CA3105434A1 - Reacteur a double flux, nacelle de celui-ci et methode de fonctionnement associee - Google Patents

Reacteur a double flux, nacelle de celui-ci et methode de fonctionnement associee Download PDF

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Publication number
CA3105434A1
CA3105434A1 CA3105434A CA3105434A CA3105434A1 CA 3105434 A1 CA3105434 A1 CA 3105434A1 CA 3105434 A CA3105434 A CA 3105434A CA 3105434 A CA3105434 A CA 3105434A CA 3105434 A1 CA3105434 A1 CA 3105434A1
Authority
CA
Canada
Prior art keywords
nacelle
fan
apertures
circumferentially
duct wall
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CA3105434A
Other languages
English (en)
Inventor
Philippe-Andre TETRAULT
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US16/699,001 external-priority patent/US20210163141A1/en
Application filed by Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Publication of CA3105434A1 publication Critical patent/CA3105434A1/fr
Pending legal-status Critical Current

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  • Structures Of Non-Positive Displacement Pumps (AREA)
CA3105434A 2019-11-28 2021-01-07 Reacteur a double flux, nacelle de celui-ci et methode de fonctionnement associee Pending CA3105434A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US16/699,001 US20210163141A1 (en) 2019-11-28 2019-11-28 Gas turbine engine, nacelle thereof, and associated method of operating a gas turbine engine
US16/699,001 2019-11-28
US16/774,778 US11807379B2 (en) 2019-11-28 2020-01-28 Turbofan engine, nacelle thereof, and associated method of operation
US16/774,778 2020-01-28

Publications (1)

Publication Number Publication Date
CA3105434A1 true CA3105434A1 (fr) 2021-05-28

Family

ID=76088944

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3105434A Pending CA3105434A1 (fr) 2019-11-28 2021-01-07 Reacteur a double flux, nacelle de celui-ci et methode de fonctionnement associee

Country Status (1)

Country Link
CA (1) CA3105434A1 (fr)

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