Invention Grant
- Patent Title: Intermediate case supporting removable panels fitted with retaining elements
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Application No.: US16835465Application Date: 2020-03-31
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Publication No.: US11261758B2Publication Date: 2022-03-01
- Inventor: Frédéric Jacques Eugène Goupil , Rémi Abarrou , Azath Mohamed
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pearne & Gordon LLP
- Priority: FR1903585 20190403
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F02C7/32

Abstract:
An intermediate turbojet case comprises a hub that supports removable panels and bleed lines, the hub comprising a flank provided with openings, each bleed line having an upstream end engaged in an opening in the flank and a downstream end terminated by a base plate through which it is fixed to an internal face of a removable panel by way of screws, each removable panel having a front edge at which it is fixed to an external lip of the hub by screws. At least one removable panel comprises a downstream edge supporting a retaining element close to the internal face to hold the base plate in contact with the internal face during a phase in which the removable panel is fixed to the hub by screwing, this phase preceding attachment of the base plate to the removable panel by screwing.
Public/Granted literature
- US20200318494A1 INTERMEDIATE CASE SUPPORTING REMOVABLE PANELS FITTED WITH RETAINING ELEMENTS Public/Granted day:2020-10-08
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