Methods and apparatus for operating gas turbine engines
CA 2499675 C · Owner: Turco, John B. · Inventors: Turco, John B.; Wollenweber, Gary Craig
Overview
Its claims, description and drawings are in the Canadian Patents Database.
Open the CIPO recordAbstract From the Canadian patent
An aircraft gas turbine engine assembly (10) including at least one propelling gas turbine engine (11) comprising a core engine (13) and an exhaust (32). The core engine includes at least one turbine (20) for generating thrust for the aircraft; and at least one auxiliary engine (12) including an inlet (24) at least one turbine (44), and an exhaust (80). The inlet is coupled in flow communication with at least one propelling gas turbine engine such that a portion of airflow (31) flowing through the propelling engine is extracted from the propelling engine upstream from the propelling engine turbine and is channeled to the auxiliary engine for generating power.
Read the whole patent
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 March 3, 2005 and granted October 22, 2013. A Canadian patent filed from October 1, 1989 lasts 20 years from filing, so its term ended March 3, 2025.
- 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.