Methods and apparatus for assembling gas turbine engines
CA 2545761 C · Owner: General Electric Company · Inventors: Renggli, Bernard James; Jumper, Matthew Wilson
Overview
Its claims, description and drawings are in the Canadian Patents Database.
Open the CIPO recordAbstract From the Canadian patent
A nozzle assembly (100) for an engine (10) including a core engine (40) and at least one bypass duct (52) for channeling airflow around the core engine includes a liner (110) comprising an inner surface and an outer surface wherein the inner surface confines airflow within a nozzle bypass duct (108) and the outer surface confines airflow discharged from the core engine. A plurality of strut members (106) are coupled to and support the liner. A plurality of fairings (104) are in flow communication with the at least one bypass duct and each fairing is upstream from a respective one of the plurality of strut members to facilitate directing a portion of the airflow from the bypass duct past the …
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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 4, 2006 and granted October 15, 2013. A Canadian patent filed from October 1, 1989 lasts 20 years from filing, so its term ended May 4, 2026.
- Certificates of supplementary protection extend only drug patents, and it isn't classified as one.
- We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
Timeline
Timeline From CIPO dates
Sources & verification
Official CIPO records
Everything on this page comes from the CIPO record linked above. Contains information licensed under the Open Government Licence – Canada.