US3077075A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Rotary radial flow jet engine
Assignee: Individual
•
Filing: 1957-03-15
•
Granted: 1963-02-12
•
Expires: 1977-03-15
Abstract
No abstract record available.
Inventors
- 👤 Turanciol Fuad
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 11:56
CPC Classifications
F; F02; F02K; F02K7/00; F02K7/005
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
162 words
A ROTARY RADIAL FLOW JET ENGINE COMPRISING A ROTOR INCLUDING TWO DISKS ROTATABLE ABOUT A COMMON AXIS AND SPACED AXIALLY THEREOF FOR DEFINING A COMBUSTION CHAMBER THEREBETWEEN, SAID ROTOR HAVING A FIRST AIR INLET TO THE COMBUSTION CHAMBER BETWEEN SAID DISKS, MEANS SUPPLYING FUEL TO THE COMBUSTION CHAMBER BETWEEN SAID DISKS, SAID DISKS HAVING BETWEEN THEM A PLURALITY OF DISCHARGE PORTS ARRANGED AROUND SAID DISKS FOR DISCHARGE OF COMBUSTION GAS THERETHROUGH FROM THE COMBUSTION CHAMBER BETWEEN SAID DISKS IN A DIRECTION GENERALLY TANGENTIALLY OF SAID DISKS AND OPPOSITE TO THE DIRECTION OF MOVEMENT OF THE PERIPHERIES OF SAID DISKS DURING ROTATION OF SAID ROTOR, AND CENTRIFUGAL BLOWER MEANS AT THE SIDE OF EACH DISK REMOTE FROM THE COMBUSTION CHAMBER AND THE OTHER DISK, ROTATABLE WITH SAID DISKS ABOUT THE AXES THEREOF FOR SUPPLYING COOLING AIR TO COOL THE SIDES OF SAID DISKS OPPOSITE THE COMBUSTION CHAMBER AND INCLUDING A SECOND AIR INLET ALONGSIDE SAID FIRST AIR INLET AND OPENING ADJACENT TO AND
Claim 2
Dependent Claim
162 words
A ROTARY RADIAL FLOW JET ENGINE COMPRISING A ROTOR INCLUDING TWO DISKS ROTATABLE ABOUT A COMMON AXIS AND SPACED AXIALLY THEREOF FOR DEFINING A COMBUSTION CHAMBER THEREBETWEEN, SAID ROTOR HAVING A FIRST AIR INLET TO THE COMBUSTION CHAMBER BETWEEN SAID DISKS, MEANS SUPPLYING FUEL TO THE COMBUSTION CHAMBER BETWEEN SAID DISKS, SAID DISKS HAVING BETWEEN THEM A PLURALITY OF DISCHARGE PORTS ARRANGED AROUND SAID DISKS FOR DISCHARGE OF COMBUSTION GAS THERETHROUGH FROM THE COMBUSTION CHAMBER BETWEEN SAID DISKS IN A DIRECTION GENERALLY TANGENTIALLY OF SAID DISKS AND OPPOSITE TO THE DIRECTION OF MOVEMENT OF THE PERIPHERIES OF SAID DISKS DURING ROTATION OF SAID ROTOR, AND CENTRIFUGAL BLOWER MEANS AT THE SIDE OF EACH DISK REMOTE FROM THE COMBUSTION CHAMBER AND THE OTHER DISK, ROTATABLE WITH SAID DISKS ABOUT THE AXES THEREOF FOR SUPPLYING COOLING AIR TO COOL THE SIDES OF SAID DISKS OPPOSITE THE COMBUSTION CHAMBER AND INCLUDING A SECOND AIR INLET ALONGSIDE SAID FIRST AIR INLET AND OPENING ADJACENT TO AND
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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) | 1966-02-11 | 1966-08-13 | 1967-02-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1970-02-11 | 1970-08-13 | 1971-02-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1974-02-11 | 1974-08-13 | 1975-02-12 | $7700.00 | Window Closed / Lapsed |