Invention Grant
- Patent Title: Assembly for turbomachine combustion chamber comprising a boss and an annular element
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Application No.: US15320619Application Date: 2015-06-19
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Publication No.: US10941943B2Publication Date: 2021-03-09
- Inventor: Ludovic Andre Joel Naudot , Philippe Olharan , Jean Menet-Haure
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1455862 20140624
- International Application: PCT/FR2015/051633 WO 20150619
- International Announcement: WO2015/197954 WO 20151230
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F23R3/00 ; B23P11/00 ; F23R3/06 ; F23R3/46

Abstract:
An assembly for a turbomachine combustion chamber, including a boss for turbomachine combustion chamber, including a tubular body configured to be inserted in a receiving orifice formed in an annular wall of a flame tube and to accommodate a shank of a connecting pin for connecting the flame tube to an external casing, a first end of the boss including an annular flange configured to prevent radial translational movement of the boss in a first direction, and a second end of the boss being configured to be crimped to the wall of the flame tube so as to prevent radial translational movement of the boss in a second direction, and an annular element configured to fit coaxially with the receiving orifice and in radial contact with the annular wall of the flame tube on the one hand and with the annular flange of the boss on the other.
Public/Granted literature
- US20170198915A1 ASSEMBLY FOR TURBOMACHINE COMBUSTION CHAMBER COMPRISING A BOSS AND AN ANNULAR ELEMENT Public/Granted day:2017-07-13
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