Abstract:
A system for determining the quantity of a liquid agricultural product available for spraying on a field from a tank in an airplane comprising a payload storage tank for holding the agricultural product, an elongated magnetostrictive linear displacement transducer tube located vertically in the aircraft payload storage tank, a probe float slidably coupled to move up or down on the elongated magnetostrictive linear displacement transducer tube, and a permanent magnet coupled to the probe float. The position of the magnet is sensed by the elongated magnetostrictive linear displacement transducer tube which generates a signal that marks the level of the liquid in the aircraft payload storage tank, and converter means converts the generated signal that marks the level of the liquid in the aircraft payload storage tank to a quantity of liquid in the aircraft payload storage tank which is displayed to the pilot.

Description:
REFERENCE TO RELATED APPLICATIONS 
       [0001]    This patent application claims the benefit of U.S. Provisional Application No. 61/262,612 filed on Nov. 19, 2009, the disclosure of which is incorporated herein by reference in its entirety. 
     
    
     BACKGROUND OF THE INVENTION 
       [0002]    1. Field of the Invention 
         [0003]    The present invention relates to a method and system for determining the quantity of liquid product that remains in an airplanes hopper by measuring the liquid volume of an liquid agricultural product in an aircraft pay load hopper. 
         [0004]    2. Background of the Invention 
         [0005]    Hopper tanks for holding liquid agricultural product which is to be dispensed over a farm by a small airplane can have irregular shapes and sizes. This can result in the fact that the indication of the level of the agricultural product in the hopper tank, typically provided by a sensor of one of the various known types, can not easily be converted into a reliable indication of the quantity or volume of the agricultural product that is available for spraying. Unreliable information that relates to the quantity of liquid agricultural product that is present in the small airplane payload hopper can have a negative effect on the loading, balancing and operation of the airplane when taking off, during flight and on landing. 
         [0006]    Systems for indicating liquid agricultural product level currently in use include mechanical, electromechanical or electronic “damping” means which makes it possible to attenuate the oscillations of the indication provided to the use upon variation in the level of the liquid agricultural product in the airplanes hopper tank due to swashing and in general, to oscillations in the level due to maneuvers or dynamic conditions involving rapid variations of the airplane such as turns, banks, accelerations, abrupt changes in altitude, etc. Such systems may measure rapid dynamic variations in the level of the liquid agriculture product in the hopper tank which does not relate to effective variations in the quantity or volume of agricultural product that is available in the tank for spraying. 
         [0007]    Thus, there exists a need for a simple system for determining the quantity or volume of liquid agriculture product that is in an airplanes payload hopper that is available for spraying that is reliable. 
       SUMMARY OF THE INVENTION 
       [0008]    In an exemplary embodiment of the present invention, there is disclosed a system for determining the quantity of a liquid agricultural product available for spraying on a field from a tank in an airplane comprising a payload storage tank for holding the agricultural product, an elongated magnetostrictive linear displacement transducer tube located vertically in the aircraft payload storage tank, a probe float slidably coupled to move up or down on the elongated magnetostrictive linear displacement transducer tube, and a permanent magnet coupled to the probe float. The position of the magnet is sensed by the elongated magnetostrictive linear displacement transducer tube which generates a signal that marks the level of the liquid in the aircraft payload storage tank, and converter means converts the generated signal that marks the level of the liquid in the aircraft payload storage tank to a quantity of liquid in the aircraft payload storage tank which is displayed to the pilot. 
         [0009]    The more important features of the invention have thus been outlined in order that the more detailed description that follows may be better understood and in order that the present contribution to the art may better be appreciated. Additional features of the invention will be described hereinafter and will form the subject matter of the claims that follow. 
         [0010]    Before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments and of being practiced and carried out in various ways. Also it is to be understood that the phraseology and terminology employed herein are for the purpose of description and should not be regarded as limiting. 
         [0011]    As such, those skilled in the art will appreciate that the conception, upon which this disclosure is based, may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention. 
         [0012]    The foregoing has outlined, rather broadly, the preferred feature of the present invention so that those skilled in the art may better understand the detailed description of the invention that follows. Additional features of the invention will be described hereinafter that form the subject of the claims of the invention. Those skilled in the art should appreciate that they can readily use the disclosed conception and specific embodiment as a basis for designing or modifying other structures for carrying out the same purposes of the present invention and that such other structures do not depart from the spirit and scope of the invention in its broadest form. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0013]    Other aspects, features, and advantages of the present invention will become more fully apparent from the following detailed description, the appended claim, and the accompanying drawings in which similar elements are given similar reference numerals. 
           [0014]      FIG. 1  is a side view of a small crop duster airplane with an irregular shaped payload hopper having a magnetostrictive linear displacement transducer for determining the volume of a liquid agricultural product located in the irregular shaped payload hopper that is displayed on a digital quantity gauge in accordance with the principles of the invention; and 
           [0015]      FIG. 2 , is a block diagram of the present invention. 
       
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENT 
       [0016]    Referring to  FIG. 1 , there is disclosed a side view of a small crop duster airplane with an irregular shaped payload hopper having a Magnetostrictive Linear Displacement Transducer (MLDT) for determining the volume of a liquid agricultural product located in the irregular shaped payload hopper that is displayed on a digital quantity gauge in accordance with the principles of the invention. 
         [0017]    The present invention is a quantity system and method that uses an MLDT to determine the liquid volume in the payload hopper of an airplane. The MLDT transmits the height reading of the liquid to a converter/display located in the cockpit. The converter/display filters the signal, thereby removing the sloshing in the signal, and converts the filtered height to a volume that appears on a digital display. 
         [0018]    The MLDT possesses a single physical wear point, the float. Utilizing this mostly solid state electronic system increases the total reliability of the system. The MLDT system has an additional advantage in that there is no mechanical limitation to the resolution that the MLDT can give. Taking advantage of the higher resolution and combining this with a calibrated filter and signal converter allows the precise quantity of liquid product in the payload hopper to be digitally displayed on a gauge. 
         [0019]    The device is comprised of the following: 
         [0020]    An agricultural aircraft payload hopper  12  which contains a liquid agriculture product. 
         [0021]    A probe float  14  which floats on the surface of the liquid agriculture product in a payload tank in the airplane that may be square, round, rectangular, irregular, etc. 
         [0022]    A Magnetostrictive Linear Displacement Transducer (MLDT) tubular member  16  that senses the height of the probe float. 
         [0023]    Filtering electronics  18  which receives a signal from the magnetostrictive linear displacement transducer and smooths out the height signal. 
         [0024]    Converter electronics  20  which receives the filtered height signal of the liquid in the irregular tank from the filtering electronics  18  of the liquid in the irregular tank and converts it to a tank quantity. 
         [0025]    A readout display  22  which is coupled to receive the signal from the converting electronics to show the quantity of liquid product in the irregular tank 
         [0026]    The agricultural aircraft payload hopper  12  is a storage tank mounted internally or externally on an agricultural aircraft which holds the liquid product that is to be sprayed on a field or farm from the air. The agricultural aircraft payload hopper  12  can be made of metal, plastic, or fiberglass and the shape may be a simple geometric shape, but more commonly has a complex shape with a drafted bottom. 
         [0027]    The probe float  14  consists of a buoyant member such as wood, Styrofoam, or a sealed metal member which is less dense than the liquid in the tank being measured so that it can mark the position or height of the liquid in the tank. The float contains a permanent magnet whose position is sensed by the MLDT  16 . 
         [0028]    The Magnetostrictive Linear Displacement Transducer (MLDT)  16  is a distance measuring device. It uses magnetostrictive technology to sense the distance the permanent magnet in the float is away from the head or end of the MLDT. 
         [0029]    The filtering electronics  18 , a circuit which is known by one having ordinary skill in the art, is an electrical circuit that is used to smooth the signal from the MLDT sensor. For example, to filter an analog signal a resistor capacitor circuit, an inductor capacitor circuit, a single capacitor or any other filter known in the art may be used. Filtering a digital signal is typically done using a program which is known by one having ordinary skill in the art. For example, this may be by averaging the digital readings over a set period of time or using a statistical analysis to remove the highs and lows to smooth out the signal, or any other currently used digital signal filtering. 
         [0030]    In an embodiment the filtering electronics  18 , converter electronics  20 , and digital display, which are shown as separate components may be combined in a single microprocessor which would simplify the electronic lay out. 
         [0031]    In an embodiment of the present invention, on takeoff the reading of the quantity of fluid in the agricultural aircraft payload hopper tank is automatically switched from ground attitude to level-flight attitude. This change automatically changes the scale of the signal from the converting electronics to account for pitch attitude changes of the airplane. In operation the engine gauges are used to determine if power is being produced. When the airplane is on the ground and the engine is at idle, the quantity gauge is in its ground mode. As soon as the throttle is moved to demand power the engine torque gauge show this change. The quantity gauge detects this change in the engine torque gauge and goes to level flight mode. It is understood that other indicators can be used to indicate that the airplane is in flight mode such as checking if the prop knob is in feather, checking the airspeed indicator and selecting flight mode based on the airplanes speed. 
         [0032]    Ground mode and level flight mode are not just different tables to convert float height to quantity. The mode also selects the filter that is to be used. In flight there is more movement of the airplane and the chemical is dispensed at a slower rate. Therefore, a larger filter may be needed or wanted. In ground mode the airplane is normally stationary while it is being loaded and the load is put in the airplane at a fast rate so a smaller filter may be needed or desired for a faster response. 
         [0033]    In another embodiment the brightness of the display in the cockpit is adjustable. This can be done using a dimmer, such as a rheostat or a push button switch to select two or more different levels of brightness, or any other adjustment method known in the art. 
         [0034]    In another embodiment a second display may be mounted in a location for an aircraft loader to see. 
         [0035]    Referring to  FIG. 2 , there is shown a block diagram of the present invention. The embodiment shown in the drawing includes a single agricultural aircraft payload hopper tank  12  with an MLDT  16  mounted within the tank. Depending upon the fluid level in the agricultural aircraft payload hopper tank  12 , the probe float  14  which contains a permanent magnet whose position is sensed by the MLDT moves up or down along the MLDT  16 . The Signal from the MLDT  16  is sent through filtering electronics  18  to converting electronics  20  and then to the digital readout display  22 . 
         [0036]    In an embodiment the signal may be first sent to the converting electronics  20  and then to the filtering electronics  18 . 
         [0037]    The filtering electronics  18 , converting electronics  20 , and digital readout display  22  may be placed in individual boxes and located throughout the aircraft. The most space saving variation for the cockpit area would be to mount only the digital readout display  22  in the cockpit, with the converting electronics  20  and filtering electronics  18  elsewhere in the aircraft. 
         [0038]    In operation, the probe float  14  is on the surface of the liquid in the agricultural aircraft payload hopper tank  12 . The MLDT  16  sends a signal of the height of the probe float  14  through conducting wires to the filtering means  18  and the converting means  20  where the signal is processed and then to the display means  22  which shows the quantity of fluid in the tank. 
         [0039]    The Filtering electronics  18  smoothes out the sloshing of the liquid in the agricultural aircraft payload hopper tank  12  so that the digital readout display  22  shows a stable quantity. The converting means  20  converts the height of the probe float  14  in the agricultural aircraft payload hopper tank  12  to the quantity of liquid in the agricultural aircraft payload hopper tank  12 . 
         [0040]    In an embodiment of the present invention the output of the magnetostrictive linear displacement transducer  16  can be an analog output of the level of fluid in an agricultural aircraft payload hopper tank  12  where the analog output of the MLDT  16  is fed to the filtering electronics  18  which can be a ten micro farad capacitor located across the analog inputs. The signal across the capacitor is converted with a map function which scales the analog input signal to a quantity of fluid in the tank which can be used to control a seven segment LCD display. In an embodiment of the invention the analog signal can be fed to a multi-meter to display the readings. 
         [0041]    Prior art systems utilize either: A) A full mechanical system that use a float connected thru additional linkages to a mechanical gauge which is prone to linkage wear which results in backlash and resolution loss, B) An electrical system such as a resistive potentiometer, rotary encoder, or reed switch, which has electrical contact wear points, which limit the reliability of the gauge and the resolution that can be displayed. 
         [0042]    In the present invention there are no moving parts aside from the probe float which increases the reliability of the system in the physically rugged environment of agricultural aircraft. In addition, the present invention has a 0.001 inches resolution capability which is far superior to the current agriculture aircraft industry systems, such as the reed switch system that has a resolution of 0.375 inches. This gain in resolution allows for increased precision of the display. 
         [0043]    While there have been shown and described and pointed out the fundamental novel features of the invention as applied to the preferred embodiments, it will be understood that the foregoing is considered as illustrative only of the principles of the invention and not intended to be exhaustive or to limit the invention to the precise forms disclosed. Obvious modifications or variations are possible in light of the above teachings. The embodiments discussed were chosen and described to provide the best illustration of the principles of the invention and its practical application to enable one of ordinary skill in the art to utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated All such modifications and variations are within the scope of the invention as determined by the appended claims when interpreted in accordance with the breadth to which they are entitled.