CA3305202A1 - Helicopter turbine engine subassembly and helicopter turbine engine comprising such a subassembly - Google Patents

Helicopter turbine engine subassembly and helicopter turbine engine comprising such a subassembly

Info

Publication number
CA3305202A1
CA3305202A1 CA3305202A CA3305202A CA3305202A1 CA 3305202 A1 CA3305202 A1 CA 3305202A1 CA 3305202 A CA3305202 A CA 3305202A CA 3305202 A CA3305202 A CA 3305202A CA 3305202 A1 CA3305202 A1 CA 3305202A1
Authority
CA
Canada
Prior art keywords
hélicoptère
turbomachine
ensemble
sous
comprenant
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
CA3305202A
Other languages
English (en)
Inventor
Alexandre Paul Raimond DEBAT
Sébastien Mathieu COMBEBIAS
Olivier Robert
Nicolas Christophe PERRA
Original Assignee
Safran Helicopter Engines SAS
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
Application filed by Safran Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Publication of CA3305202A1 publication Critical patent/CA3305202A1/fr
Pending legal-status Critical Current

Links

CA3305202A 2023-09-18 2024-09-17 Helicopter turbine engine subassembly and helicopter turbine engine comprising such a subassembly Pending CA3305202A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FRFR2309821 2023-09-18

Publications (1)

Publication Number Publication Date
CA3305202A1 true CA3305202A1 (fr) 2025-03-27

Family

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