US4540337A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Ram air turbines
Assignee: Kongsberg Gruppen ASA
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Filing: 1983-05-09
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Granted: 1985-09-10
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Expires: 2003-05-09
Abstract
Abstract A cup shaped disc (13) consisting of a central portion (20) having radially extending blades (18) is attached with its central portion to the protruding hub portion (12) of a radial flow turbine wheel (2) consisting of a backing plate (10) extending transversely to its rotational axis (7) and having axially protruding turbine blades (11) in addition to the protruding hub. At high rotational speeds this disc (13) will tend to straighten out, whereby the effective portion of the turbine blades will be reduced and the increase in the rotational speed restricted. This is of importance in ram air turbines for missiles.
Inventors
- 👤 Sten O. Olsen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 22:44
CPC Classifications
F; F42; F42C; F42C15/00; F42C15/28; F42C15/295; F05; F05B; F05B2220/00; F05B2220/30; F05B2220/31
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
231 words
A ram air turbine for driving an electric generator in a missile, the turbine comprising a turbine housing having a flow passage for ducting the incoming ram air, a turbine wheel having blades to which the ram air is supplied from said flow passage, wherein the turbine wheel includes means actuated by centrifugal force upon an increase in the rotational speed of the turbine sheel for uniformly restricting the cross section of the flow passage to all of said turbine blades and thus the amount of ram air acting on the blades of the turbine wheel to an extent depending upon the rotational speed of the turbine wheel, wherein the turbine wheel is a radial turbine wheel having a protruding central hub portion and the incoming ram air is incident upon the turbine wheel along the axial direction and thereafter flows past the blades in a radial direction, and wherein the centrifugal force actuated means comprises a disc of cup shape and inverted relative to the axial direction of the incoming ram air, the central portion of said disc being attached to said protruding hub of said radial turbine wheel, said disc being manufactured from a resilient material which upon rotation of the turbine wheel allows straightening-out deflection of the cup-shaped disc due to centrifugal forces, the outer edges of the disc lifting from an undeflected position against the turbine wheel.
Claim 2
Dependent Claim
231 words
A ram air turbine for driving an electric generator in a missile, the turbine comprising a turbine housing having a flow passage for ducting the incoming ram air, a turbine wheel having blades to which the ram air is supplied from said flow passage, wherein the turbine wheel includes means actuated by centrifugal force upon an increase in the rotational speed of the turbine sheel for uniformly restricting the cross section of the flow passage to all of said turbine blades and thus the amount of ram air acting on the blades of the turbine wheel to an extent depending upon the rotational speed of the turbine wheel, wherein the turbine wheel is a radial turbine wheel having a protruding central hub portion and the incoming ram air is incident upon the turbine wheel along the axial direction and thereafter flows past the blades in a radial direction, and wherein the centrifugal force actuated means comprises a disc of cup shape and inverted relative to the axial direction of the incoming ram air, the central portion of said disc being attached to said protruding hub of said radial turbine wheel, said disc being manufactured from a resilient material which upon rotation of the turbine wheel allows straightening-out deflection of the cup-shaped disc due to centrifugal forces, the outer edges of the disc lifting from an undeflected position against the turbine wheel.
Claim 3
Dependent Claim
55 words
A ram air turbine according to claim 1, wherein the radially outer portion of said disc is divided by radial slots into separate blades, -sections the turbine further comprising interengaging means for providing conforming movement of said separate blade-sections, whereby each blade-section is deflected to essentially the same degree at a given turbine wheel speed.
Claim 4
Dependent Claim
29 words
A ram air turbine according to claim 2, wherein said interengaging means includes said blade-sections being sized to overlap adjacent blade sections for the entire range of straightening-out deflection.
Claim 5
Dependent Claim
55 words
A ram air turbine according to claim 3, wherein the disc has outwardly bent outer edges and thus a cup shape similar to a lily flower, and in which the lateral edges of each blade-section lie above one adjacent blade-section and below the other, respectively, in a repeating pattern about the periphery of said disc.
Claim 6
Dependent Claim
22 words
A ram air turbine according to any one of the claims 2 to 4, wherein said disc is made from spring steel.
Claim 7
Dependent Claim
26 words
A ram air turbine according to any of the claims 1 to 5, further including stops for restricting the extent of straightening-out deflection of the disc.
Claim 8
Dependent Claim
58 words
A ram air turbine according to claim 6, wherein the turbine blades have inwardly directed radial protrusions, and wherein the outer edge of the disc extends below said inwardly directed protrusions of the turbine blades, so that the lower side of the protrusions form said stops for limiting the straightening-out deflection of the disc at high rotational speeds.
Claim 9
Dependent Claim
52 words
A ram air turbine according to claim 7, wherein a running clearance is provided between the turbine blades and said housing, said housing including said turbine housing including an annular skirt surrounding said flow passage and extending radially inside the protrusions to block the flow of ram air into the running clearance.
References Cited (Backward Citations)
DE280189C
Cited
US147282A
Cited
US3128989A
Cited
US1186289A
Cited
GB126707A
Cited
US2459815A
Cited
US4161371A
Cited
US3352536A
Cited
US2766964A
Cited
US3069137A
Cited
US3733143A
Cited
US3856432A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-09-09 | 1989-03-11 | 1989-09-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-09-09 | 1993-03-11 | 1993-09-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-09-09 | 1997-03-11 | 1997-09-10 | $7700.00 | Window Closed / Lapsed |