BACKGROUND OF THE INVENTION
[0001] This invention relates to spraying apparatus and more particularly to a unique nozzle
extension for use in combination with a spray gun to facilitate spraying of a polymeric
material into an enclosed cavity to completely coat the interior surfaces thereof
and thus form an integral leak-proof fuel container such as, for example, an in situ
formed fuel tank.
[0002] While the invention is developed for spray- coating integral aircraft fuel tanks,
ie, tanks in situ formed within the fuselage or wing cavities of an aircraft, it may
also be applied to any other type vehicle including automotive type vehicles wherein
the tanks are formed within the body framework of the vehicle.
[0003] According to the prior art practice of fuel tank manufacture as it pertains to aircraft,
such tanks are made as a single complete unit and thereafter installed into an enclosed
cavity provided for it within the confines of the aircraft framework. Tanks of the
type alluded to are made by various techniques wherein fuel resistant polymeric coatings
are applied to reinforcement fabric, the fabric being firstly laid up onto a mold
and/or mandrel which approximates the configuration of the cavity into which the tank
is to be installed. Obviously, the volume capacity of a tank made according to this
practice is determined by and dependent upon how closely one is able to make the tank
fit the cavity configuration.
[0004] Recent improvements in fuel resistant materials, and more particularly with respect
to air-curable polyurethane elastcners, have made it feasible to make fuel tanks which
are an integral part of the vehicle. This type of tank is an attractive alternative
to the prior art tanks in that the total enclosed volume space provided for the tank
is utilized for fuel storage.which obviously allows for greater fuel capacity in a
particular aircraft while also decreasing the weight of such prior art fabric-reinforced
tanks. Exemplary of polyurethanes alluded to are these disclosed in U.S. Patent No.
4,247,678 assigned to The Goodyear Tire & Rubber Company, Akron, Ohic and also in
co-pending applications Serial Numbers 502,832 and 502,867 both of which were filed
on June 9, 1983.
[0005] While these polyurethane materials and/or cements have proved effective for in situ
formed fuel tanks, various areas of the tank cavity are difficult, if not impossible,
to cover using conventional spraying apparatus. Difficulty is especially encountered
in such areas as the nooks and corners of the tank cavity and around access ports
provided through the cavity for various controls such as hydraulic and/or electrical
lines. Furthermore, it is extremely difficult to spray-coat the back sides of fasteners
such as screws, bolts, nuts and the like which are used in fabricating the aircraft
even though personnel may be able to crawl into the larger fuselage tank cavities,
with the spraying equipment.
[0006] It is therefore in accordance with one aspect of the present invention an object
to provide spraying apparatus that dispenses a substantially precise volume of particulate
elastomeric material which when evenly dispersed over the surfaces of the cavity and
cured, provides a substantially leak-proof in situ formed fuel tank within the confines
of the vehicle body. cavity.
SUMMARY OF THE INVENTION
[0007] Various aspects and advantages of the invention are achieved in a nozzle extension
unit for use in combination with a spray gun when dispensing a sprayable polymeric
material into an enclosed cavity having limited accessibility comprising an input
connector for attachment of the unit to the spray gun, a nozzle tip including roll
and yaw rotatable swivels, at least one filter screen element mounted in-line within
the unit, and a length of flexible high pressure hose interconnecting the input connector
to the nozzle tip.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] An appreciation of the inventive concept and the attendant advantages thereof will
be readily understood by reference to the following description when considered with
the accompanying drawings in the several figures in which like reference numerals
designate like parts and wherein:
FIGURE 1 is a perspective view, in section, of a portion of the body framework of
a typical aircraft forming a wing tank cavity illustrating the complexity of the tank
as it includes various fasteners, wall sections, and the like within the confines
of the cavity;
FIGURE 2 is a perspective view of a spray gun extension nozzle forming the basis of
this invention as it may be attached to a state-of-the-art airless spray gun (shown
in ghost lines); and
FIGURE 3 is an elevational view, in partial section, of the nozzle extension shown
in Fig. 2 illustrating the specific arrangement of the elements thereof.
DETAILED DESCRIPTION OF THE PREFERRED
EMBODIMENT
[0009] Referring to Figure 1 of the drawings, a portion of a typical aircraft wing tank
is illustrated and generally indicated by reference numeral 10. Tanks of this type
are formed within the framework of the wing structure and typically comprise a top
plate 12, a bottom plate 14, and a plurality of walls 16 that interconnect the top
plate to the bottom plate. The walls 16 are attached to the top and bottom plates
via a plurality of rivets 18 and/or bolt-and- nut fasteners 20 which extend through
flange portions 16a of the wall 16. A plurality of transversely extending walls 22
may also be included in the structural configuration and these will typically have
a plurality of apertures 24 which decrease the weight of the structure as well as
permit fuel to flow between various compartments formed by the intersecting walls
16 and 22.
[0010] Figure 1 is intended to illustrate the problem involved in attempting to seal the
interior spaces of this type complex-shaped structure and, because access into the
tank cavity is limited, it becomes an exercise in futility to attempt to spray-coat
all surfaces within the cavity using conventional spraying equipment. While aircraft
fuselage tanks are larger and provide somewhat greater access, fuel leakage from these
tanks cannot be tolerated inasmuch as the control functions of the aircraft are located
within the fuselage. Therefore, it is imperative that the tank does not leak when
attempting to in situ form such tank within the fuselage cavity. For this reason,
aircraft fuselage tanks have conventionally been made as separate units which are
leak tested prior to their installation into the aircraft framework assembly.
[0011] The present invention provides a nozzle extension for attachment to and use with
a state-of-the-art spraying apparatus which allows personnel to direct a fuel resistant
polyurethane elastomer into the most inaccessible areas of an aircraft fuel tank cavity.
More specifically, the invention provides a unique "spray finger" unit that duplicates
the swivel motion of a person's wrist and therefore allows complete freedom of spraying
motion within enclosed spaces such as within aircraft wing and fuselage tank cavities.
[0012] The apparatus forming the present inventive concept is illustrated in Figure 2 as
it may be affixed to and operated in conjunction with a typical spray gun apparatus
illustrated in ghost lines and generally indicated by reference numeral 26. The spray
gun 26 is adapted for receiving various chemical components and/or materials which
comprise the composite of the finished fuel tank and these enter the gun at "A", are
controlled through a valve assembly at "B", and exit through a nozzle at "C".
[0013] The nozzle extension is generally indicated by reference numeral 100 and comprises
a length of flexible high pressure hose 40 interconnecting a connector 30 at one end
to the "spray finger" nozzle unit 50 at the opposite end. More particularly now with
reference to Figure 3 of the drawings, the nozzle extension 100 is illustrated in
an elevational view with various portions shown in longitudinal cross-section and,
because of its overall length, the figure is separated into the three sections 30,
40, and 50 which are interconnected by a dot-dashed line 101 to indicate the manner
of assembly. Dot-dashed line 101 is also the axis of rotation A of various in-line
swivels forming an integral part of the unit 100 and these will be described more
specifically hereinafter.
[0014] The connector 30 is such as to be readily attached to the output of the gun 26 at
"C" and comprises a body 32 having a female threaded end 34 that threads onto the
spray gun 26. The opposite end comprises a male threaded nipple 36 that defines a
bore or chamber 32a that carries a relatively course 50 mesh filter screen element
38 therein in an axially in-line positon within the chamber. The screen element 38
also includes a washer end 38a which effects a seal at the output of the chamber 32a.
The filter screen effectively breaks up any large lumps of spray material that may
exit through the spray gun 26.
[0015] Interconnection of the input filter connector 30 to the output nozzle unit 50 is
accomplished through a length of flexible hose generally indicated by reference numeral
40. The hose section 40 may be of any length and comprises a flexible, high pressure,
wire-braided rubber hose 42 having an axially in-line swivel connector 44A at the
input end of the hose and substantially similar in-line swivel connector 44B at the
output end thereof. The swivels 44A and 44B include female threaded nuts 46A and 46B
and these are mounted on flanged nipple ends 48A and 48B respectively. The swivels
44A and 44B are sealed by 0-ring seals 47A and 47B in a conventional manner. Input
swivel 44A further includes a second female threaded nut 49 that adapts to the male
nipple 36 of the filter connector 30. The swivel connectors 44A, 44B are conventional
connections and eliminate kinking of the wire braid hose 42 when the hose section
40 is connected to the gun 26 and nozzle unit 50.
[0016] The output connecting nut 46B of the hose section 40 is adapted for threading engagement
with a high pressure in-line axial swivel indicated by reference numeral 52. The swivel
52 is a product of the Spraying Systems Company of Wheaton, Illinois. The swivel 52
is a sealed unit and the specifics of the elements forming the swivel are not important
for this description suffice to say that it is designed for swivel operation at high
pressures. The section 52 also includes a female threaded nut 54 at the output end
that threads onto a second in-line filter connector 56.
[0017] The connector 56 comprises input and output threaded nipple ends 56A and 56B respectively.
The output end 56B defines an enlarged bore or filter screen chamber 56a that carries
a screen element 58 therein in axial in-line position within the chamber 56a. The
screen element comprises a plurality of serially connected dises having openings therethrough
of approximately 0.020 inch (.51 mm) and further includes a washer type end 58a that
effects a sealing relationship with the end of the chamber in the usual manner.
[0018] The nozzle section 50 further comprises a "yaw swivel" generally indicated by reference
numeral 80. The swivel 80 comprises an upper or input body portion 60 that is connected
in swivel relationship to a lower or output body portion 70. The two body portions
60, 70 define chamber bores 60a and 70a respectively which have a common "yaw" swivel
axis Ay. The upper body portion 60 includes an input bore 62 that is defined by a
flanged nipple 64 which carries a mounted female threaded nut 66 thereon for attachment
to the nipple end 56B of the filter connector 56. The lower body portion 70 includes
an output bore 72 that is defined by a male threaded nipple end 74 which also defines
a filter chamber 74a. The upper input body portion 60 and lower output body portion
70 are joined at 76 such that the portion 70 swivels with respect to the body portion
60 about the "yaw" axis A. The two body portions 60, 70 are maintained in their swivel
relationship by a swivel bolt 82 that is captured in the bore 70a by its head portion
82a and in the bore 60a by a cap nut 84. The cap nut 84 is threaded onto the end 82b
of the bolt 82. The swivel alignment of the bolt 82 is maintained in the upper body
60 by a flange 82c that also effectively seals that end of the bore 60a. The upper
and lower bores 60a and 70a are further pressure sealed by seals 68 and 78 respectively.
[0019] The output nipple 74 of the body portion 70 houses a combination filter screen/check
valve element 88 which is axially positioned within the chamber 74a and it includes
a washer end 88a that seals the output end of the chamber. The element 88 comprises
a 100-mesh screen 83 that encircles a ball check valve comprised of a spring that
forces a ball to close off the output orifice at a predetermined low pressure.
[0020] An output tube 90 is connected to the yaw swivel 80 by a female threaded nut 92 which,
when threaded onto the nipple 74, effects the seal as between the filter washer 88a
and the end of the chamber 74a. The tube 90 is bent to an angle "α" of approximately
120 degrees with respect to the rotational axis A and it includes a small nozzle tip
94 that is threadably received on the end of the tube. The nozzle tip 94 comprises
a nozzle disc 96 having a spray orifice and a seal disc 98 and this is a conventional
arrangement.
[0021] From the foregoing description it should now be appreciated that an operator may
move the spray nozzle 50 in any desired direction and/or angle to direct a spray of
material with one hand while operating the spray gun 26 with the other hand. The in-line
high pressure swivel 52 provides rotation about the A
r roll axis of the nozzle unit 50 while the swivel 80 provides rotation about the A
y yaw axis. In addition, the flexible hose 42 provides pitch motion ability about the
A pitch axis.
[0022] In the operation of the apparatus 100, in-line filter elements 38, 58, and 88 break
up and/or filter out any pigment lumps that exist in a polyurethane cement as may
be used for in situ formed fuel tanks. Such lumps have been a source of aggravation
with conventional spraying equipment. Further, the check valve of the element 88 shuts
off the flow of spray material at the nozzle tip 50 when the spray gun 26 is shut
off and the internal pressure drops below a specific value. This shut off at the tip
end of the unit 100 eliminates continued dripping of material out of the tip orifice
94 since the entire length of the nozzle extension unit 100 contains spray material.
[0023] While the invention may be used at pressures up to 4,000 psi, its best configuration
includes a nozzle disc 96 having an orifice opening of about .009 inch (.23 mm) and
operating at a pressure of about 900 psi. This combination provides a very uniform
coating of polyurethane cement. Of course other nozzle openings within the range of
.005 to .020 inch (0.13 mm to 0.5 mm) may also be applied with attendant variations
in the operating pressure and these will be determined by experience depending upon
the type of material being dispensed through the apparatus.
1. A nozzle extension unit for attachment to and use in combination with a spray gun
to provide pitch, roll, and yaw motion when dispensing a sprayable polymeric material
into an enclosed substantially inaccessible cavity characterized by:
an input connector for attachment to the spray gun and having an in-line positioned
filter of 50 mesh screen mounted therein;
a nozzle tip having in-line positioned roll and yaw axis mounted swivels, a spray
orifice at the output end of a length of tubing bent at an angle with respect to the
roll axis, and at least one in-line positioned filter of 100 mesh screen mounted therein;
and
a length of substantially flexible high pressure hose interconnecting the input connector
to the nozzle tip to flexibly extend the nozzle tip a specific distance away from
the spray gun.
2. The nozzle extension unit as set forth in Claim 1 further characterized by a second
in-line positioned filter of 100 mesh screen mounted within the nozzle tip.
3. The nozzle extension unit as set forth in Claim 1 further characterized by an in-line
positioned valve mounted within the nozzle tip to stop the flow of polymeric material
out of the spray orifice when the internal pressure within the unit drops below a
predetermined value.
4. The nozzle extension unit as set forth in Claim 1 wherein the angle of the bent
tubing which carries the spray orifice is approximately 120 degrees with respect to
the roll axis of the unit.
5. The nozzle extension unit as set forth in Claim 1 characterized by a spray orifice
within the range of 0.13-0.5mm (.005-.020 inch).
6. The nozzle extension unit as set forth in Claim 1 characterized by a spray orifice
of approximately 0.23mm (.009 inch).