Aerial Topdressing Issues Around Product Flow Properties One Size - - PowerPoint PPT Presentation

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Aerial Topdressing Issues Around Product Flow Properties One Size - - PowerPoint PPT Presentation

Aerial Topdressing Issues Around Product Flow Properties One Size Does Not Fill All NZCPA Miles Grafton, Rob Murray & Ian Yule Email: M.Grafton@Massey.ac.nz Problem Statement Materials Various Urea DAP Superphosphate Lime


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SLIDE 1

Aerial Topdressing Issues Around Product Flow Properties

One Size Does Not Fill All NZCPA Miles Grafton, Rob Murray & Ian Yule

Email: M.Grafton@Massey.ac.nz

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SLIDE 2

Problem Statement

  • Materials Various
  • Urea DAP Superphosphate Lime slurries and

liquids

  • Many products’ properties change with time and

storage conditions

  • Delivery Equipment Standard
  • Hopper, box, multi-vane spreader or spray gear
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SLIDE 3

Factors That Affect Bulk Solid Flow

  • Moisture Content
  • Humidity
  • Temperature
  • Pressure
  • Fat (Not applicable to fertiliser)
  • Particle Size Distribution
  • Angle of Repose
  • Bulk Density
  • Angle of Internal Friction
  • Cohesion
  • Adhesion
  • Compressibility (more than 20% tend not to be free flowing)
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SLIDE 4

Mass Flow – Funnel Flow

Photographs provided by John Maber

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SLIDE 5

Cohesive tapped Limes bridging in a beaker

Typical to all Limes tested

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SLIDE 6

Bulk solids will vary in bulk density depending on their history

Bulk Density Comparisons

500 1,000 1,500 2,000 2,500 A B C D E F G H I Limes Kg/ cubic metre As ReceivedBulk Density Kg/m³ Tap Density Kg/m³ Loose Bulk Density Kg/m³

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SLIDE 7

Jenike Shear Cell Some answers after some time

  • Angle of internal friction angle of wall

friction

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SLIDE 8

Some experimental work, some

geometry and some charts

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SLIDE 9

Flow measurements LabView RFID tags & load cell

  • Full Size Experiments will be undertaken
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SLIDE 10

A Model Hopper to Compare Theoretical and Actual Hopper ½ Angles

  • Shimadsu tensile tester to calibrate load

cell

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SLIDE 11

Early days of NZ topdressing fertiliser in the top and out the bottom

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SLIDE 12

Equipment has changed but the principle is the same

  • Aircraft, Loaders, GPS, Materials
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SLIDE 13

Structure of presentation

  • Justification for modelling work
  • Overall aim - VRAT
  • Modelling particle ballistics
  • Improving spreading techniques

Aerial topdressing technology

Where are we headed?

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SLIDE 14

Variable rate of hill country: agronomic impact of using decision tree model

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SLIDE 15

GPS Proof of Placement

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SLIDE 16

GPS Well positioned aircraft & manual control of product release

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SLIDE 17

Distribution pattern GA200c aircraft

100 200 300 400 500 600 700

  • 13 -12 -11 -10
  • 9
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  • 2
  • 1

1 2 3 4 5 6 7 8 9 10 11 12 Distance from Centre (m) Application rate (kg ha-1) Actual Predicted

Comparison of the actual and predicted lateral distribution pattern for a thirty-tray transverse test for a Gippsland Aeronautics GA200C fixed wing aircraft with a six duct spreader. Data source: 2002 field report, aircraft flying conditions – altitude 25 m, superphosphate, ground speed 54 m s-1, wind velocity 0 m s-1, wind angle 0° from flight direction.

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SLIDE 18

50 100 150 200 250

  • 10
  • 9
  • 8
  • 7
  • 6
  • 5
  • 4
  • 3
  • 2
  • 1

1 2 3 4 5 6 7 8 9 10 Lateral position (m) Deposition (kg ha-1) 0.5mm 1.9mm 3.7 mm 4.7 mm 7.0 mm

Predicted lateral deposition for 0.5, 1.9, 3.7, 4.7 and 7mm diameter particles from a GA200C fixed wing aircraft with a six duct spreader. Conditions - altitude 25 m, superphosphate, ground speed 54 m s-1, wind velocity 0 m s-1, wind angle 0° from flight direction

Distribution pattern GA200c aircraft

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SLIDE 19

50 100 150 200 250 300 350 400

  • 10
  • 9
  • 8
  • 7
  • 6
  • 5
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  • 2
  • 1

1 2 3 4 5 6 7 8 9 10 Lateral position (m) Deposition (kg ha -1)

DUCT1 DUCT2 DUCT3 DUCT4 DUCT5 DUCT6

Predicted lateral deposition from each duct for a GA200C fixed wing aircraft with a six duct spreader. Conditions - altitude 25 m, superphosphate, ground speed 54 m s-1, wind velocity 0 m s-1, wind angle 0° from flight direction

Distribution pattern GA200c aircraft

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SLIDE 20

Modeled transverse fertilizer distribution of particles ejected from a Gippsland Aeronautics GA200C fixed wing aircraft with a six duct spreader – altitude 25 m, aircraft heading 360°, superphosphate, ground speed 54 m s-1, no wind and 4 ms-1 wind blowing from 315°

Distribution pattern GA200c aircraft

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SLIDE 21

Modeled spatial fertilizer deposition of particles ejected from a Gippsland Aeronautics GA200C fixed wing aircraft with a six duct spreader – altitude 25 m, superphosphate, ground speed 56 m s-1, wind in case A) no wind, B) 4 m s-1 wind blowing from 315°

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SLIDE 22

Deposition

50 100 150 200 250 300 350 400 1 2 3 4 5 6 7 8 9 10 Collector number Application Rate (kg/ha) Actual Predicted

  • Predicted mean application 93 kg ha-1

(std. dev. 92 kg ha-1)

  • Total quantity of fertiliser applied was

predicted to be 1.9 tons (CV) of 0.97.

  • Within the application zone, 1597 kg of

fertiliser over 14.87 ha

  • In the non-application zone, 193.3 kg of

superphosphate over 3.0 ha was applied.

  • The remaining 103.9 kg was applied
  • utside the trial boundary.
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SLIDE 23

Predicted field scale application (kg ha-1) using automated hopper door control on a 25 ha trial site, 15 km North of Kimbolton, Manawatu, New Zealand.

Automated Control

  • Predicted mean application rate was 107 kg

ha-1

  • Total fertiliser applied, 1.8 tons at a CV of

0.93.

  • Within the application zone, 1819 kg of

fertiliser over 15.59 ha,

  • In the non-application zone, 71.1 kg of

superphosphate over 1.49 ha was applied.

  • The remaining 45.7 kg was applied outside

the trial boundary.

  • In the automated control system case, only

6% of the total fertiliser spread was outside the application area, compared to 16% in previous example

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SLIDE 24

Table 1. Economic analysis for the application of superphosphate fertilizer on a 25 ha trial site, 15 km North of Kimbolton, Manawatu, New Zealand. Results are also extrapolated to a hypothetical 1500 ha (effective) farm scale. Superphosphate cost NZ$ 191 ton-1 (Ravensdown, 2005), target application rate 150 kg ha-1.

Parameter Trial Modeled Automated modeled Extrapolated Trial Extrapolated Automated Units Area of application zone 19 19 1500 1500 [ha] Area of non-application zones 6 6 474 474 [ha] Total fertilizer applied 1.9 1.8 150 145 [t] Fertilizer applied outside field boundary (a) 104 46 8211 3632 [kg] Fertilizer applied in non-application zone (b) 193 71 15237 5605 [kg] Total quantity of fertilizer applied off target (a + b) 297 117 23447 9237 [kg] Cost of off target application 57 22 4500 1737 [NZD $] Cost per hectare 3.0 1.1 3.0 1.1 [NZD $ ha-1]

Economics

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SLIDE 25

401 340 389 325 311 316 Return ($/ha) 1.37 1.27 1.33 1.51 1.06 1.18 Fertiliser Response ($/kg) $ 1,008,618 $ 854,967 $ 979,285 $ 817,957 $ 783,681 $ 795,363 Profit $ 140,222 $ 128,558 $ 140,081 $ 105,952 $ 140,228 $ 128,547 *Cost Fert 738 671 738 542 738 671 Fert Used (T) 18 15 17 14 14 14 Mean SU/ha 45070 38585 43914 36246 36246 36246 Potential SU 24789 21222 24153 19935 19935 19935 Available Pasture 9846 8429 9593 7918 7918 7918 Mean kgDM/ha Full VRAT Reduced VRAT Simple VRAT Simple VRAT Inc Blanket Blanket Excludes Non responsive zones

Breakdown of Results Breakdown of Results

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SLIDE 26
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SLIDE 27

Fletcher Aircraft delivering Lime demonstrating shear fractured flow

Film courtesy of John Maber

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SLIDE 28

The way forward

  • Bulk solids flow affected through many means
  • Product history & storage
  • Moisture content and humidity
  • Particle size distribution
  • Compressibility & bulk density
  • Temperature
  • Better storage and on farm facilities
  • More consistent product with less variability
  • Better control of moisture and less fines to reduce

compressibility and variations in bulk density

  • This should enable better control of on farm application

rates