US3357656A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbine propulsion and drive for aircraft rotor means
Assignee: Individual
•
Filing: 1965-07-06
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Granted: 1967-12-12
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Expires: 1985-07-06
Abstract
No abstract record available.
Inventors
- 👤 Adolphe C Peterson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 16:37
CPC Classifications
B; B64; B64C; B64C29/00; B64C29/0008; B64C29/0016; B64C29/0025; B64C27/00; B64C27/04; B64C27/12
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
155 words
IN A ROTOR MEANS FOR AIRCRAFT: A PYLON STRUCTURE MOUNTED ON AN AIRCRAFT FUSELAGE AND FORMED TO HAVE A ROTOR BEARING AND TO HAVE ADJACENT A SIDE THEREOF A TURBINE MOUNTING AND A TURBINE CASING AFFIXED INTEGRALLY THEREWITH; AN AIRFOIL ROTOR ROTATABLY MOUNTED BY SAID ROTOR BEARING ON SAID PYLON STRUCTURE; A TURBINE ROTOR MEANS ROTATABLY MOUNTED IN THE TURBINE CASING AND HAVING TURBINE BLADE MEANS ROTATING IN THE TURBINE CASING AND HAVING TRANSMISSION SPEED REDUCTION MEANS TRANSMITTING TO THE AIRFOIL ROTOR; A PRIMARY COMBUSTION TURBINE MOUNTED ON THE AIRCRAFT FUSELAGE AND HAVING A DISCHARGE FOR GASEOUS FLUID THROUGH CONDUIT MEANS IN SAID PYLON STRUCTURE AND TO SAID FIRST NAMED TURBINE CASING TO DRIVE THE TURBINE ROTOR MEANS; THE MOUNTING OF SAID PYLON STRUCTURE ON SAID AIRCRAFT FUSELAGE INCLUDING A BEARING MEANS BETWEEN SAID PYLON STRUCTURE AND SAID AIRCRAFT FUSELAGE WHEREBY SAID PYLON STRUCTURE IS ROTATABLE ON ITS AXIS IN SAID LAST NAMED BEARING MEANS.
Claim 2
Dependent Claim
155 words
IN A ROTOR MEANS FOR AIRCRAFT: A PYLON STRUCTURE MOUNTED ON AN AIRCRAFT FUSELAGE AND FORMED TO HAVE A ROTOR BEARING AND TO HAVE ADJACENT A SIDE THEREOF A TURBINE MOUNTING AND A TURBINE CASING AFFIXED INTEGRALLY THEREWITH; AN AIRFOIL ROTOR ROTATABLY MOUNTED BY SAID ROTOR BEARING ON SAID PYLON STRUCTURE; A TURBINE ROTOR MEANS ROTATABLY MOUNTED IN THE TURBINE CASING AND HAVING TURBINE BLADE MEANS ROTATING IN THE TURBINE CASING AND HAVING TRANSMISSION SPEED REDUCTION MEANS TRANSMITTING TO THE AIRFOIL ROTOR; A PRIMARY COMBUSTION TURBINE MOUNTED ON THE AIRCRAFT FUSELAGE AND HAVING A DISCHARGE FOR GASEOUS FLUID THROUGH CONDUIT MEANS IN SAID PYLON STRUCTURE AND TO SAID FIRST NAMED TURBINE CASING TO DRIVE THE TURBINE ROTOR MEANS; THE MOUNTING OF SAID PYLON STRUCTURE ON SAID AIRCRAFT FUSELAGE INCLUDING A BEARING MEANS BETWEEN SAID PYLON STRUCTURE AND SAID AIRCRAFT FUSELAGE WHEREBY SAID PYLON STRUCTURE IS ROTATABLE ON ITS AXIS IN SAID LAST NAMED BEARING MEANS.
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) | 1970-12-11 | 1971-06-12 | 1971-12-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1974-12-11 | 1975-06-12 | 1975-12-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1978-12-11 | 1979-06-12 | 1979-12-12 | $7700.00 | Window Closed / Lapsed |