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US3289770A Expired / Lapsed US ⏱️ 0.0 years remaining

Helicopter rotor system

Assignee: Bolkow GmbH
•
Filing: 1964-08-03
•
Granted: 1966-12-06
•
Expires: 1984-08-03
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Abstract

No abstract record available.

Inventors

  • 👤 Derschmidt Hans

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 15:35
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/54; B64C27/001; B64C27/32; B64C27/37; B64C27/39; B64C2027/005

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 126 words
A HELICOPTER ROTOR CONSTRUCTION COMPRISING A ROTOR ROTATABLE ABOUT AN AXIS WHICH IS SUBSTANTIALLY VERTICAL, A PLURALITY OF ROTOR BLADES PIVOTALLY MOUNTED ON SAID ROTOR AT A SPACED LOCATION FROM THE AXIS OF ROTATION THEREOF AND EACH BEING PIVOTAL FOR MOVEMENT IN LEAD-LAG DIRECTIONS ABOUT AN AXIS SUBSTANTIALLY PARALLEL TO THE AXIS OF ROTATION OF SAID ROTOR DURING THE ROTATION OF SAID ROTOR, AND MASS IMBALANCE PRODUCING MANS OPERATIVELY ASSOCIATED WITH SAID ROTOR BY A TRANSMISSION MEANS, THE TRANSMISSION ROTIO OF WHICH EFFECTS A MASS ROTATIONAL SPEED OF A MULTIPLE OF THE ROTOR SPEED IN THE DIRECTION OF ROTATION OF THE ROTOR, SAID MULTIPLE CORRESPONDS TO THE NUMBER OF ROTOR BLADES, FOR INFLUENCING THE PIVOTAL LEAD-LAG MOVEMENT OF SAID ROTOR BLADES DURING ROTATION OF SAID ROTOR.
Claim 2
Dependent Claim 126 words
A HELICOPTER ROTOR CONSTRUCTION COMPRISING A ROTOR ROTATABLE ABOUT AN AXIS WHICH IS SUBSTANTIALLY VERTICAL, A PLURALITY OF ROTOR BLADES PIVOTALLY MOUNTED ON SAID ROTOR AT A SPACED LOCATION FROM THE AXIS OF ROTATION THEREOF AND EACH BEING PIVOTAL FOR MOVEMENT IN LEAD-LAG DIRECTIONS ABOUT AN AXIS SUBSTANTIALLY PARALLEL TO THE AXIS OF ROTATION OF SAID ROTOR DURING THE ROTATION OF SAID ROTOR, AND MASS IMBALANCE PRODUCING MANS OPERATIVELY ASSOCIATED WITH SAID ROTOR BY A TRANSMISSION MEANS, THE TRANSMISSION ROTIO OF WHICH EFFECTS A MASS ROTATIONAL SPEED OF A MULTIPLE OF THE ROTOR SPEED IN THE DIRECTION OF ROTATION OF THE ROTOR, SAID MULTIPLE CORRESPONDS TO THE NUMBER OF ROTOR BLADES, FOR INFLUENCING THE PIVOTAL LEAD-LAG MOVEMENT OF SAID ROTOR BLADES DURING ROTATION OF SAID ROTOR.

References Cited (Backward Citations)

FR748909A Cited
US2127888A Cited
FR798294A Cited
DE1015318B Cited
US3139937A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-12-05 1970-06-06 1970-12-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-12-05 1974-06-06 1974-12-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-12-05 1978-06-06 1978-12-06 $7700.00 Window Closed / Lapsed

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