Earth working machine and blade condition control system therefor

• US 4,431,060 A
• Filed: 04/15/1981
• Issued: 02/14/1984
• Est. Priority Date: 04/15/1981
• Status: Expired due to Fees

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Tractor Co (Caterpillar Incorporated)
• Inventors: Scholl, Rolland D., Easterling, Gene B.
• Primary Examiner(s): Stouffer, Richard T.
• Application Number:
  US06/278,491
• Time in Patent Office: 1,035 Days
• Field of Search: 172/2, 172/4.5, 172/793, 172/795, 172/796, 172/797, 172/799, 33/313, 33/328, 33/351, 37/DIG. 1, 37/DIG. 20, 404/84, 73/432 R, 73/507, 73/510
• US Class Current: 172/4.5
• CPC Class Codes: E02F 3/844 for positioning the blade, e.g. hydraulically
• CPC Class Codes: E02F 3/845 using mechanical sensors to determine the blade position, e.g. inclinometers, gyroscopes, pendulums

Abstract

An earth working machine having an earth shaping blade (30) employs a control system for maintaining the blade (30) at a desired slope relative to a reference grade irrespective of lateral movement of the blade (30) or deflection of front and rear frame sections (15, 18). A ground engaging trailing wheel (96) mounted at the rear of the blade (30) senses rotation of the blade (30) relative to the direction of machine travel resulting from rotation or lateral shifting of the blade (30) and operates a potentiometer (124) to produce a control signal proportional to the magnitude of blade rotation. A first pair of accelerometers (128, 130) mounted on the blade (30) for rotation by the trailing wheel (96) produces blade controlling signals respectively corresponding to the change in slope and pitch of the blade (30) relative to the front frame section (15) of the machine. A second pair of accelerometers (42, 44) mounted at transversely spaced locations on the front frame section (15) produce control signals indicative of the roll of the front frame section (15) while an additional accelerometer (90) mounted on the rear frame section (18) produces control signals indicative of the frame pitch. An electronic circuit (94) algebraically combines the control signals for use in controlling the operation of a pair of hydraulic cylinders (38, 40) which maintain the blade (30) at a desired slope.

Claims

1. In an earth working machine including an articulated frame (10) adapted for moving over the earth and having a front frame section (15) and a rear frame section (18) pivotally coupled with said front frame section (15), an earth working blade (30), means (22, 26, 28) for mounting said blade (30) for rotation on said front frame section (15), means (38, 40) connected between said blade mounting means (22, 26, 28) and said front frame section (15) for adjustably supporting said blade mounting means (22, 26, 28) on said front frame section (15), apparatus for automatically controlling said supporting means (38, 40) to maintain said blade (30) at a preselected slope relative to a reference plane irrespective of lateral movement of said front frame section (15) relative to said rear frame section (18), the improvement comprising:

blade circle angle detector means (96) for sensing rotation of said blade (30) relative to the line-of-flight thereof, said blade circle angle detector means (96) including a ground engaging guide number (116) and means (102, 110, 112,

     114) for mounting said guide member (116) rearward of said blade (30) for rotation about a reference axis extending perpendicular to said reference plane;

angular position sensing means (90) for sensing changes in the inclination of said rear frame section (18) relative to said reference plane;

electronic resolver means (94) for producing a control signal indicative of the degree of both the rotation of said blade (30) relative to said line-of-flight and the inclination of said rear frame section (18) relative to said reference plane; and

control means (88, 60,

     64) for operating at least one of said adjustable supporting means (38,

     40) and maintaining said blade (30) at said preselected slope thereof.

2. The apparatus of claim 1, wherein said guide member mounting means (102, 110, 112, 114) includes:

a support (108, 110,

     112) rotatably mounted on said blade mounting means (22, 26,

     28) and being rotatable about said reference axis, and

a connecting element (114) extending rearwardly away from said blade (30) and being connected to said support (108, 110,

     112), said ground engaging guide member (116) being rotatably mounted on said connecting member (114).

3. The apparatus of claim 2, wherein said guide member mounting means (102, 110, 112, 114) includes:

a bracket assembly (102) secured on said blade mounting means (22, 26,

     28) and wherein said support (108, 110,

     112) includes a shaft (110) journalled for rotation on said bracket assembly (102) and a spacer (112) secured on one end of said shaft (110) and extending radially outward from the longitudinal axis of said shaft (110), said connecting member (114) being elongate and having one end thereof pivotally connected with said spacer (112).

4. The apparatus of claim 3, wherein said guide member mounting means (102, 110, 112, 114) includes a counterweight (120) secured to said spacer (112) in spaced relationship to the longitudinal axis of said shaft (110) opposite said connecting member (114).

5. The apparatus of claim 2, wherein said electronic resolver means (94) includes:

a tangent function potentiometer (124) having first and second portions (124,

     126) shiftable relative to each other and being respectively connected to said shaft (110) and said bracket assembly (102).

6. The apparatus of claim 1, including first and second means (128,130) carried by said guide member mounting means (102,110,112,114) for respectively sensing changes in the magnitude of inclination of said blade (30) along first and second axes extending substantially perpendicular to each other and substantially parallel to said reference plane.

7. The apparatus of claim 6, wherein each of said first and second means (128, 130) includes:

an accelerometer (128,

     130) adapted for producing first and second sensed output signals respectively indicative of the corresponding change in blade inclination and pitch, and wherein said electronic resolver means (94) includes first circuit means (272) for algebraically combining said first and second output signals with said control signal.

8. The apparatus of claim 7, wherein said angular position sensing means (90) includes accelerometer means (90) for producing a third sensed output signal indicative of the changes in inclination of said rear frame section (18) and wherein said electronic resolver circuit (94) includes second circuit means (224) for algebraically combining said third output signal with said second output signal.

9. The apparatus of claim 1, wherein said sensing means (90) is mounted on said rear frame section (18) and said control means (88, 60, 64) is operably coupled with said resolver means (94).

10. In an earth working machine including an articulated frame (10) adapted for moving over the earth and having a front frame section (15) and a rear frame section (18) pivotally coupled with said front frame section (15), an earth working blade (30), means (22, 26, 28) for mounting said blade (30) for rotation on said front frame section (15), means (38, 40) connected between said blade mounting means (22, 26, 28) and said front frame section (15) for adjustably supporting said blade mounting means (22, 26, 28) on said front frame section (15), apparatus for automatically controlling said supporting means (38, 40) to maintain said blade (30) at a preselected slope relative to a reference plane irrespective of lateral movement of said front frame section (15) relative to said rear frame section (18), the improvement comprising:

blade circle angle detector means (96) for sensing rotation of said blade (30) relative to the line-of-flight thereof, said angle detector means (90) being connected with said blade (30) and being operational to sense the line-of-flight of said blade (30) only when said angle detector means (90) engages the earth;

angular position sensing means (90) for sensing changes in the inclination of said rear frame section (18) relative to said reference plane;

electronic resolver means (94) for producing a control signal indicative of the degree of both the rotation of said blade (30) relative to said line-of-flight and the inclination of said rear frame section (18) relative to said reference plane; and

control means (88, 60,

     64) for operating at least one of said adjustable supporting means (38,

     40) and maintaining said blade (30) at said preselected slope thereof.