Squeeze film damper oil control
AssigneeGeneral Electric Company
InventorMelvin Bobo
Life of this patent
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Abstract
A damper bearing assembly and method for damper oil conservation and recirculation. The assembly includes opposed channels enclosing a squeeze film space and open to direct flow from the damper squeeze film space. The channels can isolate the squeeze film space from leakage points in the assembly, and can be profiled to direct fluid exiting from the high pressure region away from leakage points. The channels isolate the low pressure region in the squeeze film from leakage points to prevent air entrainment.
Claims10
A damper bearing assembly for use in a gas turbine engine, the bearing assembly comprising:
- (a) a bearing support member disposed for rotation in a housing, the support member and housing defining a fluid annular squeeze film space there between;
- (b) the squeeze film space enclosed by a pair of opposed, circumferentially extending channels disposed in the housing, each channel open to direct flow from the annular squeeze film space;
- (c) each channel in flow communication with an associated clearance gap formed between a support member sidewall and a housing sidewall, and wherein each channel radially and axially spaces the squeeze film space from the channel's associated clearance gap;
- (d) each channel including a circumferentially extending surface portion which is inclined with respect to flow exiting the squeeze film space to direct flow away from the channel's associated clearance gap.
In a damper bearing assembly including a bearing support member disposed in a housing to define a fluid filled annular squeeze film space, a method of recirculating damper fluid comprising the steps of:
- (a) flowing fluid from a high pressure region in the squeeze film space directly into a pair of circumferentially extending channels enclosing the squeeze film space;
- (b) channeling the fluid to a low pressure region in the squeeze film space;
- and
- (c) impinging the fluid on an inclined channel surface portion in each channel to direct the fluid into the channels.
A damper bearing assembly for use in a gas turbine engine, the bearing assembly comprising:
- (a) a bearing outer race disposed for rotation in bearing housing, the outer race including a race annular surface separating spaced-apart race sidewalls, the housing including a housing annular surface facing the race annular surface and a pair of spaced-apart housing sidewalls, each housing sidewall facing an adjacent race sidewall;
- (b) an annular squeeze film space defined between the race and housing annular surfaces;
- (c) a pair of clearance gaps defined between adjacent race and housing sidewalls;
- and
- (d) a pair of circumferentially extending channels disposed in the housing and enclosing the squeeze film space, each channel having a nominal cross-sectional area at least twice the cross-sectional area of the squeeze film space, each channel directly open to flow from the annular squeeze film space, and each channel having a surface portion spaced axially and radially from an associated clearance gap and inclined between 30 and 60 degrees with respect to flow entering the channel and impinging on the inclined surface portion, the surface portion inclined to direct flow entering the channel away from a clearance gap associated with the channel.
Dependencies are inferred from the claim text.