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Title:
軸対称の封止可能なギムレットを有する軸受ホルダ
Document Type and Number:
Japanese Patent JP6395833
Kind Code:
B2
Abstract:
A bypass engine bearing holder (1) that holds an upstream bearing (6) and defines, with said upstream bearing, an oil chamber (100) and an air chamber (200), comprising a frusto-conical portion (11) defining an upstream bearing chamber (160) and a downstream inner chamber (150), and includes an outer collar (13) connected, by a weld (135), to a flange (15) that extends outward from the frusto-conical portion (11). The outer collar (13) has a sealable gimlet (131) engaging with the upstream bearing (6) such as to seal the oil chamber (100). The bearing holder (1) includes a plurality of oil recovery ducts (8) leading to the downstream inner chamber (150) and to the upstream bearing chamber (160). The oil recovery ducts (8) lead to the upstream bearing chamber (160), downstream from the weld (135) of the outer collar (13) on the flange (15), the weld (135) of the outer collar (13) being axisymmetric.

Inventors:
Noel, Frederick
Doubre, Benoit Arjemiro Mathieu
Do Susa, Mario Cesar
Gosalussian-Pryrieux, Gregory
Pomier, Nicola
Application Number:
JP2016532635A
Publication Date:
September 26, 2018
Filing Date:
November 18, 2014
Export Citation:
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Assignee:
Saffron Aircraft Engines
International Classes:
F01D25/16; F02C7/00; F02C7/28
Domestic Patent References:
JP2006125398A
JP2006153013A
JP2006342798A
JP10299416A
Foreign References:
US20130183142
FR2752024A1
US20090199534
Attorney, Agent or Firm:
Kawaguchi International Patent Office