USPatent applicationPatented

Torque converter having an integrated cover with bearing support

Granted 15 May 2012 · 1 office action

Current assignee: SCHAEFFLER TECHNOLOGIES AG & CO. KG · originally Schaeffler Group

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Inventors: Scott Schrader · Examiner: Daniel Lopez · AU 3745 · TC 3700

Life of the application

15 dated events
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Abstract

A torque converter including a cover, the cover having an axis and having an axially extending flange about the axis, the flange defining an aperture, a pilot fitted within the aperture, and a turbine hub connected to the flange.

Description

5 parts
›Priority to U.S. Provisional Patent Application Ser. No…

Priority to U.S. Provisional Patent Application Ser. No. 61/003,047, filed Nov. 14, 2007, is claimed, the entire disclosure of which is hereby incorporated by reference herein.

The present invention relates generally to a torque converter having a cover.

›BACKGROUND

U.S. Pat. Nos. 5,667,043 and 6,085,879, hereby incorporated by reference herein, disclose torque converters.

FIG. 1 is a cross sectional view of a prior art torque converter 10 , for example as in U.S. Pat. No. 5,667,043. Torque converter 10 contains a cover 2 , an impeller 32 , a turbine 30 , a stator 34 and a lock-up clutch 38 . Lock-up clutch 38 includes a piston 28 , a plate 40 , and friction linings 24 , 26 . Between cover 2 and piston 28 is a chamber 20 . Turbine 30 is oriented concentrically to a hub axis 4 . Connected to cover 2 via a weld is a bearing neck 6 which is guided into a crankshaft of an internal combustion engine. Bearing neck 6 and a support ring 8 form one piece, referred to as a pilot 14 . Pilot 14 includes a flow guide 16 which can extend into chamber 20 . Piston 28 is connected via leaf springs 22 to a ring plate 18 . Ring plate 18 can be pressed to support ring 8 . Support ring 8 is connected to a turbine hub 12 via a bearing 42 . Turbine hub 12 is mounted on a drive shaft 36 .

›SUMMARY OF THE INVENTION

A torque converter including a cover, the cover having an axis and having an axially extending flange about the axis, the flange defining an aperture, a pilot fitted within the aperture, and a turbine hub connected to the flange.

›BRIEF DESCRIPTION OF THE INVENTION

FIG. 1 illustrates a sectional view of a prior art torque converter.

An embodiment of the present invention is described with respect to the following detailed description taken in conjunction with the accompanying drawing, in which:

FIG. 2 illustrates a sectional view of one embodiment of a torque converter of the present invention.

FIG. 3 illustrates the pilot in the embodiment of FIG. 2 of the present invention.

FIG. 4 is a perspective view of the embodiment of FIG. 2 of the present invention.

›DETAILED DESCRIPTION

FIG. 2 and FIG. 4 both show a section of a torque converter 100 which can have a pump impeller, a turbine, an impeller, a stator and a lock-up clutch as described with respect to the torque converter in FIG. 1 . Torque converter 100 of the present invention has an axis A and includes a cover 102 and a pilot 106 . Cover 102 encloses a turbine hub 108 . Cover 102 has an axially extending flange 104 bending inward toward turbine hub 108 . Flanges 104 define an aperture 118 . Pilot 106 is fitted in aperture 118 . Pilot 106 may be welded 130 to cover 102 . A space 120 is created between pilot 106 and cover 102 . Flow holes 114 are stamped in flanges 104 of cover 102 allowing fluid to flow through passageway 110 . Flange 104 supports a ball bearing 112 located between flange 104 of cover 102 and turbine hub 108 . Turbine hub 108 thus may also have an axially extending flange 109 , with bearing 112 located radially inward with respect to flange 109 .

Pilot 106 may be forged. Pilot 106 may have four different radial diameters D 1 , D 2 , D 3 and D 4 . Diameter D 4 may be equivalent to a diameter of aperture 118 in cover 102 . The portion of pilot 106 with diameter D 4 is inserted in aperture 118 and may have a fin 116 . D 4 axially extends contacting the sides of aperture 118 . Fin 116 drives the flow from stamped flow holes 114 through passageway 110 , or vice versa. The portion of pilot 106 having diameter D 3 is welded to cover 102 .

FIG. 3 shows pilot 106 in a more detailed section. Pilot 106 has 4 cylindrical portions 122 , 124 , 126 and 128 with varying diameters D 1 , D 2 , D 3 , D 4 . Portion 128 has a fin 116 . Diameters of the cylindrical portions D 1 and D 3 are larger than other portions D 2 and D 4 , D 4 being the smallest.

The present invention eliminates one component from the current art which enhances performance. Furthermore, the reduction in the necessary components may improve both cost and efficiency of manufacturing. Flange 104 may for example be created integral with the cover, for example via a punching process.

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Claims as granted

18 claims

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Classifications

2 codes
IPC · International Patent Classification
Section F — Mechanical engineering; lighting; heating; weapons
  • F16D33/18
USPC · US Patent Classification
60/330

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File wrapper

⤢ drag to zoomJan 2009Jul 2009Jan 2010Jul 2010Jan 2011Jul 2011Jan 2012Jul 2012USPTOApplicantNon-final rejectionExaminer-initiated interview
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Pendency
3.5 y
1,280 days filing → grant
Office actions
1
non-final + final
Responses
1
no RCE
Interviews
1
examiner interview summaries
Examiner
Daniel Lopez
art unit 3745 · TC 3700
Citations: 5 back · 1 forward

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Chain of title

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