Patent US4669959A successfully refreshed from Google Patents.
US4669959A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Breach lock anti-rotation key
Assignee: RTX Corp
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Filing: 1984-07-23
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Granted: 1987-06-02
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Expires: 2004-07-23
Abstract
Abstract The anti-rotational breach lock comprises a full ring of equally spaced dogs slideably engaging complementary lugs extending from the disk restrain the blades axially. A key fits any space between lugs and has an in situ bent tab nested between the key and ring that engages the back and front end of the ring to lock the key into place. Because the key can fit anywhere around the circumference of the disk and as many keys as spaces can be deployed, the key may serve to balance the rotor.
Inventors
- 👤 Robert R. Kalogeros
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 12:44
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/027; F01D5/30; F01D5/3007; F01D5/3015
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
167 words
For a gas turbine engine having a rotor comprising a disk and a plurality of turbine blades circumferentially spaced in recesses formed on the outer circumference of said disk, a breach-lock formed from an annularly shaped member having a plurality of dogs extending from an edge of said member, uniformly spaced complementary lugs extending from said disk for engagement with said dogs for axially restraining said turbine blades in said disk and defining uniform spaces between adjacent lugs, at least one removable key having a generally rectangular shaped body dimensioned to fit into any one of said uniform spaces and circumferentially restraining said annularly shaped member to lock it into place, and a tab formed from sheet metal members sandwiched between said body and said annular shaped member having one portion extending behind said annular shaped member and another portion extending in front of said annular shaped member and bent in situ to engage the front of said annular shaped member to secure said key in place.
Claim 2
Dependent Claim
167 words
For a gas turbine engine having a rotor comprising a disk and a plurality of turbine blades circumferentially spaced in recesses formed on the outer circumference of said disk, a breach-lock formed from an annularly shaped member having a plurality of dogs extending from an edge of said member, uniformly spaced complementary lugs extending from said disk for engagement with said dogs for axially restraining said turbine blades in said disk and defining uniform spaces between adjacent lugs, at least one removable key having a generally rectangular shaped body dimensioned to fit into any one of said uniform spaces and circumferentially restraining said annularly shaped member to lock it into place, and a tab formed from sheet metal members sandwiched between said body and said annular shaped member having one portion extending behind said annular shaped member and another portion extending in front of said annular shaped member and bent in situ to engage the front of said annular shaped member to secure said key in place.
Claim 3
Dependent Claim
28 words
For a gas turbine engine as in claim 1, wherein said rectangularly shaped body has a continuous slot formed on at least 3 sides for receiving said tab.
Claim 4
Dependent Claim
27 words
For a gas turbine engine as in claim 2 wherein the number of said tabs fitted into said uniform spaces are selected to dynamically balance said rotor.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-06-01 | 1990-12-01 | 1991-06-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-06-01 | 1994-12-01 | 1995-06-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-06-01 | 1998-12-01 | 1999-06-02 | $7700.00 | Window Closed / Lapsed |