IP Library › Granted Patent US 12,276,080
Granted Patent B2
US 12,276,080 · App. 17/963,375 · Granted Apr 15, 2025

Vacuum excavation apparatus having a deceleration vessel and methods for excavating a site

Inventors: Andy Strobel (Knoxville, IA); Corey Lanoue (Pella, IA); Daniel Hofland (Pella, IA); Adam Bates (Leighton, IA); David Gift (Pella, IA); Tayte Askelsen (Pella, IA); James W. Skinner (Pella, IA); Nathan J. Meyer (Knoxville, IA)
Assignee: Vermeer Manufacturing Company
E02F5/226B01D33/0353B01D33/804B04C5/14B04C5/28B04C9/00E02F3/8816E02F3/8891E02F3/907E02F3/925E02F3/9262E02F3/9268E02F3/9275E02F3/94E02F7/06F04B15/02F04B15/023F04B23/02F04B23/04F04B43/1253B01D45/16B04C5/26B04C2009/005B07B1/30E02F9/14
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Quick Facts
Patent No.
US 12,276,080
App. No.
17/963,375
Granted
Apr 15, 2025
Kind
B2
Abstract

Hydro excavation vacuum apparatus that process spoil material onboard the apparatus by separating water from the cut earthen material are disclosed.

Claims (30)

1. A hydro excavation vacuum apparatus for excavating earthen material comprising:

a vacuum system for removing cut earthen material and water from an excavation site in an airstream;

a deceleration system for collecting cut earthen material and water from the airstream, deceleration system comprising:

a deceleration vessel adapted to reduce a velocity of the airstream to allow material to fall from the airstream, the deceleration vessel being adapted such that the airstream is not vortexed within the deceleration vessel, the deceleration vessel having an inlet and a spoil material outlet disposed below the inlet; and

a material-engaging face configured to contact material entrained in the airstream;

an inlet conduit connected to the deceleration vessel inlet, the inlet conduit having a longitudinal axis, the longitudinal axis of the inlet conduit intersecting the material-engaging face, the material-engaging face forming an angle with a vertical axis of the deceleration vessel at the intersection between the longitudinal axis and the material-engaging face, the angle being from 5° to 60°;

a dewatering system comprising a vibratory screen for separating water from cut earthen material discharged from the spoil material outlet;

a cyclone fluidly connected to the deceleration vessel and downstream of the deceleration vessel; and

a wand for directing pressurized water toward earthen material to cut the earthen material.

2. The hydro excavation vacuum apparatus as set forth in claim 1 wherein the deceleration vessel comprises a lower portion that tapers inward toward the spoil material outlet.

3. The hydro excavation vacuum apparatus as set forth in claim 1 wherein the deceleration vessel comprises an air outlet disposed above the inlet.

4. The hydro excavation vacuum apparatus as set forth in claim 3 further comprising a plurality of cyclones including the cyclone, wherein the deceleration vessel comprises a plurality of air outlets, each outlet being fluidly connected to a respective cyclone of the plurality of cyclones to separate material entrained in an airstream withdrawn from the outlets.

5. The hydro excavation vacuum apparatus as set forth in claim 1 wherein the deceleration vessel has an effective cross-sectional area, the inlet conduit having an effective cross-sectional area, a ratio of the effective cross-sectional area of the deceleration vessel to the effective cross-sectional area of the inlet conduit being at least 7.5:1 to reduce the velocity of the airstream to allow material to fall from the airstream.

6. The hydro excavation vacuum apparatus as set forth in claim 1 further comprising an airlock disposed below the deceleration vessel to receive material discharged from the spoil material outlet.

7. A hydro excavation vacuum system for excavating earthen material comprising:

a chassis;

wheels attached to the chassis for transporting the hydro excavation vacuum system;

a vacuum system supported by the chassis for removing cut earthen material and water from an excavation site in an airstream;

a deceleration system supported by the chassis for collecting cut earthen material and water from the airstream, deceleration system comprising:

a deceleration vessel adapted to reduce a velocity of the airstream to allow material to fall from the airstream, the deceleration vessel being adapted such that the airstream is not vortexed within the deceleration vessel, the deceleration vessel having an inlet and a spoil material outlet disposed below the inlet; and

a material-engaging face configured to contact material entrained in the airstream;

an inlet conduit connected to the deceleration vessel inlet, the inlet conduit having a longitudinal axis, the longitudinal axis of the inlet conduit intersecting the material-engaging face, the material-engaging face forming an angle with a vertical axis of the deceleration vessel at the intersection between the longitudinal axis and the material-engaging face, the angle being from 5° to 60°; and

a dewatering system comprising a vibratory screen for separating water from cut earthen material discharged from the spoil material outlet;

a cyclone fluidly connected to the deceleration vessel and downstream of the deceleration vessel; and

a wand for directing pressurized water toward earthen material to cut the earthen material.

8. The hydro excavation vacuum system as set forth in claim 7 wherein the deceleration vessel comprises a lower portion that tapers inward toward the spoil material outlet.

9. The hydro excavation vacuum system as set forth in claim 7 wherein the deceleration vessel comprises an air outlet disposed above the inlet.

10. The hydro excavation vacuum system as set forth in claim 9 further comprising a plurality of cyclones including the cyclone, wherein the deceleration vessel comprises a plurality of air outlets, each outlet being fluidly connected to a respective cyclone of the plurality of cyclones to separate material entrained in an airstream withdrawn from the outlets.

11. The hydro excavation vacuum system as set forth in claim 7 wherein the deceleration vessel has an effective cross-sectional area, the inlet conduit having an effective cross-sectional area, a ratio of the effective cross-sectional area of the deceleration vessel to the effective cross-sectional area of the inlet conduit being at least 7.5:1 to reduce the velocity of the airstream to allow material to fall from the airstream.

12. The hydro excavation vacuum system as set forth in claim 7 further comprising an airlock disposed below the deceleration vessel to receive material discharged from the spoil material outlet.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 11, 2022
From: STROBEL, ANDY; LANOUE, COREY; HOFLAND, DANIEL; BATES, ADAM; GIFT, DAVID; ASKELSEN, TAYTE; SKINNER, JAMES; MEYER, NATHAN
To: VERMEER MANUFACTURING COMPANY
Reel/Frame 061376/0353 →
Continuity (2)
Continuation 16630057
Related Publication 20230030715A1 · Feb 2, 2023
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