US4350236A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Electromagnetic clutch assembly
Assignee: Lockheed Martin Corp
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Filing: 1980-12-08
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Granted: 1982-09-21
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Expires: 2000-12-08
Abstract
Abstract A clutch assembly for use in a high speed starter motor/turbine assembly wherein the elements thereof must be extremely well balanced. Opposing clutch elements are unitary rigid structures without moving parts. The starter motor rotor and one of the clutch elements are assembled as a unitary balanced structure for high speed rotation and axial movement to engage or disengage the other clutch element and its associated balanced turbine load.
Inventors
- 👤 Paul H. Stahlhuth
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 17:03
CPC Classifications
F; F02; F02N; F02N15/00; F02N15/02; F16; F16D; F16D27/00; F16D27/10; F16D27/108; F16D27/112; Y; Y10; Y10T; Y10T74/00; Y10T74/13; Y10T74/131; Y10T74/134
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
138 words
An electromagnetic clutch assembly for controlling the engagement and disengagement of a rotatable prime mover with a rotatable load wherein said assembly includes: a clutch rotor having a frictional engagement surface attached to said load and mounted for axial rotation about a first axis; a clutch armature having a frictional engagement surface opposed to said clutch rotor engagement surface rigidly attached to said prime mover and mounted for axial rotation about said first axis; electromagnetic means mounted adjacent said clutch rotor and clutch armature to cause engagement of said clutch rotor and clutch armature engagement surfaces and thereby communicate rotational driving forces from said prime mover to said load through said frictional engagement surfaces when energized by an external electrical source; and means for mounting said clutch armature and prime mover to move axially as a single unit.
Claim 2
Dependent Claim
138 words
An electromagnetic clutch assembly for controlling the engagement and disengagement of a rotatable prime mover with a rotatable load wherein said assembly includes: a clutch rotor having a frictional engagement surface attached to said load and mounted for axial rotation about a first axis; a clutch armature having a frictional engagement surface opposed to said clutch rotor engagement surface rigidly attached to said prime mover and mounted for axial rotation about said first axis; electromagnetic means mounted adjacent said clutch rotor and clutch armature to cause engagement of said clutch rotor and clutch armature engagement surfaces and thereby communicate rotational driving forces from said prime mover to said load through said frictional engagement surfaces when energized by an external electrical source; and means for mounting said clutch armature and prime mover to move axially as a single unit.
Claim 3
Dependent Claim
52 words
A clutch assembly as in claim 1, wherein said mounting means provides that said clutch armature and prime mover are spring biased into an axial position in which said engagement surface of said clutch armature is not engaged with said engagement surface of said clutch rotor when said electromagnetic means is de-energized.
Claim 4
Dependent Claim
57 words
A clutch assembly as in claim 2, wherein said prime mover is defined as a rotor element, of a motor having a motor housing, wherein said rotor element has a rotor shaft extending axially therefrom and said clutch armature is formed as a unitary structure of ferrous material rigidly attached to said shaft of said motor rotor.
Claim 5
Dependent Claim
43 words
A clutch assembly as in claim 3, wherein said mounting means includes rotational bearings connected to support said rotor shaft, said bearings are slidably mounted in said motor housing and said biasing springs are mounted in said housing to axially bias said bearings.
Claim 6
Dependent Claim
40 words
A clutch assembly as in claim 4, wherein said load is a balanced turbine rotor assembly with a turbine housing containing a coaxial turbine shaft and said clutch rotor is a unitary structure rigidly attached to said coaxial turbine shaft.
Claim 7
Dependent Claim
49 words
A clutch assembly as in claim 5, wherein said rotor element is utilized to engage said turbine rotor through said clutch assembly and drive it to a rotational speed of approximately 80,000 rpm while said electromagnetic means is energized and subsequently disengaged therefrom when said electromagnetic means is de-energized.
References Cited (Backward Citations)
US1246691A
Cited
US2046910A
Cited
US2666509A
Cited
US2946418A
Cited
US3458022A
Cited
US3451516A
Cited
US3674122A
Cited
US3912060A
Cited
US3863743A
Cited
US3978953A
Cited
US4194610A
Cited
US4187939A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-09-20 | 1986-03-22 | 1986-09-21 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-09-20 | 1990-03-22 | 1990-09-21 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-09-20 | 1994-03-22 | 1994-09-21 | $7700.00 | Window Closed / Lapsed |