-
公开(公告)号:US20160003129A1
公开(公告)日:2016-01-07
申请号:US14854642
申请日:2015-09-15
Applicant: EATON CORPORATION
Inventor: Matthew Gareld SWARTZLANDER , Jason Christopher KOVAL
CPC classification number: F02B33/38 , F02B39/04 , F02B39/16 , F04C18/126 , F04C18/16 , F04C28/10 , F04C28/18 , F04C29/06 , F04C29/065 , F04C29/12
Abstract: A Roots-type supercharger 100, 1100 includes a housing 120, 1120, a first rotor 200, a second rotor 300, an outlet volume 400, a transfer volume 500, and a bleed port 600, 600′, 1600. The housing includes an interior chamber 130, an inlet port 140, and an outlet port 150, 1150. The first rotor 200 and the second rotor 300 have a plurality of lobes 210, 310, respectively. The outlet volume 400 is substantially bounded between the outlet port, the first rotor, the second rotor, and the interior chamber of the housing. The transfer volume 500 is substantially bounded between the first rotor, the second rotor, and the interior chamber of the housing. The bleed port 600, 600′, 1600 is adapted to fluidly connect the outlet volume and the transfer volume at least during a portion of a transfer volume cycle. The variable bleed port may include a plate that pivots about a pivot or slides along a slide. The plate may be arc shaped and may arc around a centerline of one of the rotors. The plate may be positioned within an operating cavity. The operating cavity may be defined within the housing between a bearing plate and a main housing of the housing. A method of supercharging an internal combustion engine includes bleeding a transfer volume to an outlet volume through a bleed port.
Abstract translation: 罗茨式增压器100,1100包括壳体120,1120,第一转子200,第二转子300,出口容积400,输送体积500和排出口600,600',1600.壳体包括 内部室130,入口端口140和出口端口150,1150。第一转子200和第二转子300分别具有多个叶片210,310。 出口容积400基本上限定在出口,第一转子,第二转子和壳体的内部室之间。 传送体积500基本上限定在第一转子,第二转子和壳体的内部室之间。 排出口600,600',1600适于至少在传送体积循环的一部分期间流体地连接出口容积和传送体积。 可变排气口可以包括围绕枢轴枢转或者沿滑动件滑动的板。 该板可以是弧形的并且可围绕其中一个转子的中心线。 板可以定位在操作腔内。 操作空腔可以在壳体内限定在轴承板和壳体的主壳体之间。 一种对内燃机进行增压的方法包括通过排放口将转运体积泄漏到出口容积。
-
公开(公告)号:US20170248019A1
公开(公告)日:2017-08-31
申请号:US15513517
申请日:2015-09-22
Applicant: EATON CORPORATION
Inventor: Matthew Gareld SWARTZLANDER
IPC: F01C21/08 , F01C13/00 , F04C2/18 , F04C28/04 , F03B13/08 , F03B15/00 , F01C20/04 , F04C14/04 , F01C1/16 , F04C18/18
CPC classification number: F01C21/08 , F01C1/16 , F01C13/00 , F01C20/04 , F03B3/103 , F03B13/06 , F03B13/08 , F03B13/086 , F03B15/00 , F03C2/08 , F04C2/084 , F04C2/16 , F04C2/18 , F04C13/008 , F04C14/04 , F04C18/18 , F04C28/04 , F04C2240/20 , F05B2210/402 , F05B2220/32 , F05B2240/301 , F05B2250/25 , Y02E10/22 , Y02E10/223 , Y02E10/226 , Y02E10/28 , Y02E60/17
Abstract: A gear pump for power generation comprises a first rotor and a second rotor in a case. The first rotor comprises a first plurality of radially spaced teeth, wherein the first plurality of radially spaced teeth wrap around the first rotor helically in a clockwise direction, and wherein at a first position the first plurality of radially spaced teeth have a helix angle different than the helix angle of the first plurality of radially spaced teeth at a second position. The second rotor comprises a second plurality of radially spaced teeth, wherein the second plurality of radially spaced teeth wrap around the second rotor helically in a counter-clockwise direction, and wherein at a first position the second plurality of radially spaced teeth have a helix angle different than the helix angle of the second plurality of radially spaced teeth at a second position.
-
3.
公开(公告)号:US20170146012A1
公开(公告)日:2017-05-25
申请号:US15323495
申请日:2015-07-01
Applicant: EATON CORPORATION
Abstract: A method of treating, tuning, assembling, and/or overhauling a twin rotor device (200, 1200) includes applying a coating material (102) on an internal set of working surfaces (218, 222, 224, 226, 228, 1218, 1222, 1224, 1226, 1228) of the twin rotor device when at least partially assembled. The coating may be factory or field applied to a new or used twin rotor device. The working surfaces may be uncoated or previously coated and may be built-up as the coating material forms a coating (206, 1206) on at least some of the working surfaces. Manufacturing variations of a pair of rotors (220, 1220) and a housing (210, 1210) may be compensated by the coating. One or more performance characteristics of the twin rotor device may be improved by the coating, and variation between a series of twin rotor device may be reduced or substantially eliminated. The coating may reduce internal leakage and increase volumetric efficiency of the twin rotor device. The twin rotor device may be a supercharger 200, a screw compressor 1200, or other twin rotor device.
-
-