The Affect of Flat-fan Nozzle Angle on Aerial Spray Droplet Spectra Presented at ASAE/NAAA Technical Session 39 th Annual NAAA Convention Silver Legacy.

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Presentation transcript:

The Affect of Flat-fan Nozzle Angle on Aerial Spray Droplet Spectra Presented at ASAE/NAAA Technical Session 39 th Annual NAAA Convention Silver Legacy Hotel and Casino Dec. 5, 2005 Robert E. Wolf, Scott Bretthauer, Dennis Gardisser Paper # AA05-003

Objective: The objective of this study was to evaluate the affect of spray angel on flat-fan droplet spectrums for fixed wing aerial applications. Patterns? Compared to USDA Models?

Materials and Methods: Multiple studies KS, CO, IL Multiple Aircraft Cessna AT 502 AT Thrush CP11TT with CP aerial flat-fan nozzles Multiple Angle Tests Collected Spray Droplets on WSP Compared to USDA Model

Materials and Methods: Kansas Trial – Wamego Airport CP11TT with flat-fan nozzles 2 GPA ( nozzles) 5 GPA ( nozzles) 40 psi Average speed mph by GPS Sprayed into head wind Application height feet Multiple angles of orientation 8,15,30,45,60,75 CP-06 Swivel

CP Swivel: Quick change angle device 15 degree increments Flexibility to increase the angle of attack Will this influence the droplet spectrum?

Materials and Methods: Illinois Trials – Mattoon, Lincoln CP11TT with flat-fan nozzles 2, 3, 4, and 5 GPA 4015, 4020, 4025, psi AT502, AT802’s, 510 Thrush, Cessna , 150, 188 mph GPS measured Sprayed into head wind Application height feet Orientation – 8 and 30 degrees Determined by rotating the nozzle body and the nozzle

Collection Procedure: 1 pass per angle Water sensitive paper on each collector 1 x 3 or 2 x 3 inch Collectors evenly spaced across the swath width Analyzed with DropletScan and composite statistics reported DV0.1, VMD, DV0.9 Compared to USDA Model

USDA Aerial Nozzle Atomization Models

Cessna 188 PSI, 35 nozzles, 115 MPH) Wamego

Cessna 188 PSI, 35 nozzles, 115 MPH) Wamego

JARBA (Rotating Boom)

Goodland 2003 AT 502 – 140 MPH - 45

Summary of findings - Kansas: Nozzle angle increase - results in smaller droplets Wamego with Cessna 115 MPH At 2 and 5 GPA For VD0.1, VMD, and VD0.9 Nozzle orifice size increase - results in larger droplets 2 GPA resulted in droplets smaller than the USDA Model 5 GPA was better matched to the USDA Model

Summary of findings - Illinois: Nozzle orifice size increase - results in larger droplets Not always true and not much effect AT 502 – slight increase AT 802’s – increase and decrease Nozzle angle increase - results in smaller droplets True for all tests For VD0.1, VMD, and VD0.9 All the Air Tractors and Thrush droplets - larger than the USDA Model Cessna 188 matched the USDA Model

Conclusions: Increasing the nozzle angle reduces the size of the droplet spectra These data sets indicate about 2-3 micron reduction in the VMD for each degree of downward slope Trends are consistent with the USDA Models At higher speeds the measurements tended to have a droplet spectra larger the USDA Model predicted Angle adjustment is an option for adjusting the droplet spectrum

Acknowledgements: Cary Rucker Rick Reed Harley Curless Don Haley David Kurtz Les Cady Carolyn Baecker