US3144907A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Helicopter rotor and method of making a blade member thereof
Assignee: Kaman Aircraft Corp
•
Filing: 1959-11-04
•
Granted: 1964-08-18
•
Expires: 1979-11-04
Abstract
No abstract record available.
Inventors
- 👤 George F Lubben
- 👤 John J Schauble
- 👤 George A Mccoubrey
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 06:16
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/46; B64C27/473; B64C27/04; B64C27/12; B64C27/16; B64C27/18; B64C27/54
Claims Analysis
Total Claims: 1
Claim 1
Independent Claim
313 words
THE COMBINATION IN A HELICOPTER ROTOR, OF A HUB ROTATABLE ABOUT AN APPROXIMATELY VERTICAL AXIS, A GRIP MEMBER CONNECTED WITH THE HUB FOR PIVOTAL MOVEMENT ABOUT A NONRADIAL AXIS IN FIXED RELATION TO THE HUB, A BLADE BODY EXTENDING RADIALLY OUTWARDLY FROM THE GRIP MEMBER AND HAVING AN AIRFOIL LIFTING PORTION, INTERENGAGING ELEMENTS RESPECTIVELY ON SAID GRIP MEMBER AND ON THE INNER END OF SAID BODY FOR PREVENTING BODILY MOVEMENT OF THE INNER END OF THE BODY IN ANY NONRADIAL DIRECTION WHICH ELEMENTS ARE CONSTRUCTED AND ARRANGED TO PERMIT SAID BODY TO MOVE RELATIVELY TO THE HUB MEMBER EITHER ROTATABLY ABOUT THE RADIAL AXIS OR RADIALY OUTWARDLY, FOUR SEPARATE GENERALLY RADIAL TENSION-TORSION MEMBERS FIXEDLY CONNECTED AT THEIR INNER ENDS WITH THE GRIP MEMBERS AND FIXEDLY CONNECTED AT THEIR OUTER ENDS WITH THE BLADE BODY WHICH TENSION-TORSION MEMBERS PREVENT RADIALLY OUTWARD MOVEMENT OF THE BLADE BODY AND WHICH TENSION-TORSION MEMBERS HAVE TORSIONAL RESILIENCY TO RESIST ROTATIVE MOVEMENT OF SAID BODY ABOUT SAID RADIAL AXIS WHILE PERMITTING SUCH MOVEMENT TO A LIMITED EXTENT, TWO OF SAID TENSION-TORSION MEMBERS BEING IN SUPERPOSED POSITIONS AND VERTICALLY SPACED FROM EACH OTHER THROUGHOUT THEIR ENTIRE LENGTH AND CONSTITUTING A PAIR OF MEMBERS SPACED IN THE LEADING DIRECTION FROM SAID RADIAL AXIS AND THE OTHER TWO OF SAID TENSION-TORSION MEMBERS BEING IN SUPERPOSED POSITIONS AND VERTICALLY SPACED FROM EACH OTHER THROUGHOUT A PORTION OF THEIR LENGTH AND IN ENGAGEMENT WITH EACH OTHER THROUGHOUT ANOTHER PORTION OF THEIR LENGTH AND CONSTITUTING A PAIR OF MEMBERS SPACED IN THE TRAILING DIRECTION FROM SAID RADIAL AXIS, A SERVO-FLAP CARRIED BY THE AIRFOIL PORTION OF THE BLADE BODY AND ANGULARLY ADJUSTABLE RELATIVE THERETO, AND MEANS FOR ANGULARLY ADJUSTING SAID SERVO-FLAP TO ENABLE IT DURING ROTOR ROTATION TO AERODYNAMICALLY EFFECT ADJUSTMENT OF THE BLADE BODY ABOUT SAID RADIAL AXIS AND RELATIVELY TO THE GRIP MEMBER AS PERMITTED BY THE TORSIONAL RESILIENCY OF SAID TENSIONTORSION MEMBERS.
References Cited (Backward Citations)
GB418698A
Cited
US2429646A
Cited
US2430948A
Cited
FR909803A
Cited
US2600531A
Cited
US2674327A
Cited
US2631676A
Cited
US2620884A
Cited
US2606278A
Cited
US2754918A
Cited
US2771144A
Cited
US2757745A
Cited
US2754917A
Cited
US2963094A
Cited
US2818123A
Cited
US2950768A
Cited
US2961051A
Cited
US2994384A
Cited
US2949967A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1967-08-18 | 1968-02-17 | 1968-08-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1971-08-18 | 1972-02-17 | 1972-08-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1975-08-18 | 1976-02-17 | 1976-08-18 | $7700.00 | Window Closed / Lapsed |