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Canadian application, no grantCanada

Hovering gyro aircraft

CA 2348217 A1 · Owner: Carter, Jay W. Jr. · Inventors: Carter, Jay W. Jr.

CIPO record

Overview

Drawings and full text

Its claims, description and drawings are in the Canadian Patents Database.

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Abstract From the Canadian patent

A fixed wing rotorcraft uses differential thrust between wing mounted propellers, to provide counter torque when the rotor is being powered by a power source. The, rotorcraft is comprised of s fuselage to which fixed wings are attached. A rotor is, attached on an upper side of the fuselage and provides lift at low speeds while the wings, provide a majority of the lift at high speeds. When at high speeds the rotor may be slowed, to reduce advancing tip speed and retreating blade stall. Forward thrust and counter, torque is provided by propellers mounted on either side of the fuselage or even on the, wings.

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Listed from its CIPO record in Patent Yard's archive of Canadian patents past their term. Its claims, description and drawings are in the CIPO record and on Google Patents, and the Claude kit works from them.

Why it's free to use

  • Filed May 22, 2001. No grant is recorded for it in Canada; had it been granted, its 20-year term would have ended May 22, 2021.
  • A certificate of supplementary protection adds at most two years for a drug, so even that would have ended by May 22, 2023.
  • We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
FiledMay 22, 2001
GrantedNo grant recorded
Term endedMay 22, 2021
Patent numberCA 2348217 A1
Classification (IPC)B64C27/02 +1 more

Timeline

Timeline From CIPO dates

2002200420062008201020122014201620182020Application filedMay 22, 2001Term endedMay 22, 2021

Sources & verification

Everything on this page comes from the CIPO record linked above. Contains information licensed under the Open Government Licence – Canada.