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Canadian application, no grantCanada

Jet engine thrust reverser system having torque limited synchronization

CA 2463817 A1 · Owner: Honeywell International Inc. · Inventors: Chakkera, Kevin K.; Johnson, Andrew T.

CIPO record

Overview

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

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Abstract From the Canadian patent

A thrust reverser system that has one or more moveable thrust reverser components for redirecting the thrust of a jet engine. The thrust reverser system has a torque limiter coupled between synchronization mechanisms that mechanically couple actuators used to drive the thrust reverser. The torque limiter reduces the potential for the transmission of excessive torque between the different moveable thrust reverser components and reduces the likelihood , of secondary system damage due to a jam in the system. Thus the cost and/or , weight associated with each of the components comprising the system may be reduced.

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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 October 16, 2002. No grant is recorded for it in Canada; had it been granted, its 20-year term would have ended October 16, 2022.
  • A certificate of supplementary protection adds at most two years for a drug, so even that would have ended by October 16, 2024.
  • We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
FiledOctober 16, 2002
GrantedNo grant recorded
Term endedOctober 16, 2022
Patent numberCA 2463817 A1
Classification (IPC)F02K1/76 +2 more

Timeline

Timeline From CIPO dates

2003200520072009201120132015201720192021Application filedOct 16, 2002Term endedOct 16, 2022

Sources & verification

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