The present invention relates to suspension systems for vehicles of the like. More particularly, the present invention relates to a semi-active anti-roll system that controls the roll of the vehicle during maneuvering such as when rounding a corner.
The statements in this section merely provide background information related to the present disclosure and may not constitute prior art.
Suspension systems are provided to filter or isolate the vehicle's body (sprung portion) from the vehicle's wheels and axles (unsprung portion) when the vehicle travels over vertical road surface irregularities as well as to control body and wheel motion. In addition, suspension systems are also used to maintain an average vehicle attitude to promote improved stability of the vehicle during maneuvering. The typical passive suspension system includes a spring and a damping device in parallel which are located between the sprung portion and the unsprung portion of the vehicle.
Hydraulic actuators, such as shock absorbers and/or struts, are used in conjunction with conventional passive suspension systems to absorb unwanted vibration which occurs during driving. To absorb this unwanted vibration, hydraulic actuators include a piston located within a pressure cylinder of the hydraulic actuator. The piston is connected to the sprung portion or body of the vehicle through a piston rod. Because the piston is able to restrict the flow of damping fluid within the working chamber of the hydraulic actuator when the piston is displaced within the pressure cylinder, the hydraulic actuator is able to produce a damping force which counteracts the vibration of the suspension. The greater the degree to which the damping fluid within the working chamber is restricted by the piston, the greater the damping forces which are generated by the hydraulic actuator.
In recent years, substantial interest has grown in automotive vehicle suspension systems which can offer improved comfort and road handling over the conventional passive suspension systems. In general, such improvements are achieved by utilization of an “intelligent” suspension system capable of electronically controlling the suspension forces generated by hydraulic actuators.
Different levels in achieving the ideal “intelligent” suspension system called a semi-active or a fully active suspension system are possible. Some systems control and generate damping forces based upon the dynamic forces acting against the movement of the piston. Other systems control and generate damping forces based on the static or slowly changing dynamic forces, acting on the piston independent of the velocity of the piston in the pressure tube. Other, more elaborate systems, can generate variable damping forces during rebound and compression movements of the hydraulic actuator regardless of the position and movement of the piston in the pressure tube.
In addition to controlling the damping forces generated in the hydraulic actuators using a semi-active or fully active suspension system, it would be advantageous to add an anti-roll function to the suspension system by inter-connecting the right and left corners of the vehicle.
A suspension system combines the advantages of a semi-active damper system and an active anti-roll system. The two front hydraulic actuators and the two rear hydraulic actuators are each mechanically interconnected using fluid lines. The front and rear hydraulic actuators are not mechanically interconnected. Instead of using fluid lines between the front and rear hydraulic actuators, an electronic connection through the electronic controller links the front and rear suspensions.
Further areas of applicability will become apparent from the description provided herein. It should be understood that the description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.
The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. There is shown in
Referring to
Each pressure tube 30a-30d defines a working chamber 42a-42d. Each piston 32a-32d is slidably disposed within a respective pressure tube 30a-30d and divides the respective working chamber 42a-42d into an upper working chamber 44a-44d and a lower working chamber 46a-46d. Piston 32a-32d undergoes sliding movement with respect to pressure tube 30a-30d without generating undue frictional forces and piston 32a-32d seals upper working chamber 44a-44d from lower working-chamber 46a-46d. Each piston rod 34a-34d is attached to a respective piston 32a-32d and extends through upper working chamber 44a-44d and through an upper end cap or rod guide 48a-48d which closes the upper end of pressure tube 30a-30d. A sealing system seals the interface between rod guide 42a-48d, pressure tube 30a-30d and piston rod 34a-34d. The end of piston rod 34a-34d opposite to piston 32a-32d is adapted to be secured to the sprung portion of vehicle 10. The end of pressure tube 30a-30d opposite to rod guide 48a-48d is adapted to be connected to the unsprung portion of vehicle 10.
In communication with upper working chamber 44a-44d is a first check valve 50a-50d, a second check valve 52a-52d and an electronically controlled variable valve 54a-54d. First check valve 50a-50d prohibits fluid flow from upper working chamber 44a-44d but allows fluid flow into upper working chamber 44a-44d. Second check valve 52a-52d allows fluid flow from upper working chamber 44a-44d but prohibits fluid flow into upper working chamber 44a-44d. Electronically controlled variably valve 54a-54d controls fluid flow as described below.
In communication with lower working chamber 46a-46d is a first check valve 60a-60d, a second check valve 62a-62d and an electronically controlled variable valve 64a-64d. First check valve 60a-60d prohibits fluid flow from lower working chamber 46a-46d but allows fluid flow into lower working chamber 46a-46d. Second check valve 62a-62d allows fluid flow from lower working chamber 46a-46d but prohibits fluid flow into lower working chamber 46a-46d. Electronically controlled-variable valve 64a-64d controls fluid flow as described below. An accumulator 66a-66d is in communication with working chamber 42a-42d as detailed below.
A first interconnecting fluid line 70 and a second interconnecting fluid line 72 allow working chambers 42aand 42b of actuators 26 to communicate with each other as described below. A third interconnecting fluid line 74 and a fourth interconnecting line 76 allow working chambers 42c and 42d of rear actuators 20 to communicate with each other as described below. An electronic control unit 78 is in communication with electronically controlled variable valves 54a-54d, in communication with electronically controlled variable valves 64a-64d and in communication with the sensors at each wheel 18 and each wheel 24 which senses the position and/or the velocity and/or the acceleration of body 16 with respect to rear suspension 12 and front suspension 14.
The construction of rear suspension 12 and front suspension 14 is basically the same. There is no mechanical connection between front and rear suspensions 12 and 14, there is only an electrical connection through electronic control unit 78. As detailed above, the suspension system comprises four actuators (two rear actuators 20 and two front actuators 26); four accumulators 66a-66d; eight electronically controlled variable valves 54a-54d and 64a-64d; sixteen check valves 50a-50d, 52a-52d, 60a-60d and 62a-62d; and four interconnecting lines 72-78. The working principle of the suspension system will now be described in four operating modes; bounce input, single wheel input, roll input and articulation input.
In a pure bounce mode, all four wheels are going to move synchronously. The fluid flows for each corner of vehicle 10 will be the same. The working principle for front left actuators 26 will be described. It is to be understood that the fluid flow in right front actuator 26 and left and right rear actuators 20 will be the same as that described below for left front actuator 26.
When left front actuator 26 is compressed, fluid is pushed out of lower working chamber 46a and through check valve 62a. The rod volume portion of the fluid flow is pushed through electronically controlled variable valve 64a into accumulator 66a. The other part of the fluid flow is pushed through electronically controlled variable valve 54a, through check valve 50a and into upper working chamber 44a. The damping forces are controlled by controlling electronic controlled variable valves 54aand 64ausing electronic control unit 78.
When left front actuator 26 is extended or rebounds, fluid is pushed out of upper working chamber 44a, through check valve 52a, through electronically controlled variable valve 64a, through check valve 60a and into lower working chamber 46a. A rod volume of fluid flow flows out of accumulator 66a through check valve 60a into lower working chamber 46a. The damping forces are controlled by controlling electronically controlled variable valve 64ausing electronic control unit 78.
As discussed-above, the three remaining actuators 26, 20 and 20 have the same working principle and fluid flows in bounce as described above.
In the case of a single wheel input, there are two options. These two options will be described in relation to a single wheel input to left front actuator 26. It is to be understood that the two options and the fluid flow described below for front left actuator 26 are the same for front right actuator 26 and for left and right actuators 20.
The first option is to have full single wheel stiffness. In this option, electronically controlled variable valves 54b and 64b should be closed by electronic control unit 78 so that it isn't possible for fluid flow to occur in right front actuator 26. The fluid flow for left front actuator 26 occurs as follows. When left front actuator 26 is compressed, fluid is pushed out of lower working chamber 46a and through check valve 62a. The rod volume portion of the fluid flow is pushed through electronically controlled variable valve 64a into accumulator 66a. The other part of the fluid flow is pushed through electronically controlled variable valve 54a, through check valve 50a and into upper working chamber 44a. The damping forces are controlled by controlling electronic controlled variable valves 54a and 64a using electronic control unit 78.
When left front actuator 26 is extended or rebounds, fluid is pushed out of upper working chamber 44a, through check valve 52a, through electronically controlled variable valve 64a, through check valve 60a and into lower working chamber 46a. A rod volume of fluid flow flows out of accumulator 66athrough check valve 60a into lower working chamber 46a. The damping forces are controlled by controlling electronically controlled variable valve 64a using electronic control unit 78.
As discussed above, the three remaining actuators 26, 20 and 20 have the same working principle and fluid flows as described above.
The second option is to have reduced single wheel stiffness which can provide increased comfort. In this option, electronically controlled variable valves 54b and 64b should be opened by electronic control unit 78. When actuator 26 is compressed, fluid is pushed out of lower working chamber 46a and through check valve 62a. Part of the rod volume fluid flow is pushed through electronically controlled variable valve 64a and into accumulator 66a. The other part of the rod volume portion of the fluid flow is pushed through electronically controlled variable valve 64a through interconnecting line 70, through check valve 50b and into upper working chamber 44b of right front actuator 26. This fluid flow pushes piston 32b downward where fluid flow is pushed from lower working chamber 46b of right front actuator 26 through check valve 62b, through electronically controlled variable valve 64b into accumulator 66b. The other part of the fluid flow is pushed through electronically controlled variable valve 54a, through check valve 50a and into upper working chamber 44a. The damping forces are controlled by controlling electronically controlled variable valves 54a and 64a using electronic control unit 78.
When left front actuator 26 is extended or rebounds, fluid is pushed out of upper working chamber 44a, through check valve 52a, through electronically controlled variable valve 64a, through check valve 60a and into lower working chamber 46a. A part of the rod volume of fluid flows out of accumulator 66a through check valve 60a into lower working chamber 46a. The other part of the rod volume flows from upper working chamber 44b of right front actuator 26 through check valve 52b, through electronically controlled variable valve 54b, through interconnecting line 70, through check valve 60a into lower working chamber 46a. This fluid flow causes piston 32b to move upward where fluid flow is replaced in lower working chamber 46b from accumulator 66b through check valve 60b. The damping forces are controlled by controlling electronically controlled variable valve 64a using electronic control unit 78.
This second option provides less total single wheel stiffness. As discussed above, the three remaining actuators 26, 20 and 20 have the same working principle and fluid flow as described above.
In the roll mode, it is desired to have as high as possible stiffness for the suspension system. A typical roll motion is when the front and rear left wheel go into compression and the front and rear right wheel go into extension or rebound. The opposite roll motion is when the front and rear left wheel go into extension or rebound and the front and rear right wheel go into compression. When vehicle 10 is in a roll mode, the axis between the front wheels and the axis between the rear wheel roll in the same direction. The fluid flow will be described using the front wheels of vehicle 10. It is to be understood that the rear wheels of vehicle 10 react in the same manner and have the same fluid flow. Also, the following description is for a left-hand roll where the left wheel goes into compression and the right wheel goes into rebound or extension. It is to be understood that the fluid flow for an opposite right hand roll is the same but opposite in direction.
During a left hand roll, electronically controlled variable valves 54a and 64b are closed. The fluid from lower working chamber 46a of front left actuator 26 is pushed through check valve 62a, through electronically controlled variable valve 64aand into accumulator 66a. The fluid from upper working chamber 44b of right front actuator 26 is pushed through check valve 52b, through electronically controlled variable valve 54b, through interconnecting line 70 and into accumulator 66a. The fluid that is flowing into upper working chamber 44a of left front actuator 26 is flowing out of accumulator 66b, through interconnecting line 72, through check valve 50a and into upper working chamber 44a. The fluid flow flowing into lower working chamber 46b of right hand actuator 26 is flowing out of accumulator 66b, through check valve 60b and into lower working chamber 46b. The roll damping is controlled by controlling the fluid flow through electronically controlled variable valves 64a and 54b by electronic control unit 78.
As discussed above, the fluid flow between left rear and right rear actuators 20 is the same as that described above for left front and right front actuators 26. Also, for a roll in the opposite direction, the fluid flow between left front and right front actuators 26 and the fluid flow between left rear and right rear actuators 20 are in the opposite direction to that described above.
In the case of articulation, the axis between the two front wheels and the axis between the two rear wheels are rolled in opposite directions. In this situation, it is desirable to have as less as possible stiffness. For exemplary description, the following discussion is based upon the left front actuator 26 going into compression, the right front actuator 26 going into rebound, the left rear actuator 20 going into rebound and the right rear actuator 20 going into compression. It is to be understood that the fluid flow is the same but opposite in direction when articulation occurs in the opposite direction.
During the described articulation movement, for the left and right front corners, electronically controlled variable valves 64aand 54b are closed. The fluid is pushed from lower working chamber 46a of left front actuator 26, through check valve 62a and through electronically controlled variable valve 54a. Part of the fluid flows through check valve 50a and into upper working chamber 44a of left front actuator 26. The rod volume flow of fluid flows through interconnecting line 72, through check valve 60b and into lower working chamber 46b of right front actuator 26. The fluid pushed out of upper working chamber 44b of right front actuator 26 is pushed through check valve 52b, through electronically controlled variable valve 64b, through check valve 60b, and into lower working chamber 46b of right front actuator 26. There is no flow to or from accumulators 66a and 66b and thus no additional stiffness built up. The damping characteristics are controlled by controlling the fluid flow through electronically controlled variable valves 54a and 64b by electronic control unit 78.
During the described articulation movement, for the left and right rear corners, electronically controlled variable valves 54c and 64d are closed. The fluid is pushed from lower working chamber, 46d of right front actuator 20, through check valve 62d and through electronically controlled variable valve 54d. Part of the fluid flows through check valve 50d into upper working chamber 44d of right rear actuator 20. The rod volume flow of fluid flows through interconnecting line 74, through check valve 60c and into lower working chamber 46c of left rear actuator 20. The fluid pushed out of upper working chamber 44c of left rear actuator 20 is pushed through check valve 52c, through electronically controlled variable valve 64c, through check valve 60c and into lower working chamber 46c of left rear actuator 20. There is no flow to or from accumulators 66a and 66b and thus no additional stiffness built up. The damping characteristics are controlled by controlling the fluid flow through electronically controlled variable valves 54d and 64c by electronic control unit 78.
A typical pitch motion is when the front left and right wheels go into compression and the rear left and right wheels go into extension or rebound. The opposite pitch motion is when the front left and right wheels go into extension or rebound and the rear left and right wheels go into compression.
During pitch motion, front left and right actuators are controlled the same as that described above for the bounce mode except that instead of all four wheels moving in the same direction, the front wheels move in a direction opposite to the rear wheels. The fluid flow will be the same as that described above for the bounce mode except that the front actuators 26 will move in compression when the rear actuators 20 move in extension or rebound and the front actuators 26 will move in extension or rebound when the rear actuators 20 move in compression.
The above described suspension system offers the ability to control electronically by electronic control unit 78 all of the damping characteristics similar to a semi-active damper system but, the above described suspension system can also control single wheel input, vehicle roll movement, articulation movement and pitch movement. The above described suspension system eliminates mechanical decoupling of the roll, articulation and pitch modes and uses only an electronically decoupling using electronic control unit 78.
This application claims the benefit of U.S. Provisional Application No. 60/692,433, filed on Jun. 21, 2005. The disclosure of the above application is incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
3895816 | Takahashi et al. | Jul 1975 | A |
3941403 | Hiruma | Mar 1976 | A |
4277076 | Hanna | Jul 1981 | A |
4293139 | Brown | Oct 1981 | A |
4335901 | Gladish | Jun 1982 | A |
4390188 | Rouse | Jun 1983 | A |
4397477 | Harrison | Aug 1983 | A |
4404892 | Nakamura et al. | Sep 1983 | A |
4469315 | Nicholls et al. | Sep 1984 | A |
4566718 | Kanai et al. | Jan 1986 | A |
4573705 | Kanai et al. | Mar 1986 | A |
4595072 | Barnea | Jun 1986 | A |
4621833 | Soltis | Nov 1986 | A |
4625993 | Williams et al. | Dec 1986 | A |
4722545 | Gretz et al. | Feb 1988 | A |
4743046 | Schnittger | May 1988 | A |
4761022 | Ohashi et al. | Aug 1988 | A |
4828229 | Fannin et al. | May 1989 | A |
4848791 | Bridges | Jul 1989 | A |
4867466 | Soltis | Sep 1989 | A |
4999776 | Soltis et al. | Mar 1991 | A |
5020826 | Stecklein et al. | Jun 1991 | A |
5097419 | Lizell | Mar 1992 | A |
5098119 | Williams et al. | Mar 1992 | A |
5130926 | Watanabe et al. | Jul 1992 | A |
5188390 | Clark | Feb 1993 | A |
5218546 | Bradshaw et al. | Jun 1993 | A |
5230529 | Harvey-Bailey | Jul 1993 | A |
5231583 | Lizell | Jul 1993 | A |
5258913 | Baldauf | Nov 1993 | A |
5265704 | Landesfeind | Nov 1993 | A |
5265913 | Scheffel | Nov 1993 | A |
5338010 | Haupt | Aug 1994 | A |
5351790 | Machida | Oct 1994 | A |
5434782 | Henry | Jul 1995 | A |
5483448 | Liubakka et al. | Jan 1996 | A |
5490068 | Shimizu et al. | Feb 1996 | A |
5510985 | Yamaoka et al. | Apr 1996 | A |
5517847 | Campbell et al. | May 1996 | A |
5521821 | Shimizu et al. | May 1996 | A |
5539639 | Devaud et al. | Jul 1996 | A |
5556115 | Heyring | Sep 1996 | A |
5559700 | Majeed et al. | Sep 1996 | A |
5563789 | Otterbein et al. | Oct 1996 | A |
5570288 | Badenoch et al. | Oct 1996 | A |
5572425 | Levitt et al. | Nov 1996 | A |
5584498 | Danek | Dec 1996 | A |
5601306 | Heyring | Feb 1997 | A |
5606503 | Shal et al. | Feb 1997 | A |
5682968 | Boichot et al. | Nov 1997 | A |
5682980 | Reybrouck | Nov 1997 | A |
5692587 | Fratini, Jr. | Dec 1997 | A |
5706196 | Romstadt | Jan 1998 | A |
5721681 | Borschert et al. | Feb 1998 | A |
5725239 | de Molina | Mar 1998 | A |
5794966 | MacLeod | Aug 1998 | A |
5808890 | Sasaki | Sep 1998 | A |
5882017 | Carleer | Mar 1999 | A |
5897130 | Majeed et al. | Apr 1999 | A |
6076837 | Kokotovic | Jun 2000 | A |
6129368 | Ishikawa | Oct 2000 | A |
6220406 | de Molina et al. | Apr 2001 | B1 |
6244398 | Girvin et al. | Jun 2001 | B1 |
6259982 | Williams et al. | Jul 2001 | B1 |
6264212 | Timoney | Jul 2001 | B1 |
6279854 | Lindahl | Aug 2001 | B1 |
6283483 | Johnson et al. | Sep 2001 | B1 |
6298292 | Shono et al. | Oct 2001 | B1 |
6502837 | Hamilton et al. | Jan 2003 | B1 |
6598885 | Delorenzis et al. | Jul 2003 | B2 |
6679504 | Delorenzis et al. | Jan 2004 | B2 |
6789017 | Aanen et al. | Sep 2004 | B2 |
6811167 | Coombs et al. | Nov 2004 | B2 |
6814364 | Coombs et al. | Nov 2004 | B2 |
6816799 | Yu et al. | Nov 2004 | B2 |
6871866 | Gloceri et al. | Mar 2005 | B2 |
6886837 | Gibbs | May 2005 | B2 |
6886841 | Coombs et al. | May 2005 | B2 |
6932367 | Radamis | Aug 2005 | B2 |
7055831 | Brandenburger | Jun 2006 | B2 |
7055832 | Germain | Jun 2006 | B2 |
7076351 | Hamilton et al. | Jul 2006 | B2 |
7360777 | Mizuno et al. | Apr 2008 | B2 |
7413063 | Davis | Aug 2008 | B1 |
7637516 | Mizuno et al. | Dec 2009 | B2 |
7641181 | Delorenzis | Jan 2010 | B2 |
20040094929 | Ribi | May 2004 | A1 |
20040113377 | Klees | Jun 2004 | A1 |
20050240326 | Lauwerys et al. | Oct 2005 | A1 |
20060151964 | Kasamatsu | Jul 2006 | A1 |
20070045067 | Schedgick et al. | Mar 2007 | A1 |
Number | Date | Country |
---|---|---|
1 238834 | Feb 2002 | EP |
2243349 | Apr 1991 | GB |
2337730 | Mar 1998 | GB |
504473 | Oct 2002 | TW |
WO 9523076 | Feb 1995 | WO |
Number | Date | Country | |
---|---|---|---|
20060287791 A1 | Dec 2006 | US |
Number | Date | Country | |
---|---|---|---|
60692433 | Jun 2005 | US |