blades. A second supporting and driving structure is provided which has built-in transverse flexibility but which can transmit torque. This structure is redundant during normal operation of the engine but comes into use when the frangible connection is broken and allows the fan rotor to rotate eccentrically around a new axis in an inverted condition.
Inventors
- 👤 Stephen Sales
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 09:03
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/04; F01D21/045; F01D25/00; F01D25/16; F05; F05B; F05B2260/00; F05B2260/30; F05B2260/301; F05B2260/3011; F05D; F05D2220/00; F05D2220/30; F05D2220/32; F05D2220/327
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
142 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main shaft, a mounting structure for supporting the rotor on the shaft and including a driving connection for transmitting drive between the rotor and the main shaft and which includes a portion dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the rotor and the shaft to support the rotor and to maintain a driving connection between the rotor and shaft when the driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft about an altered axis.
Claim 2
Dependent Claim
142 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main shaft, a mounting structure for supporting the rotor on the shaft and including a driving connection for transmitting drive between the rotor and the main shaft and which includes a portion dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the rotor and the shaft to support the rotor and to maintain a driving connection between the rotor and shaft when the driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft about an altered axis.
Claim 3
Dependent Claim
138 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main shaft, a mounting structure for supporting the rotor on the shaft and including a driving connection for transmitting drive between the rotor and the main shaft and which includes a portion dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the rotor and the shaft to support the rotor and to maintain a driving connection between the rotor and shaft when the driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said driving connection and sufficiently transversely flexible to support rotation of the rotor in an inverted condition.
Claim 4
Dependent Claim
138 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main shaft, a mounting structure for supporting the rotor on the shaft and including a driving connection for transmitting drive between the rotor and the main shaft and which includes a portion dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the rotor and the shaft to support the rotor and to maintain a driving connection between the rotor and shaft when the driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said driving connection and sufficiently transversely flexible to support rotation of the rotor in an inverted condition.
Claim 5
Dependent Claim
147 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main drive shaft, a mounting structure for supporting the rotor on the shaft and including a first frangible driving connection for transmitting drive from the main shaft to the rotor and which is dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the shaft to the rotor to support the rotor and to maintain a second driving connection from the shaft to the rotor when the first driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said first driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft about an altered axis.
Claim 6
Dependent Claim
147 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a main drive shaft, a mounting structure for supporting the rotor on the shaft and including a first frangible driving connection for transmitting drive from the main shaft to the rotor and which is dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the shaft to the rotor to support the rotor and to maintain a second driving connection from the shaft to the rotor when the first driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said first driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft about an altered axis.
Claim 7
Dependent Claim
147 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a man drive shaft, a mounting strucutre for supporting the rotor on the shaft and including a first frangible driving connection for transmitting drive from the main shaft to the rotor and which is dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the shaft to the rotor to support the rotor and to maintain a second driving connection from the shaft to the rotor when the first driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said first driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft in an inverted condition.
Claim 8
Dependent Claim
147 words
A gas turbine engine comprising a rotor, a plurality of blades carried by the rotor, a man drive shaft, a mounting strucutre for supporting the rotor on the shaft and including a first frangible driving connection for transmitting drive from the main shaft to the rotor and which is dimensioned to fracture when out-of-balance loads on the rotor caused by loss of at least part of a blade from the rotor exceed a predetermined magnitude, and a separate torsionally stiff, drive means interconnecting the shaft to the rotor to support the rotor and to maintain a second driving connection from the shaft to the rotor when the first driving connection of the mounting structure has broken, said separate drive means being transversely more flexible than said first driving connection and sufficiently transversely flexible to support rotation of the rotor on the main shaft in an inverted condition.
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) | 1983-05-06 | 1983-11-05 | 1984-05-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-05-06 | 1987-11-05 | 1988-05-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-05-06 | 1991-11-05 | 1992-05-06 | $7700.00 | Window Closed / Lapsed |