Patent Abstract:
A time and labor saving device used in the aviation refueling process for holding an aviation style fuel nozzle in place over a open vessel so that the filter screen may be easily inspected while additionally providing for the collection and recycling of fuel that is lost while inspection is made.

Full Description:
[0001]    This application claims benefit of provisional application No. 60/881,176 filed on Jan. 19, 2007 
     
    
     FIELD OF THE INVENTION 
       [0002]    The present invention relates to improvements in the process and procedures for the inspection and replacement of fuel filters and/or filter screen specifically used in aircraft refueling operations at airport ground fueling stations as specifically set forth in the Air Transport Association otherwise known as ATA. The ATA specifications are the results of 12 international industry associations who represent airlines, manufacturers, suppliers and repair agencies associated with the airline industry. 
         [0003]    An additional feature of the invention is in the reclaiming and reuse of aviation fuel within the considerable length of hose that extends from the fueling truck to the aircraft when said hose must be removed for inspection and or replacement. There can be large amounts of aviation fuel remaining in the fuel line that can be potentially lost during the required hose replacement process. This invention allows for this fuel to be reclaimed in a novel and efficient manner wherein the hose is attached via the Underwing Nozzle to the invention to allow venting during this process. 
       BACKGROUND OF THE INVENTION 
       [0004]    ATA Specification  103  identifies certain quality inspection procedures and safety tests commonly used at storage and transportation facilities that handle jet fuel. It also includes certain forms designed to record performance of the appropriate tests and inspections. All aviation refueling operations must comply with these procedures. 
         [0005]    ATA Specifications are created by the airline industry to revolutionize the multi-billion dollar aviation parts business; ATA Specifications are a comprehensive set of specifications, products and services that are designed to overcome challenges that have plagued the industry for decades. 
         [0006]    Widely used by the world&#39;s airlines and suppliers, the system has served the industry for more than 40 years and has evolved to embrace the latest technological advances in information exchange, by streamlining business and operational processes and reducing administrative costs. 
         [0007]    ATA specifications have grown to become the backbone of the aviation industries current process and quality controls. As a result, the industry has attributed significant operational efficiencies and cost savings to ATA specifications. 
         [0008]    Among one of these very important procedures that must be carried out on a routine basis is the inspection and replacement of a fuel filter screen assembly that resides in the Underwing Nozzle. The filter screen acts as the final fuel filtering component before aviation fuel enters the aircraft. The fuel screen comprises of a non-bypassable 100 mesh nozzle/connector screen formed in a cone and affixed to a ring with a snap and or removal apparatus. 
         [0009]    Specifically, Specification  103  states that each Underwing Nozzle fuel screen be examined for particles or other solid contaminants and furthermore states that if particles are found that the operator is to investigate possible sources of contamination. Specification  103  additionally requires a form to be filled out to document the inspection and that the form is retained for 12 months. There are several manufacturers of the Underwing Nozzle and this predominate nozzle is utilized worldwide by more companies and at more airports than any other nozzle. Tens of thousands of these nozzles are used on a daily basis for commercial aviation refueling, military operations and private jet refueling. 
         [0010]    Current operations for inspection and changing this fuel screen assembly include one person holding the Underwing Refueling Nozzle while another person facilities the operation of disconnecting the hose from the Underwing Refueling Nozzle to inspect the filter screen assembly. 
         [0011]    During this operation the aviation fuel within the hose and nozzle are lost or otherwise spilt upon the ground. Some airport refueling operators will perform this operation over a bucket in the attempt to catch some of the fuel. 
         [0012]    While lost fuel is expected in current inspection operations there is the danger that particles and/or other contamination that could be from inner hose lining, pipe rust, sand, low point sediment, equipment failure, seals, gasket, etc. will be flushed out with the loss of fuel and that early detection of contamination indicators will not be apparent, as they are lost with the spilt fuel. 
         [0013]    In most cases the fuel is lost and spilt on the ground causing both environmental and fire hazard concerns for airport operators. Said fuel can also be splashed or otherwise spilled on the operators during this inspection procedure. 
         [0014]    Even the manufacturer of the Underwing Nozzle acknowledges this problem and states in their catalogs that with a standard nozzle/hose system, the hose must be drained to accomplish checking the filter. 
         [0015]    Even if additional steps are utilized to prevent this problem such as using a commercially available Dry Break apparatus instead of the standard quick disconnect, the fuel in the nozzle still needs to be caught during the inspection of the filter screen and the fuel are typically spilt upon the ground. 
         [0016]    An additional important feature of the invention is in the hose replacement process of the fueling truck wherein the pumping action of the fuel truck is reversed to become a vacuum or suction action to drain the fuel hose contents back into the fuel truck tank. 
         [0017]    While the Underwing Nozzle is attached to the invention the nozzle poppet valve remains open while the hose is redirected to the suction side of the truck pump from the pumping or discharge side for the purpose of draining the fuel hose. 
         [0018]    The present operation procedure includes operators manually opening a poppet valve on the Underwing Nozzle so that fuel can be removed from up to fifty feet of hose. This operation can typically require more than one operator to perform. 
         [0019]    A poppet valve on a Underwing Nozzle will consist of a hole, usually round or oval, and a tapered plug, usually a disk shape on the end of a shaft, sometimes called a valve stem. This valve must be opened to allow suction from the Underwing Nozzle for reclaiming the fuel contents from the volume of the hose to the fuel truck tank. 
         [0020]    The invention as described herein allows for one person to perform this operation thus saving additional man hours while also creating a more efficient operational procedure. 
       SUMMARY OF THE INVENTION 
       [0021]    An object of the present invention is to remedy this problem of spilt fuel and to further more improve the quality control process by allowing for one individual to perform this operation instead of the present practice of utilizing two people, thus saving man hours and resources. 
         [0022]    The improved process allows for quicker and more efficient operation while saving the fuel for further inspection and proper disposal. This procedure will also eliminate the unnecessary spillage of aviation fuel on the ground where it can seep into the groundwater causing environmental and safety concerns. 
         [0023]    In accordance with the present invention an improved and novel means of checking the aviation refueling nozzle fuel screen is preformed by providing a container or fuel receptacle for the purpose of receiving fuel lost during the inspection procedure. 
         [0024]    Said container having disposed within its central opening a annular bayonet connector with a central drain to container mounted at an angle thus providing a complementary configuration to receive and engage an underwing nozzle wherein said nozzle is easily connected and held in place so that an operator can break apart the filter screen connection and make required inspections and replacement. 
         [0025]    The invention as described, allows for the procedure to be reduced from a two man operation to a one-man operation while also collecting the spilt fuel for recycling and safe removal. 
         [0026]    Once the Underwing Nozzle is serviced, the nozzle is quickly re-connected and put back into service and the container can be easily removed and drained of contaminates and fuel. 
         [0027]    Additionally, during the fuel hose replacement process one operator can now connect the Underwing Nozzle to the invention thereby mechanically opening the poppet valve so that the same operator can then also operate the suction controls for removing the fuel from the hose length. 
         [0028]    Said invention taking the place of a second operator that would normally have to physically open the poppet valve or otherwise disconnect the dry break to allow for air to be vented or otherwise sucked into the hose for the operation to be completed. The invention additionally collects the fuel that is lost during the operation of removing the Underwing Nozzle from the fuel hose. 
         [0029]    From the foregoing, it will be apparent that the present invention provides for a novel and improved means for filter inspection and whereas the present invention has been described in a particular fashion, it should be understood that other and further modifications apart from those shown or suggested herein may be made within the scope of the invention. 
         [0030]    The foregoing and other objectives, features, and advantages of the invention will be more readily understood upon the consideration of the following detailed description of the invention. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0031]    The figures of the appended drawing will illustrate the manner in which the invention may be embodied. In these figures, identical references designate similar elements. 
           [0032]      FIG. 1  is a top plan view of the invention 
           [0033]      FIG. 2  is a Sectional View taken from  FIG. 1  as shown 
       
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENT 
       [0034]      FIG. 1  shows a plan view of the Aviation Refueling Filter Inspection Apparatus  10  comprising a canister, bucket, or container  12  having a plurality of openings  14  near the upper most part of the container near the proximity of the top rim. 
         [0035]    Said openings  14  for the purpose of and designed to facilitate the ease of transport and to make it easy to carry the invention  10  to desired locations. Ease of transport is important, as filter screen inspection is typically preformed on the airport tarmac or at other fueling locations requiring that the invention be portable. 
         [0036]    Openings  14  additionally providing a lighter weight unit and additionally providing for attachments and or hooking means for attaching invention  10  on a refueling truck or like transport vehicle. 
         [0037]    Container  12  shall be constructed of a rigid material suitable for the retaining of aviation fuel or like liquids and may be constructed of aluminum, steel, plastic, or other suitable material so the invention  10  can be lightweight and rugged in construction. The invention  10  shall have a general rectangular form or like shape. 
         [0038]    The front portion  20  of container  12  shall have a configuration similar to that of a bow or a front section of a boat or ship and shall come to a point  30  so that fuel shall be easily directed when it is poured from the container  12  to other receptacles (Not Shown). The front portion  20  of the container  12  thus creates a configuration that may be more easily identified for quick alignment of the Underwing Nozzle  28  shown in  FIG. 2  utilized in refueling aircraft. 
         [0039]    Container  12  shall be affixed or otherwise mounted to a rigid base support  16  with said base  16  extending beyond the front of the container  12  a number of inches so that an operator may apply their feet to the base support  16  for supporting and to steady the invention  10  during operations as may be required. 
         [0040]    Container  12  shall also have an extension of the base  16  on each side of the container  12  as required comprising a set of tabs  24  wherein tabs  24  are centrally located for applying additional foot support as may be required. 
         [0041]    Additionally, base support  16  shall have a plurality of openings  18  for the purpose of removing weight from the invention  10  and to further facilitate a fastening or mounting means for ease of transport. 
         [0042]    Container  12  shall also have centrally affixed within the void or open chamber of the container  12  a adapter plate  22  affixed or otherwise connected to the rear portion or rear wall  32  and shall furthermore be connected to the bottom of container floor  34  of the container  12  so as to form angled alignment shown more clearly in  FIG. 2 . 
         [0043]    Adapter plate  22  shall have a centered or otherwise centrally disposed bayonet type engagement connection  36  for securing the complementary and mating connection to an underwing nozzle  28  Shown in  FIG. 2 . Bayonet type engagement connection  36  comprising of a hollow extension tube  38  with a wall thickness suitable for drilling mounting holes  40 . Said bayonet connector  36  mounted directly over adapter opening  26  allowing for fuel to flow into container  12 . 
         [0044]    Hollow extension tube  38  shall be welded or otherwise affixed to the brace  22  in any suitable manner so that it will remain rigid. Extension tube  38  shall have on the top circumference a plurality of tapped holes  40  for attachment of a bayonet connector  36  designed to match a 3-lug international standard aircraft adapter that is utilized on aircraft fueling applications. 
         [0045]    Bayonet connector  36  shall be mounted to extension tube  38  with a plurality of commercially available bolts  44  as required. Bayonet connector  42  providing for a quick connect and disconnect with an Underwing Nozzle  28 . Bayonet connector shall be of a complementary design to mimic or reproduce the International Standard Aircraft Bayonet Type Coupler connection. 
         [0046]    Bayonet connector  36  furthermore having a plurality of mating lugs or prongs  42  extending radially outward from its circumference and a plurality of indexing slots  46  therein configured and dimensioned for complementary mating insertion into the Underwing Nozzle  28  wherein said mating lugs are slidably inserted and engagable by turning the Underwing Nozzle  28  a predetermined degree to form a locking connection between the bayonet connector  36  and the Underwing Nozzle  28 . 
         [0047]    Said connection facilitates the positioning of the Underwing Nozzle  28  so that it is now positioned and ready for a quick disconnect of the hose or dry break for inspection of the filter screen providing for a new and improved method of inspection utilizing only one person. Fuel that is lost in the inspection falls into the container  12  for easy removal and inspection for contamination. 
         [0048]    It maybe thus seen that the objects of the present invention set forth, as well as those made apparent from the forgoing description are efficiently attained. While preferred embodiments of the invention have been set forth for purposes of disclosure, modifications of the disclosure embodiments of the invention as well as other embodiments thereof may occur to those skilled in the art accordingly. The appended claims are intended to cover all embodiments that do not depart from the spirit and scope of the invention.

Technology Classification (CPC): 5