Invention Grant
US08944793B2 Flow and pressure ripple reduction with advance dual gear and bearing face cut 有权
流量和压力波动减少与先进的双齿轮和轴承面切割

Flow and pressure ripple reduction with advance dual gear and bearing face cut
Abstract:
An aircraft turbine engine Fuel Metering Unit (FMU) is provided including a main gear pump having a main drive gear and a main driven gear and a servo gear pump having a servo drive gear and a servo driven gear. The main drive gear and the servo drive gear are received on an input shaft. The main driven gear is mounted to a first shaft oriented parallel to and adjacent a first side of the input shaft. The main driven gear is in meshing engagement with the main drive gear. The servo drive gear is mounted to a second shaft arranged parallel to and adjacent a second, opposite side of the input shaft. The servo driven gear is in meshing engagement with the servo drive gear.
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