Computer controlled hydraulic bleed sequence

• US 10,299,423 B2
• Filed: 01/06/2017
• Issued: 05/28/2019
• Est. Priority Date: 12/11/2013
• Status: Active Grant

• Current Assignee: CNH Industrial Canada, Ltd (CNH Industrial N.V.)
• Original Assignee: CNH Industrial Canada, Ltd (CNH Industrial N.V.)
• Inventors: Sudbrink, Matthew R., Shah, Kena, Knobloch, Dean A., Henry, James W.
• Primary Examiner(s): Troutman, Matthew
• Application Number:
  US15/400,778
• Publication Number:
  US 20170112046A1
• Time in Patent Office: 872 Days
• CPC Class Codes: A01B 49/027 with a rotating, soil working support element, e.g. a roller
• CPC Class Codes: A01B 59/002 Details, component parts
• CPC Class Codes: A01B 63/32 operated by hydraulic or pneumatic means without automatic control
• CPC Class Codes: A01B 73/02 Folding frames
• CPC Class Codes: A01B 73/048 the axis being oriented in transverse direction A01B73/042 takes precedence
• CPC Class Codes: A01B 73/065 to a position essentially forward of the axis, in relation to the direction of travel
• CPC Class Codes: F01B 1/01 with one single cylinder
• CPC Class Codes: F01B 25/02 Regulating or controlling by varying working-fluid admission or exhaust, e.g. by varying pressure or quantity distributing or expansion valve gear F01L
• CPC Class Codes: F01B 31/28 Cylinders or cylinder covers

Abstract

An agricultural machine or implement has a main frame section and at least one wing section, each having lift cylinders. A main shank frame may be pivotally attached to the main frame section and may have hydraulically adjustable gauge wheels. Wing shank frames may be pivotally attached to the wing sections and may also have hydraulically adjustable gauge wheels. Bypass circuits may be used to individually adjust the lift cylinders and gauge wheel cylinders. A controller or controllers is used to purge air from the lift cylinders, gauge wheel cylinders, cylinders used to raise the shank frames for transport, and from the bypass circuits. The purge routine may be selectable as individual steps, hydraulic subsystem purges, or as one automatic purge routine.

Claims

1. An agricultural machine or implement, comprising:

a main frame section;

at least one wing section;

at least one first hydraulic subsystem including at least one main frame lift hydraulic cylinder for raising and lowering said main frame section, at least one wing section lift hydraulic cylinder for raising and lowering said at least one wing section, and at least one first bypass circuit bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

at least one controller operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main frame lift hydraulic cylinder, said at least one wing section lift hydraulic cylinder, and said at least one first bypass circuit, said at least one controller configured to bleed air from said at least one first hydraulic subsystem using the steps of;

first, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

second, retracting said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

third, bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder while extending at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder; and

fourth, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder.

2. The agricultural machine or implement of claim 1, wherein:

said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder each being provided with at least one re-phasing port;

said first step further including extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure; and

said fourth step further including extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure.

3. The agricultural machine or implement of claim 2, further comprising:

at least one main structure pivotally connected to said main frame section;

at least one wing structure pivotally connected to said at least one wing section;

at least one second hydraulic subsystem including at least one main structure gauge lift hydraulic cylinder for at least partially raising and lowering said at least one main structure, at least one wing structure gauge lift hydraulic cylinder for at least partially raising and lowering said at least one wing structure, and at least one second bypass circuit bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder, each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder being provided with at least one re-phasing port;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main structure gauge lift hydraulic cylinder, said at least one wing structure gauge lift hydraulic cylinder, and said at least one second bypass circuit, said at least one controller configured to bleed air from said at least one second hydraulic subsystem using the steps of;

first, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure;

second, retracting said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder;

third, bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder while extending at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder; and

fourth, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure.

4. The agricultural machine or implement of claim 3, wherein:

said at least one wing section lift hydraulic cylinder further comprises at least two wing section lift hydraulic cylinders; and

said third step of bleeding air from said first hydraulic subsystem further includes first bypassing said at least one main frame lift hydraulic cylinder, then bypassing said at least one main frame lift hydraulic cylinder and sequentially bypassing additional wing section lift hydraulic cylinders until each wing section lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing section lift hydraulic cylinders.

5. The agricultural machine or implement of claim 4, wherein:

said at least one wing structure gauge lift hydraulic cylinder further comprises at least two wing structure gauge lift hydraulic cylinders; and

said third step of bleeding air from said second hydraulic subsystem further includes first bypassing said at least one main structure gauge lift hydraulic cylinder, then bypassing said at least one main structure gauge lift hydraulic cylinder and sequentially bypassing additional wing structure gauge lift hydraulic cylinders until each wing structure gauge lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing structure gauge lift hydraulic cylinders.

6. The agricultural machine or implement of claim 5, further comprising:

at least one third hydraulic subsystem including at least one main structure fold hydraulic cylinder for folding said at least one main structure over said main frame section, and at least one wing structure fold hydraulic cylinder for folding said at least one wing structure against said at least one wing section;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main structure fold hydraulic cylinder and said at least one wing structure fold hydraulic cylinder, said at least one controller configured to bleed air from said at least one third hydraulic subsystem using the steps of;

first, folding said at least one main structure over said main frame section using said at least one main structure fold hydraulic cylinder;

second, folding said at least one wing structure against said at least one wing section using said at least one wing structure fold hydraulic cylinder;

third, unfolding said at least one wing structure from against said at least one wing section using said at least one wing structure fold hydraulic cylinder; and

fourth, unfolding said at least one main structure from over said main frame section using said at least one main structure fold hydraulic cylinder.

7. The agricultural machine or implement of claim 6, further comprising:

at least one of a hitch lock, a pull hitch capable of being raised and lowered, a diagonally angled draft tube and pivoting swing arm assembly, and at least one wing section pivotally connected to said main frame section;

at least one fourth hydraulic subsystem including at least one of a hitch lock cylinder connected to said hitch lock, a pull hitch hydraulic cylinder connected to said pull hitch capable of being raised and lowered, at least one pivoting swing arm hydraulic cylinder connected to said diagonally angled draft tube and pivoting swing arm assembly, and at least one main fold hydraulic cylinder connected to said at least one wing section pivotally connected to said main frame section;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said hitch lock cylinder, said pull hitch hydraulic cylinder, said at least one pivoting swing arm hydraulic cylinder, and said at least one main fold hydraulic cylinder, said at least one controller configured to bleed air from said at least one fourth hydraulic subsystem using the steps of;

first, releasing said hitch lock using said hitch lock cylinder;

second, raising said pull hitch using said pull hitch hydraulic cylinder;

third, pivoting inwards said diagonally angled draft tube and pivoting swing arm assembly using said at least one pivoting swing arm hydraulic cylinder;

fourth, folding inwards said at least one pivotally connected wing section against said main frame section using said at least one main fold hydraulic cylinder;

fifth, unfolding outwards said at least one pivotally connected wing section from against said main frame section using said at least one main fold hydraulic cylinder;

sixth, pivoting outwards said diagonally angled draft tube and pivoting swing arm assembly using said at least one pivoting swing arm hydraulic cylinder;

seventh, lowering said pull hitch using said pull hitch hydraulic cylinder; and

eighth, latching said hitch lock using said hitch lock cylinder.

8. The agricultural machine or implement of claim 6, wherein:

said at least one controller being further configured to receive operator input authorizing one of;

each of said first, second, third, and fourth steps of bleeding air from said at least one first hydraulic subsystem, each of said first, second, third, and fourth steps of bleeding air from said at least one second hydraulic subsystem, and each of said first, second, third, and fourth steps of bleeding air from said at least one third hydraulic subsystem, individually;

each of bleeding air from said at least one first hydraulic subsystem, bleeding air from said at least one second hydraulic subsystem, and bleeding air from said at least one third hydraulic subsystem, separately; and

bleeding air from said at least one first hydraulic subsystem, said at least one second hydraulic subsystem, and said at least one third hydraulic subsystem, automatically.

9. A hydraulic system of an agricultural machine or implement having a main frame section, at least one wing section, at least one main structure pivotally connected to the main frame section, and at least one wing structure pivotally connected to the at least one wing section, comprising:

at least one first hydraulic subsystem including at least one main frame lift hydraulic cylinder for raising and lowering the main frame section, at least one wing section lift hydraulic cylinder for raising and lowering the at least one wing section, and at least one first bypass circuit bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

at least one controller operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main frame lift hydraulic cylinder, said at least one wing section lift hydraulic cylinder, and said at least one first bypass circuit, said at least one controller configured to bleed air from said at least one first hydraulic subsystem using the steps of;

first, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

second, retracting said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

third, bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder while extending at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder; and

fourth, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder.

10. The hydraulic system of claim 9, wherein:

said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder each being provided with at least one re-phasing port;

said first step further including extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure; and

said fourth step further including extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure.

11. The hydraulic system of claim 10, further comprising:

at least one second hydraulic subsystem including at least one main structure gauge lift hydraulic cylinder for at least partially raising and lowering the at least one main structure, at least one wing structure gauge lift hydraulic cylinder for at least partially raising and lowering the at least one wing structure, and at least one second bypass circuit bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder, each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder being provided with at least one re-phasing port;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main structure gauge lift hydraulic cylinder, said at least one wing structure gauge lift hydraulic cylinder, and said at least one second bypass circuit, said at least one controller configured to bleed air from said at least one second hydraulic subsystem using the steps of;

first, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure;

second, retracting said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder;

third, bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder while extending at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder; and

fourth, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure.

12. The hydraulic system of claim 11, wherein:

said at least one wing section lift hydraulic cylinder further comprises at least two wing section lift hydraulic cylinders; and

said third step of bleeding air from said first hydraulic subsystem further includes first bypassing said at least one main frame lift hydraulic cylinder, then bypassing said at least one main frame lift hydraulic cylinder and sequentially bypassing additional wing section lift hydraulic cylinders until each wing section lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing section lift hydraulic cylinders.

13. The hydraulic system of claim 12, wherein:

said at least one wing structure gauge lift hydraulic cylinder further comprises at least two wing structure gauge lift hydraulic cylinders; and

said third step of bleeding air from said second hydraulic subsystem further includes first bypassing said at least one main structure gauge lift hydraulic cylinder, then bypassing said at least one main structure gauge lift hydraulic cylinder and sequentially bypassing additional wing structure gauge lift hydraulic cylinders until each wing structure gauge lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing structure gauge lift hydraulic cylinders.

14. The hydraulic system of claim 13, further comprising:

at least one third hydraulic subsystem including at least one main structure fold hydraulic cylinder for folding the at least one main structure over the main frame section, and at least one wing structure fold hydraulic cylinder for folding the at least one wing structure against the at least one wing section;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said at least one main structure fold hydraulic cylinder and said at least one wing structure fold hydraulic cylinder, said at least one controller configured to bleed air from said at least one third hydraulic subsystem using the steps of;

first, folding the at least one main structure over the main frame section using said at least one main structure fold hydraulic cylinder;

second, folding the at least one wing structure against the at least one wing section using said at least one wing structure fold hydraulic cylinder;

third, unfolding the at least one wing structure from against the at least one wing section using said at least one wing structure fold hydraulic cylinder; and

fourth, unfolding the at least one main structure from over the main frame section using said at least one main structure fold hydraulic cylinder.

15. The hydraulic system of claim 14, further comprising:

at least one fourth hydraulic subsystem including at least one of a hitch lock cylinder connected to a hitch lock of the agricultural machine or implement, a pull hitch hydraulic cylinder connected to a pull hitch of the agricultural machine or implement capable of being raised and lowered, at least one pivoting swing arm hydraulic cylinder connected to a diagonally angled draft tube and pivoting swing arm assembly of the agricultural machine or implement, and at least one main fold hydraulic cylinder connected to at least one wing section that is pivotally connected to the main frame section of the agricultural machine or implement;

said at least one controller being operably connected to at least one valve controlling hydraulic flow to at least one of said hitch lock cylinder, said pull hitch hydraulic cylinder, said at least one pivoting swing arm hydraulic cylinder, and said at least one main fold hydraulic cylinder, said at least one controller configured to bleed air from said at least one fourth hydraulic subsystem using the steps of;

first, releasing said hitch lock using said hitch lock cylinder;

second, raising said pull hitch using said pull hitch hydraulic cylinder;

third, pivoting inwards said diagonally angled draft tube and pivoting swing arm assembly using said at least one pivoting swing arm hydraulic cylinder;

fourth, folding inwards said at least one pivotally connected wing section against said main frame section using said at least one main fold hydraulic cylinder;

fifth, unfolding outwards said at least one pivotally connected wing section from against said main frame section using said at least one main fold hydraulic cylinder;

sixth, pivoting outwards said diagonally angled draft tube and pivoting swing arm assembly using said at least one pivoting swing arm hydraulic cylinder;

seventh, lowering said pull hitch using said pull hitch hydraulic cylinder; and

eighth, latching said hitch lock using said hitch lock cylinder.

16. The hydraulic system of claim 14, wherein:

said at least one controller being further configured to receive operator input authorizing one of;

each of said first, second, third, and fourth steps of bleeding air from said at least one first hydraulic subsystem, each of said first, second, third, and fourth steps of bleeding air from said at least one second hydraulic subsystem, and each of said first, second, third, and fourth steps of bleeding air from said at least one third hydraulic subsystem, individually;

each of bleeding air from said at least one first hydraulic subsystem, bleeding air from said at least one second hydraulic subsystem, and bleeding air from said at least one third hydraulic subsystem, separately; and

bleeding air from said at least one first hydraulic subsystem, said at least one second hydraulic subsystem, and said at least one third hydraulic subsystem, automatically.

17. A method of bleeding air from a hydraulic system of an agricultural machine or implement having a main frame section, at least one wing section, at least one main structure pivotally connected to the main frame section, and at least one wing structure pivotally connected to the at least one wing section, comprising the steps of:

providing at least one first hydraulic subsystem including at least one main frame lift hydraulic cylinder for raising and lowering the main frame section, at least one wing section lift hydraulic cylinder for raising and lowering the at least one wing section, and at least one first bypass circuit bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

providing each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder with at least one re-phasing port;

operably connecting at least one controller to at least one valve controlling hydraulic flow to at least one of said at least one main frame lift hydraulic cylinder, said at least one wing section lift hydraulic cylinder, and said at least one first bypass circuit;

configuring said at least one controller to bleed air from said at least one first hydraulic subsystem using the sub-steps of;

first, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure;

second, retracting said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder;

third, bypassing at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder while extending at least one of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder; and

fourth, extending said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder until each said at least one re-phasing port of each of said at least one main frame lift hydraulic cylinder and said at least one wing section lift hydraulic cylinder releases hydraulic pressure.

18. The method of claim 17, further comprising the steps of:

providing at least one second hydraulic subsystem including at least one main structure gauge lift hydraulic cylinder for at least partially raising and lowering the at least one main structure, at least one wing structure gauge lift hydraulic cylinder for at least partially raising and lowering the at least one wing structure, and at least one second bypass circuit bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder;

providing each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder with at least one re-phasing port;

operably connecting said at least one controller to at least one valve controlling hydraulic flow to at least one of said at least one main structure gauge lift hydraulic cylinder, said at least one wing structure gauge lift hydraulic cylinder, and said at least one second bypass circuit;

configuring said at least one controller to bleed air from said at least one second hydraulic subsystem using the steps of;

first, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure;

second, retracting said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder;

third, bypassing at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder while extending at least one of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder; and

fourth, extending said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder until said at least one re-phasing port of each of said at least one main structure gauge lift hydraulic cylinder and said at least one wing structure gauge lift hydraulic cylinder releases hydraulic pressure.

19. The method of claim 18, wherein:

said at least one wing section lift hydraulic cylinder further comprises at least two wing section lift hydraulic cylinders;

said at least one wing structure gauge lift hydraulic cylinder further comprises at least two wing structure gauge lift hydraulic cylinders;

said third step of bleeding air from said first hydraulic subsystem further includes first bypassing said at least one main frame lift hydraulic cylinder, then bypassing said at least one main frame lift hydraulic cylinder and sequentially bypassing additional wing section lift hydraulic cylinders until each wing section lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing section lift hydraulic cylinders; and

said third step of bleeding air from said second hydraulic subsystem further includes first bypassing said at least one main structure gauge lift hydraulic cylinder, then bypassing said at least one main structure gauge lift hydraulic cylinder and sequentially bypassing additional wing structure gauge lift hydraulic cylinders until each wing structure gauge lift hydraulic cylinder except one has been bypassed while extending the remainder of said at least one wing structure gauge lift hydraulic cylinders.

20. The method of claim 19, further comprising:

providing at least one third hydraulic subsystem including at least one main structure fold hydraulic cylinder for folding the at least one main structure over the main frame section, and at least one wing structure fold hydraulic cylinder for folding the at least one wing structure against the at least one wing section;

operably connecting said at least one controller to at least one valve controlling hydraulic flow to at least one of said at least one main structure fold hydraulic cylinder and said at least one wing structure fold hydraulic cylinder;

configuring said at least one controller to bleed air from said at least one third hydraulic subsystem using the steps of;

first, folding the at least one main structure over the main frame section using said at least one main structure fold hydraulic cylinder;

second, folding the at least one wing structure against the at least one wing section using said at least one wing structure fold hydraulic cylinder;

third, unfolding the at least one wing structure from against the at least one wing section using said at least one wing structure fold hydraulic cylinder; and

fourth, unfolding the at least one main structure from over the main frame section using said at least one main structure fold hydraulic cylinder.