High Performance Foil Rotor Improves De-Ink Pulp Screening Cameron - - PowerPoint PPT Presentation

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High Performance Foil Rotor Improves De-Ink Pulp Screening Cameron - - PowerPoint PPT Presentation

High Performance Foil Rotor Improves De-Ink Pulp Screening Cameron Pflueger 1 James A. Olson, Sean Delfel, Carl Ollivier-Gooch, Pat Martin 2 , Frederic Vaulot 1 and Robert W. Gooding 1 Department of Mechanical Engineering, Pulp and Paper Centre,


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SLIDE 1

High Performance Foil Rotor Improves De-Ink Pulp Screening

Cameron Pflueger1

James A. Olson, Sean Delfel, Carl Ollivier-Gooch, Pat Martin2, Frederic Vaulot1 and Robert W. Gooding1 Department of Mechanical Engineering, Pulp and Paper Centre, University of British Columbia, Canada

1Advanced Fiber Technologies, Montreal, Canada 2Catalyst Paper, Paper Recycling Division, Coquitlam, Canada

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SLIDE 2

Our Goal

To help our customers by:

  • enhancing pulp quality

(efficiency / fractionation)

  • increasing capacity
  • reducing power consumption
  • reducing the overall cost of

pulp screening

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SLIDE 3

Pulp Screening Basics

Pressure screens are essential for contaminant removal and fibre fractionation Cylinders and rotors are the key performance parameters

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SLIDE 4

Negative Peak, Pmin Pulse Width Positive Peak, Pmax

Nomenclature

2 3D

V P C

t Power

ρ = Pressure Coefficient: Power Consumption:

2 2 1 t P

V P C ρ =

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SLIDE 5

Previous Work

Wall Cp vs. foil camber (numerical, Feng et al. 2005).

  • 1

1 2

  • 0.6
  • 0.5
  • 0.4
  • 0.3
  • 0.2
  • 0.1

0.0 0.1

NACA 0012 (0% Camber)

NACA 4312 (4% Camber) NACA 8312 (8% Camber)

Perssure Coefficient, Cp Position, x/Chord

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SLIDE 6

CFD Single foil

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SLIDE 7

CFD Single foil

Wall Cp vs. angle-of-attack for a NACA 0012 foil (numerical, Feng et al. 2005).

2 2 1 t P

V P C ρ =

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SLIDE 8

New Developments

Foil Parameters Studied: Angle-of-attack (α) Flap Angle (δ) Flap positioning

Anderson, 1991 Canadian Forces C-130

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SLIDE 9

Results

Flap angle was varied at a constant α : δ = 7°:

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SLIDE 10

Results

δ = 15°: Flap angle was varied at a constant α :

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SLIDE 11

Results

δ = 22°: Flap angle was varied at a constant α :

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SLIDE 12

Results

δ = 29°: Flap angle was varied at a constant α :

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SLIDE 13

Results

δ = 36°: Flap angle was varied at a constant α :

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SLIDE 14

Results

The α- and δ- sweep data was combined to create surfaces of max. and min. wall CP.

  • Min. CP vs. α and δ. The ‘x’ marks the optimum of

CP = -0.82 at α = 1.2 deg. and δ = 16 deg.

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SLIDE 15

Results

Surfaces were constructed of min. and max. wall CP vs. x- and y- position of the flap LE:

  • Min. CP vs. x and y positions of the flap LE. The optimum of

CP = -0.82 is at x = -0.05*c and y = -0052*c.

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SLIDE 16

Mill Trial – De-Ink Fine Screen

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SLIDE 17

Mill Trial – De-Ink Fine Screen

Catalyst Paper, Paper Recycling Division Flowsheet

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SLIDE 18

Mill Trial – De-Ink Fine Screen

10 15 20 25 30 35 40 45 50 55 11 12 13 14 15 16 17 Tip Speed (m/s) Power (kW) DEF Rotor OEM Rotor 42%

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SLIDE 19

Mill Trial – De-Ink Fine Screen

1.0 1.2 1.4 1.6 1.8 2.0 12 13 14 15 16 17 Tip Speed (m/s) Thickening Factor DEF Rotor OEM Rotor

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SLIDE 20

Mill Trial – De-Ink Fine Screen

40% 50% 60% 70% 80% 12 13 14 15 16 17 Tip Speed (m/s) Stickies Removal Efficiency DEF Rotor OEM Rotor

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SLIDE 21

Mill Trial – De-Ink Fine Screen

0% 20% 40% 60% 80% 100%

1 2

Stickies Removal Efficiency OEM Rotor DEF Rotor Area Count

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SLIDE 22

Mill Trial – De-Ink Fine Screen

1 2 3 4 5 6 7 8 0.21 0.3 0.4 0.5 0.75 1 1.5 2 2.5 3 Stickies Distribution (mm2)

Accept Stickies Concentration (number per gram)

OEM Rotor DEF Rotor <

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SLIDE 23

Conclusions

Multi-element foil technology allows for greater control of pressure pulse.

  • Wider, stronger pulse can be obtained

Reducing Rotor Speed Increases Stickies Removal Efficiency Power savings of 42% have been shown thus far with equivalent OEM rotor capacity Preliminary mill trials extremely promising.

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SLIDE 24

Thank you! Questions?