Patent US3936230A successfully refreshed from Google Patents.
US3936230A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Self-supported, self-locating seal for turbine engines
Assignee: United States Department of the Air Force
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Filing: 1974-05-09
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Granted: 1976-02-03
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Expires: 1994-05-09
Abstract
Abstract A self-supporting, self-locating seal having a central portion and a pair of end segments so designed as to fit within the mid span joint formed between adjacent turbine engine blades. Because of the design of the seal, the seal is held securely in position simply by its geometry and the centrifugal forces applied thereto during turbine engine operation.
Inventors
- 👤 Augustus M. Helmintoller, Jr.
- 👤 Gary B. Manharth
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 17:56
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/005
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
302 words
A self-locating, self-supporting seal adapted to fit within the cavity formed between the midspan joints of adjacent blades of a turbine engine comprising an elongated body formed of a synthetic plastic material having an elongated central portion and a pair of end segments, said central portion lying in a preselected plane and having a longitudinal axis, one of said end segments being of a length substantially half the length of said central portion and being positioned at substantially 45° with respect to said longitudinal axis of said central portion, said one segment having an end portion, said end portion of said one end segment lying in a plane extending substantially 90° from said plane of said central portion in order to provide a rigid support for said seal within said turbine blade cavity, said other end segment being formed of three protrusions, the first of said protrusions being of a substantially rectangular configuration and an extension of said central portion, located along said longitudinal axis of said central portion and lying completely in the same plane as said central portion, the second of said protrusions being positioned at an angle of substantially 90° with respect to said longitudinal axis of said central portion and having an end lying in a plane extending substantially 90° from the plane of said central portion, and the third of said protrusions being located substantially opposite said second protrusion and having an end having a pair of extensions thereon, said pair of extensions extending substantially 90 ° from the plane of said central portion, whereby upon positioning of said seal within the cavity formed between the midspan joints of adjacent blades of a turbine engine said end segments of said seal by their geometry, utilize the centrifugal forces acting theron to fixedly secure said seal in position.
Claim 2
Dependent Claim
302 words
A self-locating, self-supporting seal adapted to fit within the cavity formed between the midspan joints of adjacent blades of a turbine engine comprising an elongated body formed of a synthetic plastic material having an elongated central portion and a pair of end segments, said central portion lying in a preselected plane and having a longitudinal axis, one of said end segments being of a length substantially half the length of said central portion and being positioned at substantially 45° with respect to said longitudinal axis of said central portion, said one segment having an end portion, said end portion of said one end segment lying in a plane extending substantially 90° from said plane of said central portion in order to provide a rigid support for said seal within said turbine blade cavity, said other end segment being formed of three protrusions, the first of said protrusions being of a substantially rectangular configuration and an extension of said central portion, located along said longitudinal axis of said central portion and lying completely in the same plane as said central portion, the second of said protrusions being positioned at an angle of substantially 90° with respect to said longitudinal axis of said central portion and having an end lying in a plane extending substantially 90° from the plane of said central portion, and the third of said protrusions being located substantially opposite said second protrusion and having an end having a pair of extensions thereon, said pair of extensions extending substantially 90 ° from the plane of said central portion, whereby upon positioning of said seal within the cavity formed between the midspan joints of adjacent blades of a turbine engine said end segments of said seal by their geometry, utilize the centrifugal forces acting theron to fixedly secure said seal in position.
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) | 1979-02-02 | 1979-08-04 | 1980-02-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-02-02 | 1983-08-04 | 1984-02-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-02-02 | 1987-08-04 | 1988-02-03 | $7700.00 | Window Closed / Lapsed |