Patent US3410505A successfully refreshed from Google Patents.
US3410505A
Expired / Lapsed
US
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Control systems for aerial missiles and like vehicles
Assignee: WALTER JAMES GILDON
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Filing: 1959-10-16
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Granted: 1968-11-12
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Expires: 1979-10-16
Abstract
No abstract record available.
Inventors
- 👤 Gildon Walter James
- 👤 Ferguson Thomas George
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 21:36
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/60; F42B10/66; F42B10/663; B; B64; B64C; B64C9/00; B64C9/38; F02; F02K; F02K9/00; F02K9/80; F02K9/84; F41; F41G; F41G7/00; F41G7/20; F41G7/30; F41G7/301
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
160 words
A CONTROL SYSTEM FOR AERIAL MISSILES AND LIKE VEHICLES HAVING TWO CONTROL VENTURI SYMMETRICALLY SITUATED ONE ON EITHER SIDE OF AND PARALLEL TO THE MISSILE AXIS; TWO PAIRS OF MOUNTIING BRACKETS FIXED TO THE MISISLE, ONE BRACKET ON EITHER SIDE OF EACH VENTURI; A RECTANGULAR FRAME SURROUNDING EACH VENTURI AND ROTATABLY MOUNTED IN THE ASSOCIATED PAIR OF BRACKETS, THE AXIS OF ROTATION BEING PERPENDICULAR TO THE AXIAL PLANE OF THE MISSILE THROUGH THE VENTURI; A TUBULAR DEFLECTOR SURROUNDING AND EXTENDING REARWARDLY OF EACH VENTURI EXIT AND ROTATABLY MOUNTED IN THE ASSOCIATED RECTANGULAR FRAME, ITS AXIS OF ROTATION BEING PERPENDICULAR TO THAT OF THE FRAME; A PRESSURE FLUID TO OPERATED, ROTARY VANE ACTUATOR MOUNTED ON EACH RECTANGULAR FRAME IN ALIGNMENT WITH THE AXIS OF ROTATION OF THE FRAME AND OPERATIVELY CONNECTED TO THE FRAME AND ONE MOUNTING BRACKET, FOR DEFLECTING THE FRAME; A SECOND SIMILAR ACTUATOR ATTACHED TO AN ADJACENT ARM OF EACH FRAME AND OPERATIVELY CONNECTED TO THE FRAME AND
Claim 2
Dependent Claim
160 words
A CONTROL SYSTEM FOR AERIAL MISSILES AND LIKE VEHICLES HAVING TWO CONTROL VENTURI SYMMETRICALLY SITUATED ONE ON EITHER SIDE OF AND PARALLEL TO THE MISSILE AXIS; TWO PAIRS OF MOUNTIING BRACKETS FIXED TO THE MISISLE, ONE BRACKET ON EITHER SIDE OF EACH VENTURI; A RECTANGULAR FRAME SURROUNDING EACH VENTURI AND ROTATABLY MOUNTED IN THE ASSOCIATED PAIR OF BRACKETS, THE AXIS OF ROTATION BEING PERPENDICULAR TO THE AXIAL PLANE OF THE MISSILE THROUGH THE VENTURI; A TUBULAR DEFLECTOR SURROUNDING AND EXTENDING REARWARDLY OF EACH VENTURI EXIT AND ROTATABLY MOUNTED IN THE ASSOCIATED RECTANGULAR FRAME, ITS AXIS OF ROTATION BEING PERPENDICULAR TO THAT OF THE FRAME; A PRESSURE FLUID TO OPERATED, ROTARY VANE ACTUATOR MOUNTED ON EACH RECTANGULAR FRAME IN ALIGNMENT WITH THE AXIS OF ROTATION OF THE FRAME AND OPERATIVELY CONNECTED TO THE FRAME AND ONE MOUNTING BRACKET, FOR DEFLECTING THE FRAME; A SECOND SIMILAR ACTUATOR ATTACHED TO AN ADJACENT ARM OF EACH FRAME AND OPERATIVELY CONNECTED TO THE FRAME AND
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) | 1971-11-12 | 1972-05-13 | 1972-11-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1975-11-12 | 1976-05-13 | 1976-11-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1979-11-12 | 1980-05-13 | 1980-11-12 | $7700.00 | Window Closed / Lapsed |