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WO2014046933A1 - Actuation device, in particular electronic actuator - Google Patents

Actuation device, in particular electronic actuator Download PDF

Info

Publication number
WO2014046933A1
WO2014046933A1 PCT/US2013/059181 US2013059181W WO2014046933A1 WO 2014046933 A1 WO2014046933 A1 WO 2014046933A1 US 2013059181 W US2013059181 W US 2013059181W WO 2014046933 A1 WO2014046933 A1 WO 2014046933A1
Authority
WO
WIPO (PCT)
Prior art keywords
actuation
actuation device
journal
shank
central part
Prior art date
Application number
PCT/US2013/059181
Other languages
French (fr)
Inventor
Hans-Joerg FETZER
Jochen Kraemer
Original Assignee
Borgwarner Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Borgwarner Inc. filed Critical Borgwarner Inc.
Publication of WO2014046933A1 publication Critical patent/WO2014046933A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183Arrangements of bypass valves or actuators therefor
    • F02B37/186Arrangements of actuators or linkage for bypass valves
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the invention relates to an actuation device according to claim 1 , in particular an electronic actuator.
  • Claims 11 and 12 define an exhaust-gas turbocharger according to the invention as an independently marketable product.
  • Figure 1 shows a perspective illustration of an actuation device according to the invention
  • Figure 2 shows a detail illustration of a redirecting device
  • Figure 3 shows a front view of a shielding cap
  • Figure 4 shows a perspective illustration of the shielding cap as per figure
  • Figure 5 shows a perspective sectional illustration of a known exhaust-gas turbocharger having an actuator which can be replaced with the actuation device as per figure 1 in order to convert the exhaust-gas turbocharger into a turbocharger according to invention.
  • Figure 1 illustrates an actuation device 1 according to the invention which, in the example, is in the form of an electronic actuator (electric actuator).
  • the electric actuator 1 has a housing 2 in which an actuation shank (not visible in its entirety) is guided by way of a first shank portion.
  • the actuation shank has a second shank portion 3 which projects out of the housing 2 and which is indicated by dashed lines in figure 1.
  • said second shank portion 3 is surrounded by a shielding cap 4 which is fastened, in particular screwed, to the housing 2.
  • the second shank portion 3 is, aside from a fastening region 5, covered by the shielding cap 4 in order to prevent an undesired introduction of heat into the shank portion 3.
  • the shielding cap 4 has two interconnected first and second cylinder portions 6 and 7.
  • the cylinder portion 6 has a diameter Di which is smaller than the diameter D 2 of the cylinder portion 7.
  • the cylinder portions 6 and 7 are connected to one another via a rounded transition region 19, wherein the shielding cap 4 is preferably a unipartite component.
  • the shielding cap 4 has cooling and water outlet bores 8, 9, 10 and 11.
  • a twist prevention means 12 which is in the form of a recess in the second cylinder portion 7.
  • Said recess 12 has a rectangular recess region 12A and, adjoining the latter and adjacent to the first cylinder portion 6, a conically narrowing recess region 12B.
  • the recess 12 adjoins an end-side opening 14 of the second cylinder portion 7, said opening being arranged opposite a passage recess 18 of the first cylinder portion 6, through which passage recess the shank portion 3 extends when the shielding cap 4 is in the mounted state, as can be seen in figure 1.
  • the shielding cap 4 also has a flanged portion 13 which encircles the end-side opening 14 of the second cylinder portion 7. Said flanged portion 13 is provided with recesses, of which the recesses 15, 16 and 17 are visible in figure 4. Said recesses serve for the passage of screws by which the shielding cap 4 can be fastened to the housing 2 of the actuation device 1. In principle, however, other fastening facilities are also conceivable.
  • Figures 1 and 2 also show that the actuation device 1 according to the invention is provided with a redirecting device 20.
  • Said redirecting device 20 is fixed to the fastening region 5 of the shank portion 3, for which purpose, in the example, the fastening region 5 is provided with an external thread which is not shown in detail in figure 1.
  • connection plate 23 is arranged on one end side 22 of a central part 21 of the redirecting device 20. As shown in figure 2, in the particularly preferred embodiment illustrated therein, a right angle a is enclosed between the central part 21 and the connection plate 23.
  • the redirecting device 20 has a journal plate 24 which is arranged on a longitudinal side of the central part 21. From this, it can be seen that the plane of the connection plate 23 is rotated through 90° with respect to the plane of the journal plate 24, as can be seen in detail from the illustration of figure 2. On the journal plate 24 there is arranged a journal 25 which is preferably of spherical form.
  • the journal 25 extends through a connection eyelet of one end of a coupling rod 26 in order to connect the coupling rod 26 to the actuation shank of the electric actuator 1.
  • the eyelet through which the journal 25 extends corresponds to an eyelet 29 arranged on the other end of the coupling rod 26, as can be seen in detail from the illustration of figure 1.
  • connection plate 23 to an end side 22 of the central part 21 and the arrangement, turned through 90°, of the journal plate 24 on a longitudinal side of the central part 21, a configuration of the redirecting device 20 is attained which permits a redirection of kinematic planes.
  • the journal 25 may, owing to its construction, be formed as a precision casting or bent sheet-metal part or else as an MIM part.
  • Figure 5 illustrates, as an example of a known exhaust-gas turbocharger, the turbocharger 30 which has an actuator 44 with a control rod 43.
  • Said design represents a known embodiment.
  • the exhaust-gas turbocharger 30 may however be converted into an exhaust-gas turbocharger according to the invention if the actuator 44 with its control rod 43 is exchanged for the actuation device 1 according to invention explained above in conjunction with figures 1 to 4.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

The invention relates to an actuation device (1), in particular electronic actuator, having a housing (2); having an actuation shank (3); and having a coupling rod (26) which is connected to the actuation shank (3) via a redirecting device (20).

Description

ACTUATION DEVICE, IN PARTICULAR ELECTRONIC ACTUATOR
DESCRIPTION
The invention relates to an actuation device according to claim 1 , in particular an electronic actuator.
It is an object of the present invention to provide an actuation device which makes it possible to realize a redirection of kinematic planes between the actuation shank of the actuation device and a coupling rod which is connected to the actuation shank.
This object is achieved by the features of claim 1.
The dependent claims contain advantageous developments of the invention.
Claims 11 and 12 define an exhaust-gas turbocharger according to the invention as an independently marketable product.
Further details, advantages and features of the present invention become apparent from the following description of exemplary embodiments with reference to the drawing, in which:
Figure 1 shows a perspective illustration of an actuation device according to the invention,
Figure 2 shows a detail illustration of a redirecting device,
Figure 3 shows a front view of a shielding cap,
Figure 4 shows a perspective illustration of the shielding cap as per figure
3,
Figure 5 shows a perspective sectional illustration of a known exhaust-gas turbocharger having an actuator which can be replaced with the actuation device as per figure 1 in order to convert the exhaust-gas turbocharger into a turbocharger according to invention.
Figure 1 illustrates an actuation device 1 according to the invention which, in the example, is in the form of an electronic actuator (electric actuator).
The electric actuator 1 has a housing 2 in which an actuation shank (not visible in its entirety) is guided by way of a first shank portion. The actuation shank has a second shank portion 3 which projects out of the housing 2 and which is indicated by dashed lines in figure 1. As shown in figure 1 , said second shank portion 3 is surrounded by a shielding cap 4 which is fastened, in particular screwed, to the housing 2. Here, the second shank portion 3 is, aside from a fastening region 5, covered by the shielding cap 4 in order to prevent an undesired introduction of heat into the shank portion 3.
As shown by figures 3 and 4 in conjunction with figure 1 , the shielding cap 4 has two interconnected first and second cylinder portions 6 and 7. Here, the cylinder portion 6 has a diameter Di which is smaller than the diameter D2 of the cylinder portion 7. Here, the cylinder portions 6 and 7 are connected to one another via a rounded transition region 19, wherein the shielding cap 4 is preferably a unipartite component.
As can be seen from a juxtaposition of figures 3 and 4, the shielding cap 4 has cooling and water outlet bores 8, 9, 10 and 11.
In the second cylinder portion 7, there is provided a twist prevention means 12 which is in the form of a recess in the second cylinder portion 7. Said recess 12 has a rectangular recess region 12A and, adjoining the latter and adjacent to the first cylinder portion 6, a conically narrowing recess region 12B. As can be seen from a juxtaposition of figures 3 and 4, the recess 12 adjoins an end-side opening 14 of the second cylinder portion 7, said opening being arranged opposite a passage recess 18 of the first cylinder portion 6, through which passage recess the shank portion 3 extends when the shielding cap 4 is in the mounted state, as can be seen in figure 1. The shielding cap 4 also has a flanged portion 13 which encircles the end-side opening 14 of the second cylinder portion 7. Said flanged portion 13 is provided with recesses, of which the recesses 15, 16 and 17 are visible in figure 4. Said recesses serve for the passage of screws by which the shielding cap 4 can be fastened to the housing 2 of the actuation device 1. In principle, however, other fastening facilities are also conceivable.
Figures 1 and 2 also show that the actuation device 1 according to the invention is provided with a redirecting device 20. Said redirecting device 20 is fixed to the fastening region 5 of the shank portion 3, for which purpose, in the example, the fastening region 5 is provided with an external thread which is not shown in detail in figure 1. Onto the external thread of the fastening region 5 there may be screwed two nuts 27 and 28 which, in the mounted state as shown in figure 1, engage around a connection plate 23 which is provided with a recess 26 through which the fastening region 5 can be passed, as can be seen in figure 1.
The connection plate 23 is arranged on one end side 22 of a central part 21 of the redirecting device 20. As shown in figure 2, in the particularly preferred embodiment illustrated therein, a right angle a is enclosed between the central part 21 and the connection plate 23.
Furthermore, the redirecting device 20 has a journal plate 24 which is arranged on a longitudinal side of the central part 21. From this, it can be seen that the plane of the connection plate 23 is rotated through 90° with respect to the plane of the journal plate 24, as can be seen in detail from the illustration of figure 2. On the journal plate 24 there is arranged a journal 25 which is preferably of spherical form.
As illustrated in figure 1, the journal 25 extends through a connection eyelet of one end of a coupling rod 26 in order to connect the coupling rod 26 to the actuation shank of the electric actuator 1. The eyelet through which the journal 25 extends corresponds to an eyelet 29 arranged on the other end of the coupling rod 26, as can be seen in detail from the illustration of figure 1.
By means of the arrangement, explained above, of the connection plate 23 to an end side 22 of the central part 21 and the arrangement, turned through 90°, of the journal plate 24 on a longitudinal side of the central part 21, a configuration of the redirecting device 20 is attained which permits a redirection of kinematic planes.
The journal 25 may, owing to its construction, be formed as a precision casting or bent sheet-metal part or else as an MIM part.
Figure 5 illustrates, as an example of a known exhaust-gas turbocharger, the turbocharger 30 which has an actuator 44 with a control rod 43. Said design represents a known embodiment. The exhaust-gas turbocharger 30 may however be converted into an exhaust-gas turbocharger according to the invention if the actuator 44 with its control rod 43 is exchanged for the actuation device 1 according to invention explained above in conjunction with figures 1 to 4.
The reference signs used otherwise in figure 5 are explained in the following list of reference signs, because a detailed description of the technical features indicated by said reference signs is not necessary for explaining the principles of the present invention. In addition to the above written disclosure of the invention, reference is hereby explicitly made to the illustrative presentation thereof in Figures 1 to .
LIST OF REFERENCE SIGNS
1 Actuation device (electric actuator)
2 Housing
3 Shank portion
4 Shielding cap
5 Fastening region
6, 7 First and second cylinder portion
8-1 1 Cooling and water outlet bores
12 Twist prevention means
12A Rectangular recess region
12B Conical recess region
13 Flanged portion
14 End-side opening
15-17 Recesses
18 Passage openings
19 Transition region
20 Redirecting device
21 Central part
22 End side
23 Connection plate
24 Journal plate
25 Journal
26 Coupling rod
27, 28 Nuts
29 Eyelet
30 Exhaust-gas turbocharger
31 Turbine housing
32 Compressor housing
33 Bearing housing
34 Turbine wheel
35 Shaft
36 Compressor wheel
37 Turbine housing inlet Turbine housing outlet
Flap arrangement
Flap plate
Flap lever/spindle
Flap shaft
Control rod
Actuator
Right angle

Claims

1. An actuation device (1), in particular electronic actuator,
having a housing (2);
having an actuation shank (3); and
having a coupling rod (26) which is connected to the actuation shank (3) via a redirecting device (20).
2. The actuation device as claimed in claim I, wherein the redirecting device (20) has a central part (21), on one end side (22) of which is arranged a connection plate (23).
3. The actuation device as claimed in claim 2, wherein the connection plate (23) is arranged at a right angle (a) with respect to the central part (21).
4. The actuation device as claimed in claim 2 or 3, wherein the connection plate (23) is formed with a retaining recess (26).
5. The actuation device as claimed in one of claims 2 to 4, wherein the central part (21) is of plate-shaped form.
6. The actuation device as claimed in one of claims 2 to 5, wherein a journal plate (24) is arranged on one longitudinal side of the central part (21). 7. The actuation device as claimed in claim 6, wherein the journal plate
(24) is provided with a journal (25).
8 The actuation device as claimed in claim 7, wherein the journal (25) is of spherical form.
9. The actuation device as claimed in one of claims 1 to 8, wherein the redirecting device (20) is formed as a unipartite component.
10. The actuation device as claimed in one of claims 7 to 9, wherein the journal (25) is formed as a precision casting, bent sheet-metal component or MIM component.
11. An exhaust-gas turbocharger (30) having an actuation device (1) which has a housing (2), an actuation shaft (3) and a coupling rod (26) which is connected to the actuation shank (3) via a redirecting device (20).
12. The exhaust-gas turbocharger as claimed in claim 11, characterized by at least one of the features of claims 2 to 10.
PCT/US2013/059181 2012-09-19 2013-09-11 Actuation device, in particular electronic actuator WO2014046933A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012018531.6 2012-09-19
DE102012018531 2012-09-19

Publications (1)

Publication Number Publication Date
WO2014046933A1 true WO2014046933A1 (en) 2014-03-27

Family

ID=50341862

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/059181 WO2014046933A1 (en) 2012-09-19 2013-09-11 Actuation device, in particular electronic actuator

Country Status (1)

Country Link
WO (1) WO2014046933A1 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040128996A1 (en) * 2002-07-31 2004-07-08 Siemens Aktiengesellschaft Method for determining a boost pressure setpoint in an internal combustion engine with an exhaust gas turbocharger
KR20070076772A (en) * 2006-01-20 2007-07-25 민복기 Separate diaphragm actuator for turbocharged waste gate valve
US20070209363A1 (en) * 2001-05-11 2007-09-13 Mcewen James A Turbocharger with wastegate
US20090183507A1 (en) * 2008-01-17 2009-07-23 Corey Weaver Turbocharger waste gate control
KR20120067475A (en) * 2010-12-16 2012-06-26 주식회사 만도 Electric waste gate actuator operated for turbocharger

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070209363A1 (en) * 2001-05-11 2007-09-13 Mcewen James A Turbocharger with wastegate
US20040128996A1 (en) * 2002-07-31 2004-07-08 Siemens Aktiengesellschaft Method for determining a boost pressure setpoint in an internal combustion engine with an exhaust gas turbocharger
KR20070076772A (en) * 2006-01-20 2007-07-25 민복기 Separate diaphragm actuator for turbocharged waste gate valve
US20090183507A1 (en) * 2008-01-17 2009-07-23 Corey Weaver Turbocharger waste gate control
KR20120067475A (en) * 2010-12-16 2012-06-26 주식회사 만도 Electric waste gate actuator operated for turbocharger

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