CUSTOM FARM SERCIVE OF ARIZONA (US)
| US1722467A | 1929-07-30 | |||
| FR1183961A | 1959-07-16 | |||
| FR2586167A1 | 1987-02-20 | |||
| GB765091A | 1957-01-02 | |||
| US2772061A | 1956-11-27 | |||
| US2562524A | 1951-07-31 | |||
| US4260108A | 1981-04-07 |
| 1. | A discharge device for use in discharging treatment substance (e.g. liquid) onto a crop or ground from a crop spraying aircraft, the device being adapted for mounting on an aircraft and including treatment substance supply means, characterised in that said device comprises a conduit member (2) providing an air passage (4, 6, 7), said supply means (9) supplying treatment substance to said air passage (4, 6, 7), said passage including an inlet portion (4) to receive air due to forward movement of the aircraft, and an outlet portion (6) set at an angle relative to said inlet portion (4) for directing a downward discharge of said air together with said treatment substance. |
| 2. | The device as claimed in claim 1, characterised in that the outlet portion (6) communicates with the inlet portion (4) via an elbow portion (7) of the air passage. |
| 3. | The device as claimed in any one of the preceding claims, characterised in that the supply means (9) include a nozzle inlet (9A) . |
| 4. | The device as claimed in claim 3 when dependent on claim 2, characterised in that the nozzle form inlet (9A) discharges at the elbow portion (7) of the air passage. |
| 5. | The device as claimed in claim 3 or 4, characterised in that the outlet portion (6) of the air passage has a length which is a multiple of the width of the air passage. |
| 6. | The device as claimed in claim 5, characterised in that the distance from the nozzle form inlet (9A) to the discharge from the air passage outlet portion (6) is at least three times the crosssectional width of the inlet portion (4) of the air passage. |
| 7. | The device as claimed in any one of the preceding claims, characterised in that the elbow portion (7) is of rectangular crosssection, and in that arcuate guide vanes (Vι_ to V4) are present in the neck portion (7, for improved flow through the neck portion. SUBSTITUTE SHEET . |
| 8. | The device as claimed in claim 7, characterised in that the inlet portion (4) is also of rectangular cross section while at least a part (6A) of the outlet portion (6) is of circular crosssection, and in that a transitional portion (6B) is present for a smooth transition in shape between the rectangular elbow portion (7) and the circular part (6A) of the outlet portion (6) . |
| 9. | The device as claimed in claim 1, characterised in that the inlet potion (4) is of diverging form while the outlet portion (6) is of converging form, and in that a relatively small diameter throat (15) is present between said inlet and outlet portions (4, 6) . |
| 10. | The device as claimed in any one of the preceding claims, characterised in that the inlet portion (4) has a bell mouth form inlet (3) . |
| 11. | The device as claimed in any one of the preceding claims, characterised in that the conduit member (2) is of streamline form. |
| 12. | The device as claimed in any one of the preceding claims, characterised in that the outlet portion (6) comprises a pipe extending laterally from the conduit member (2) . SUBSTITUTE SHEET. |
The present invention relates to a device for . liquid and solid delivery from crop spraying aircraft.
The present invention provides for an improved method of directing and delivering fertilizer, herbicides, irrigation water and other toxic or non- toxic chemical sprays from an inflight aircraft crop spraying system such that the residual velocity of the liquid droplets, atomised vapours and solids is sensibly downwards at high velocities on leaving the slipstream disturbance area of the spraying aircraft and does not have any significant horizontal component of velocity due to the aerodynamic turbulence of the propulsion system of the aircraft.
It is also a feature of this invention that the droplets and/or solid particles may be accelerated to subsonic, sonic or supersonic velocities using a minor portion of the energy of forward motion of the aircraft at normal flying speeds to this effect. Supersonic delivery velocity will be provided where the height of the flight path above the crops and the droplet size precludes leaf damage due to impact of the droplets etc.
According to the present invention there is provided a discharge device for use in discharging treatment substance (e.g. liquid) onto a crop or ground from a crop spraying aircraft, the device being adapted for mounting on an aircraft, said device comprising a conduit member providing an air passage, and supply means for supplying treatment substance to said air passage, said passage including an inlet portion to receive air due to forward movement of the aircraft, and an outlet portion set at an angle relative to said inlet portion for directing a downward discharge of said air together with said treatment substance.
Essentially the apparatus according to the invention is one or a number of such devices susoended
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from the wings or spray boom of an aircraft and preferably comprises a bell form inlet mouth leading to said inlet portion of the air passage, an elbow being present between the inlet and outlet portions. There is provided a smooth change of direction in the orifice device such that the included angle between the direction of the bell mouth and the exit lies normally between 90° and 45°. The bell mouth inlet will be sensibly aligned in the direction of the aircraft flight while the exit from the device will be usually, but not necessarily exclusively, downwards and inclined forward of the vertical by an angle variable according to the aircraft velocity and the droplet velocity such that the resultant absolute velocity of the droplets can be substantially vertically downwards.
The air passage can be of convergent/divergent form including a throat.
The design of the orifice convergence, throat and divergence follows normal practice for such orifices, when operating in air viz:- that the static pressure at the throat area will be approximately 53% of the developed inlet pressure at the bell mouth, which in one embodiment of the invention may be a parallel-sided or Kuchemann type compression inlet, due to the ram effect of forward flow and the divergent portion will have an included angle of 10° to 12° for a length as determined whether the exit velocity of the droplets is required to be sonic, subsonic or supersonic to a required degree.
Liquid spray or solid material will be introduced to each orifice system by means of a pressurised feed to a nozzle normally located between the bell mouth of the orifice and the throat but may be external to the bell mouth and may eject spray material in any requested direction.
The distance from the liquid spray inlet to the outlet may be at least three times the inlet diameter of the nozzle for maximum spray droplet velocity leaving the nozzle.
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Embodiment of the present invention will now be described by way of example with reference to the accompanying drawings in which: -
Fig. 1 shows a side elevation of a discharge orifice device, according to the present invention for use in spray discharge from crop spraying aircraft;
Fig. 2 shows a front elevation of the device;
Fig. 3 shows a view on section A-A of Fig. 1;
Fig. 4 shows a front view of a light aircraft fitted with a device generally as shown in Figs. 1 to 3; and
Fig. 5 shows a cross-sectional view of a further embodiment.
Referring to Figs. 1 to 3, a discharge orifice device 1 is adapted for mounting below a wing of a crop spraying aircraft and serves for the discharge of spray treatment substances (liquid) downwards onto a crop or onto the ground prior to crop growing. The device 1 comprises a streamline form body 2 having an air inlet 3 of square cross-section leading to an inlet air passage 4 in the body 2, the body wall portion 5 at the inlet 3 being of curved bell mouth form.
An outlet pipe 6 extends laterally from the body 2 to provide a downwards directed discharge flow from the device 1, and the pipe 6 communicates with the inlet air passage 4 via an elbow 7 in the body 2 the edges of which elbow 7 are defined by curved vanes V-^, V4 of a vane set V 1 to V4. Vanes V2, V3 of the set are located between the edge vanes V l7 V 4 to encourage a smooth airflow between the inlet passage 4 and the discharge pipe 6. The outer portion 6A of pipe 6 is of circular cross-section and a transition section 6B is present arranged for transition of the square section of the inlet and elbow to the circular section of portion 6A. A support strut 8 is provided to facilitate mounting of the device 1 below an aircraft wing.
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A supply conduit 9 for treatment substance (fluid) passes down through the body 2 at the elbow 7 and has a discharge nozzle 9A at the outlet end of the elbow 7 discharging downwardly into the pipe 6, so that the treatment fluid is caught up and carried by air passing through the air passage (4, 6, 7) in the device 1. The conduit 9 is connected to a suitable reservoir (not shown) of treatment substance (fluid) , and a pressurised feed of the treatment fluid to the device 1 can be employed.
The air passage (4, 6, 7) of the device 1 is arranged to give optimum results and in this connection the pipe 6 will have an appropriate length. In particular the pipe 6 (i.e. portions 6A/6B) can have a length such that the distance from the spray inlet at nozzle 9A to the outlet from the pipe 6 is preferably at least three times the inlet diameter of the orifice device for maximum spray droplet velocity leaving the orifice device 1. The pipe 6 can have a tail 6T.
The mounting of the device 1 on a crop spraying aircraft 10 is shown in Fig. 4. However, in Fig. 4 two additional similar devices 1A. IB are included located side-by-side with the device 1, the devices 1A, IB having sidewards and downwardly directed discharge pipes 6 instead of the directly downward pipe 6 of the device 1, all to give improved spray cover. In use of the device 1, when mounted on the aircraft 10, forward movement of the aircraft 10 in flight causes air to be drawn into the orifice device 1 via the inlet 3 and the air is accelerated in the device 1 to a high speed. Treatment liquid is discharged via nozzle 3A and is carried in the form of droplets by the air flow in the device so as to have a velocity substantially that of the air and the liquid droplets are discharged downwardly at speed from the outlet pipe 6.
Fig. 5 shows an alternative form of discharge orifice device 1 In this case, the inlet 4 and the elbow 7 converge to a smaller diameter threat portion
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15, while the outlet discharge 16 is of diverging form, so that the device 1 of Fig. 5 is of a distinct venturi form. Also, in this embodiment the nozzle 9A is located at the inlet portion 4 but could be located as in Fig. 1 and the conduit 9 is shown connected to a spray boom pipe 9B for treatment liquid delivery. To minimise drag consequent on fitting of the device to an aircraft, the device 1 of Fig. 5 is deployed in fairing formations 17A, 17B for both inlet and outlet sections. The device 1 can be fitted to the aircraft wing by means of a fixing bracket 18. The port wing of the aircraft 10 of Fig. 4 is shown fitted with the devices 1 of Fig. 5.
The benefits accruing to an aircraft spraying system will arise as a result of the implementation of this invention from the increased accuracy of spray deposition, the reduction of the possibility of contamination of adjacent areas by chemical material and the reduction of spray drift which could have serious adverse environmental consequences.
The present invention can be used advantageously with the spray sensing or assessment operation described in the applicant's co-pending PCT Application filed of even date.
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