Information
-
Patent Grant
-
6379200
-
Patent Number
6,379,200
-
Date Filed
Friday, July 21, 200024 years ago
-
Date Issued
Tuesday, April 30, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Ziolkowski; Timothy J.
- Cook & Franke SC
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CPC
-
US Classifications
Field of Search
US
- 137 588
- 137 56534
- 123 509
- 123 514
- 123 510
- 123 541
- 440 88
- 220 414
- 280 834
-
International Classifications
-
Abstract
A fuel storage and supply apparatus (22) for a watercraft (10) incorporating a plurality of connections (50,66) penetrating a housing (32) in a single opening in a fuel tank (12). Each connection is sealed by a radial O-ring (56,68) so that the connection may be rotated about a longitudinal axis without adversely affecting the seal. A single opening (34) in the tank may thereby be used to provide connections for a fill tube (66), fuel tube (50), vent (86), and electrical penetrations (150) for an intank pump (136) or level sensor (156).
Description
BACKGROUND OF THE INVENTION
The present invention relates generally to fuel supply systems, and more particularly to a fuel supply system for a watercraft and in particular, to a fuel tank having a plurality of sealed, rotatable connections formed through a single opening in the tank.
Present marine fuel storage and distribution systems typically include a fuel tank, a fuel conduit connected between an engine and the fuel tank, a pump for conveying fuel through the conduit, a priming pump, one or more filters for removing sediment and water from the fuel prior to its delivery to the engine, fill and vent tubes connected to the tank, a cap for the fill tube that may provide the venting function when installed, and instrumentation for providing a signal corresponding to the level of fuel within the tank. One or more of these components may be duplicated in watercraft having more than one engine, or for the purpose of improved capacity, flexibility or reliability.
It is known that each joint or connection in a fuel system is a point for potential leakage of liquid fuel and/or vapors. It is therefore desirable to minimize the number of connections within a fuel system. In particular, it is desirable to minimize the number of connection to a fuel tank, since the tank is an expensive component to fabricate and is often installed in a location that is not accessible for repair activities. Furthermore, since the tank provides the primary boundary for the containment of the fuel, it is desirable to make the tank as fail-safe as possible.
It is also known that the space requirements and layout of a fuel system are important parameters in the design of a watercraft. The location, number and capacity of fuel tanks and the layout of fuel and vent lines may not be known until the power unit(s) for the boat are selected. Accessibility for routine maintenance and servicing must also be considered when designing a marine craft fuel system.
BRIEF SUMMARY OF THE INVENTION
Thus there is a particular need for a fuel system for a watercraft that provides a high degree of flexibility for the marine designer. Such a fuel system should minimize the number of connections, and in particular, should minimize the number of penetrations into the fuel tank.
Accordingly, a fuel storage and supply apparatus for a watercraft is described herein as including: a fuel tank having an opening formed therein; a housing sealingly attached to the fuel tank within the opening, the housing having an opening formed therethrough; a tube disposed through the housing opening and longitudinally rotatable therewithin; and a radial O-ring seal disposed between a wall of the opening and an outside surface of the tube.
The tube of the watercraft fuel storage and supply apparatus is further described as including: a groove formed in the outside diameter surface of the tube for receiving and retaining the radial O-ring seal; a flange formed on the outside surface of the tube, the flange having a diameter greater than the diameter of the housing opening and having a bottom surface disposed against a top surface of the housing; and a clamping plate removably attached to the housing and covering at least a portion of the flange for retaining the tube within the housing opening.
The watercraft fuel storage and supply apparatus may further include: a valve cavity formed within the housing and in fluid communication between the interior and exterior of the tank; a check valve disposed within the valve cavity; a fuel outlet nozzle rotatably disposed within the valve cavity; and a radial O-ring seal disposed between the fuel outlet nozzle and a wall of the valve cavity. The check valve may include: a plate disposed within the valve cavity and sealed thereto about its perimeter; a hole formed in the plate for the passage of fuel therethrough; and an elastomer attached to the plate and extending therefrom to cover the hole, the elastomer operable to bend to permit fuel to pass out of the tank through the hole, and operable to seal the hole in the event of the flow of fuel into the tank.
BRIEF DESCRIPTION OF THE DRAWINGS
The features and advantages of the present invention will become apparent from the following detailed description of the invention when read with the accompanying drawings in which:
FIG. 1
is a schematic illustration of a boat having a motor and a fuel storage and supply apparatus.
FIG. 2
is a partial section view of a portion of the fuel tank of
FIG. 1
illustrating the single opening in the tank and rotatable fuel fill and delivery tubes sealed with radial O-ring seals installed into a housing in the opening.
FIG. 3
is a partial sectional view of an anti-siphon check valve built into a rotatable fuel fill tube sealed with a radial O-ring in a housing in the opening of a fuel tank.
FIG. 4
is a partial section view of a fuel tank having a single opening and an in-tank fuel pump and filter. The fuel outlet of the pump is directed to a rotatable fuel tube sealed with a radial O-ring seal into a housing in the opening. The housing also includes an electrical penetration operable to deliver electrical energy to the pump motor.
FIG. 5
is a partial section view of a fuel tank having a single opening and an in-tank fuel level sensor. Electrical connections to the sensor are made via an electrical penetration mounted to a housing in the opening. The housing also supports a rotatable fuel outlet tube sealed to the housing by a radial O-ring seal.
Similar structures illustrated in multiple figures may be designated by the same numeral in multiple figures.
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1
illustrates a watercraft
10
having an internal combustion engine
12
mounted in the interior of a boat hull
14
. A power unit drive train
16
extends through the transom
18
of the watercraft
10
to deliver power to a propeller
20
. This illustration can be recognized as representing the inboard/outboard style pleasure craft common in the watercraft industry, but one may appreciate that the apparatus described herein may be applied to any style of marine propulsion system, including inboard and outboard units. A fuel storage and supply apparatus
22
provides fuel (not shown) to engine
12
. The fuel storage and supply apparatus
22
includes a tank
24
, fuel supply lines
26
, a fuel fill tube
28
, and a fill tube cap
30
. The fuel lines
26
and fuel fill tube
28
are supported in a housing
32
mounted in a single opening
34
formed in tank
24
.
FIG. 2
is a more detailed illustration of a portion of the fuel storage and supply apparatus
22
of FIG.
1
. Housing
32
can be seen disposed within the single opening
34
of tank
12
. Housing
32
is illustrated as being threaded into an adapter
36
which, in turn, is fixedly attached to tank
12
within opening
34
. In one embodiment, tank
12
is formed by a blow molding process, wherein opening
34
is formed at the location of the blow pin used during the molding process. Adapter
36
includes precision dimensioned threads
38
formed along its inside diameter, and a flange surface
40
adapted to span the somewhat irregularly shaped opening
34
. Adapter
36
may be sealed to tank
12
by any process known in the art, such as by welding for the embodiment of a polyethylene blow molded tank
12
. Adapter
32
has formed on its exterior perimeter a series of threads
42
formed to mate with threads
38
of adapter
36
. Housing
32
may thereby be screwed into adapter
36
until its flange
44
abuts the upper surface of adapter flange
40
. A seal or gasket
46
may be disposed between the mating surfaces of adapter
36
and housing
32
. In this manner, housing
32
is sealingly and removably attached to the fuel tank
12
within the opening
34
.
Housing
32
may be formed to include any number of penetrations into the interior of tank
12
. In the embodiment illustrated in
FIG. 2
, housing
32
functions to support both fuel line
26
and fill tube
28
. Housing
32
includes an opening
48
formed therethrough for the passage of fuel tube
50
. The outlet
52
of fuel tube
50
is attached to fuel line
26
by any attachment scheme known in the art. An inlet end
54
of fuel tube
50
extends into the interior of tank
12
for attachment to a fuel tube extension (not shown) operable to draw fuel from proximate the bottom of tank
12
. Fuel tube
50
is sealed to housing
32
by a radial O-ring seal
56
. O-ring
56
may be any material known in the art to be functional in such an application, such as a rubber or fluorocarbon material. O-ring
56
is retained in position around the exterior of fuel tube
50
by being partially disposed within a groove
58
formed in the exterior surface of fuel tube
50
. The dimensions of the exterior of fuel tube
50
, the interior of opening
48
, and O-ring
56
are selected such that the O-ring provides an appropriate pressure seal against the leakage of fuel through the opening
48
around the exterior of fuel tube
50
. In most applications, the differential pressure across O-ring seal
56
will be no more than 10-15 psi, which is well within the design pressures of known radial O-ring seal designs. Advantageously, O-ring seal
56
permits fuel tube
50
to be rotated about its longitudinal axis within opening
48
without any degradation of the sealing function, thereby allowing the outlet
52
to be directed to any radial position. To restrain fuel tube
50
from vertical movement out of opening
48
, a locking plate
60
is secured by a fastener
62
to the housing
32
in order to restrain the vertical movement of flange
64
formed on the outside surface of fuel tube
50
.
Fill tube
66
is supported in housing
32
in a manner very similar to that of fuel tube
50
. A plurality of grooves
68
are formed on the outside diameter surface of tube
66
for receiving and retaining a plurality of parallel radial O-rings
70
. A flange
72
is formed on the outside diameter surface of tube
66
to have a diameter greater than the diameter of the opening
74
in which tube
66
is disposed. A bottom surface of flange
72
is held against a top surface
76
of housing
32
by clamping plate
78
. Clamping plate
78
is, in turn, held in position by fastener
80
threaded into the body of housing
32
. Clamping plate
78
covers at least a portion of flange
72
for removably retaining the tube
66
within the opening
74
of housing
32
. Fill tube
66
may be rotated about it longitudinal
1
axis to position its outlet
82
in any of a plurality of radial positions without affecting the functionality of the radial O-ring seal
70
.
FIG. 3
is a partial sectional illustration of an embodiment wherein both a fuel supply tube
84
and a vent tube
86
are rotatably mounted within a housing
88
which, in turn, is rotatably se led within an opening
90
formed in tank
12
. Radial O-ring
92
is disposed within a notch
94
formed in an exterior surface of housing
88
to provide the pressure seal against tank opening
90
. Cover plate
96
prevents the vertical movement of housing
88
and is removably attached to tank
12
by fasteners
98
. Vent tube
86
is rotatably sealed by O-ring
100
within vent opening
102
formed in housing
88
. Fuel supply tube
84
is rotatably sealed within fuel supply opening
104
by radial O-ring
106
. An anti-siphon check valve assembly
108
is formed to be integral to the housing
88
. A valve chamber
110
is formed in housing
88
and is in fluid communication with the fuel supply tube
84
and fuel inlet
112
. Check valve assembly
108
is disposed within the valve cavity
110
and includes a plate
112
sealed to housing
88
about its perimeter by gasket
114
. A plurality of holes
116
are formed in plate
112
to permit the passage of fuel from inlet
112
to fuel tube outlet
118
. An elastomeric disk
120
is attached to the plate
112
, such as by extending tang
122
through an opening
124
of plate
112
. Elastomeric disk
120
extends from the point of attachment to cover holes
116
along the upper surface of plate
112
. In this manner, elastomeric disk
120
is operable to bend upward to permit the flow of fuel out of tank
12
through inlet
112
and valve cavity
110
to outlet
118
of fuel tube
84
. However, in the event of any reverse flow through fuel tube
84
, elastomeric disk
120
is operable to be forced downward against the top of plate
12
, thereby covering holes
116
and terminating any such reverse flow. Elastomeric disk
120
may be any material known in the art and suitable for such an application, such as for example, rubber. Other styles of valves may be used, such as a spring loaded poppet valve having a predetermined opening pressure. Housing
88
and tubes
84
,
86
may be manufactured from any material compatible with the fuel to be used, and may preferably be a machinable plastic or injection molded material. As with previous embodiments, fuel supply tube
84
and vent tube
86
may be rotated about their respective longitudinal axes to position their respective outlets to any radial position without affecting the sealing function provided by O-rings
100
,
106
. Furthermore, the entire housing
88
may be rotated about a longitudinal axis without affecting the sealing function provided by O-ring
92
.
FIG. 4
is a partial cross-sectional illustration of another embodiment of a fuel tank
12
having an opening
126
formed therein, with a housing
128
disposed within opening
126
and containing a plurality of openings
130
,
132
for the installation of various components of the fuel storage and supply apparatus. A fuel tube assembly
134
may be rotatably installed within opening
132
in a manner similar to that described above. In this embodiment, a one-piece fuel pump assembly
136
including a pump and a motor apparatus is disposed within the interior of the tank
112
proximate the bottom
138
of tank
12
. A fuel line
140
is connected between an outlet of pump
136
and fuel tube assembly
134
. A replaceable fuel filter
142
is disposed within a fuel filter housing
144
attached at the inlet of pump
136
. In an alternate embodiment wherein no fuel pump and motor apparatus is installed within the tank
12
, the fuel filter
142
and housing
144
may be installed directly to the fuel line
140
. Electricity for pump
136
is provided via electrical lines
146
connected to the pins
148
of an electrical penetration assembly
150
disposed within opening
130
of housing
128
. Electrical penetration assembly
150
is rotatably sealed within opening
130
by radial O-ring seal
152
. It may be appreciated that the pump/motor
136
and filter assembly
144
may be preassembled onto housing
128
prior to its installation within opening
126
of tank
12
. The replacement of filter
142
may then be simply accomplished by the removal of cover plate
154
and housing
128
from tank
12
.
FIG. 5
illustrates an embodiment of tank
12
having an internally mounted fluid level sensor
156
disposed proximate an opening
158
in tank
12
. A housing
160
is rotatably sealed within opening
158
, and is removable to provide access to sensor
156
. Sensor
156
may be attached to tank
12
by a bracket
162
accessible through opening
158
. Electrical penetration assembly
150
, as previously described with respect to
FIG. 4
, provides power and/or signal connections for sensor
156
. Housing
162
may include one or more other openings for appropriate fluid, electrical, or penetration assembly
150
may be retained within opening
166
by the friction of O-ring
168
against the walls of opening
166
, or an additional mechanical means of retention (not shown) may be provided. In this embodiment, as with those described above, the use of a radial O-ring seal apparatus facilitates the rotational movement of the various fuel tank penetrations within housing
160
without adversely affecting the seal provided there between.
It may be appreciated that fuel storage and supply apparatus
22
of
FIG. 1
containing one or more of the features illustrated in
FIGS. 2 through 5
provides the designer of a watercraft
10
with improved flexibility of design when compared to prior art fuel storage and supply apparatus. For example, it is not uncommon for a manufacturer to design and to sell a watercraft that is complete in ever respect except for the selection of the power unit. A fuel tank may be supplied with the boat, however, the connections between the power unit and the fuel tank will remain incomplete until the power unit is later specified. Changes in the tank connections and routing of the fuel system lines is made more difficult by the fixed connections found on prior art fuel tanks. By using a housing having multiple penetrations with individually rotatable connections, a variety of optional power units may be accommodated into a previously installed tank assembly. Similarly, a single tank may be stocked for a variety of applications, with each application being accommodated by the use of a specifically selected housing assembly installed within a single standardized opening of the tank. Furthermore, the installation and maintenance of a watercraft fuel system may be simplified by the ability to rotate various connections to a fuel tank without adversely affecting the effectiveness of the fluid seal for those connections.
Thus, a method of assembling a watercraft may include the steps of providing a hull; providing a fuel tank having an opening formed therein; installing the fuel tank in the hull; assembling a power unit to the hull; selecting a fuel tank opening housing having connections corresponding to the power unit; installing the fuel tank opening housing into the fuel tank opening; and installing a fuel line between the housing and the power unit. This is especially useful if the manufacturer provides at least two different customer-specified power units for use in a watercraft, and the power units each require different fuel tank connections. By providing a plurality of corresponding tank opening housings, each fuel tank opening housing having connections corresponding to a respective one of the power units, the appropriate connections can be more easily installed after the tank is in place by simply installing the appropriate tank opening housing. Installation is further simplified by the ability to rotate the penetrations passing through the housing without adversely affecting the effectiveness of the O-ring seal.
It may be further appreciated that the use of a single housing having a plurality of rotatable connections will provide a simplified method and apparatus for the modification of the fuel storage and supply system of a watercraft. This may occur, for example, in the event that a pressurized fuel system is approved for use on a watercraft that had previously utilized a suction fuel system. A modification kit may be assembled including an in-tank pump and an appropriate housing assembly having multiple fuel supply, vent fill, and electrical connections, as appropriate.
While the preferred embodiments of the present invention have been shown and described herein, it will be obvious that such embodiments are provided by way of example only. Numerous variations, changes and substitutions will occur to those of skill in the art without departing from the invention herein. Accordingly, it is intended that the invention be limited only by the spirit and scope of the appended claims.
Claims
- 1. A watercraft fuel storage and supply apparatus comprising:a fuel tank having an opening formed therein; a housing sealingly attached to the fuel tank within the opening, the housing having an opening formed therethrough; a tube disposed through the housing opening and longitudinally rotatable therewithin; a radial O-ring seal disposed between a wall of the opening and an outside surface of the tube.
- 2. The watercraft fuel storage and supply apparatus of claim 1, further comprising:a fuel line attached to the tube and extending to a bottom portion of the tank; a replaceable fuel filter attached to the fuel line.
- 3. The watercraft fuel storage and supply apparatus of claim 1, wherein the housing is attached to the fuel tank by a threaded connection.
- 4. The watercraft fuel storage and supply apparatus of claim 1, wherein the tube further comprises:a groove formed in the outside diameter surface of the tube for receiving and retaining the radial O-ring seal; a flange formed on the outside surface of the tube, the flange having a diameter greater than the diameter of the housing opening and having a bottom surface disposed against a top surface of the housing; a clamping plate removably attached to the housing and covering at least a portion of the flange for retaining the tube within the housing opening.
- 5. The watercraft fuel storage and supply apparatus of claim 1, further comprising:a valve cavity formed within the housing and in fluid communication between the interior and exterior of the tank; a check valve disposed within the valve cavity; a fuel outlet nozzle rotatably disposed within the valve cavity; and a radial O-ring seal disposed between the fuel outlet nozzle and a wall of the valve cavity.
- 6. The watercraft fuel storage and supply apparatus of claim 5, wherein the check valve further comprises:a plate disposed within the valve cavity and sealed thereto about its perimeter; a hole formed in the plate for the passage of fuel therethrough; an elastomer attached to the plate and extending therefrom to cover the hole, the elastomer operable to bend to permit fuel to pass out of the tank through the hole, and operable to seal the hole in the event of the flow of fuel into the tank.
- 7. The watercraft fuel storage and supply apparatus of claim 1, further comprising:a further opening formed through the housing; an electrical penetration sealingly disposed within the further opening.
- 8. The watercraft fuel storage and supply apparatus of claim 7, further comprising:a pump assembly disposed within the tank and having an outlet connected to the tube; a wire connected between the pump assembly and the electrical penetration for supplying electrical power to the pump assembly.
- 9. The watercraft fuel storage and supply apparatus of claim 8, further comprising a filter attached to an inlet of the pump assembly.
- 10. The watercraft fuel storage and supply apparatus of claim 7, further comprising:a fluid level sensor disposed within the tank; and a wire connected between the fluid level sensor and the electrical penetration.
- 11. A fuel storage and supply apparatus comprising:a tank having an opening formed therein; a housing sealingly disposed within the tank opening; a fill opening formed in the housing; a fill tube rotatably disposed within the fill opening; a radial O-ring sealingly disposed between the fill tube and a surface of the fill opening; a fuel supply opening formed in the housing; a fuel supply tube rotatably disposed within the fuel supply opening; a radial O-ring sealingly disposed between the fuel supply tube and a surface of the fuel supply opening.
- 12. The fuel storage and supply apparatus of claim 11, further comprising a check valve disposed within the fuel supply opening.
- 13. The fuel storage and supply apparatus of claim 12, wherein the check valve further comprises:a plate having a plurality of holes formed therein for the passage of fuel disposed in the fuel supply opening and sealed thereto along its perimeter; an elastomeric disc attached to the plate and extending to cover the outlet ends of the plurality of holes; the elastomeric disc operable to bend to permit fuel to pass out of the tank through the plurality of holes, and operable to seal the plurality of holes in the event of the flow of fuel into the tank.
- 14. The fuel storage and supply apparatus of claim 12, further comprising:a third opening formed in the housing; an electrical penetration disposed with the third opening; and a radial O-ring sealingly disposed between the electrical penetration and a surface of the third opening.
- 15. An apparatus for sealing an opening formed in a fuel tank, the apparatus comprising;a housing operable to be sealing disposed within an opening formed in a fuel tank; an opening formed through the housing; a tube rotatably disposed through the housing opening; and a radial O-ring sealingly disposed between the housing opening and the tube.
- 16. The apparatus of claim 15, further comprising:a second opening formed through the housing; a second tube disposed to pass through the second opening; and a radial O-ring sealingly disposed between the second opening and the second tube.
- 17. The apparatus of claim 15, further comprising:a second opening formed through the housing; an electrical penetration disposed to pass through the second opening; and a radial O-ring sealingly disposed between the second opening and the electrical penetration.
- 18. The apparatus of claim 15, further comprising a check valve sealingly disposed within the housing opening.
- 19. The apparatus of claim 15, further comprising:a fuel line having a first end connected to the tube; and a filter connected to a second end of the fuel line.
- 20. The apparatus of claim 19, further comprising a pump assembly connected between the filter and the fuel line.
- 21. A kit comprising:a housing adapted to be sealingly disposed within an opening formed in a fuel tank, the housing having an opening formed there through; a tube adapted to be disposed through the housing opening; an O-ring adapted to be disposed around the tube and between the tube and the wall of the housing opening for forming a seal therebetween.
- 22. The kit of claim 21, further comprising:a fuel line adapted to have a first end attached to the tube; and a filter adapted to be attached to a second end of the fuel line.
- 23. The kit of claim 21, further comprising:the housing having a second opening formed therethrough; an electrical penetration adapted to be disposed through the second housing opening; and an O-ring adapted to be disposed around the electrical penetration and between the electrical penetration and the wall of the second housing opening for forming a seal therebetween.
- 24. The kit of claim 23, further comprising;a pump assembly adapted to have its outlet attached to the tube; and a wire connected between the electrcial penetration and the pump assembly.
- 25. A watercraft comprising:a hull; a power unit attached to the hull; a fuel tank disposed in the hull, the fuel tank having an opening formed therein; a housing sealingly disposed in the tank opening, the housing having an opening formed therethrough; a fuel tube rotatably disposed through the housing opening; an O-ring sealingly disposed between the fuel tube and a wall of the housing opening; and a fuel line connected between the fuel tube and the power unit.
- 26. The watercraft of claim 25, further comprising:a second opening formed through the housing; an electrical penetration sealingly disposed through the second opening; a pump disposed within the fuel tank and having an outlet connected to the fuel tube; and a wire connected between the pump and the electrical penetration.
- 27. The watercraft of claim 26, further comprising a fuel filter attached to an inlet of the pump.
- 28. The watercraft of claim 25, further comprising a filter disposed within the tank and connected to the tube opposed the fuel line.
- 29. The watercraft of claim 25, wherein the housing is in threaded engagement with the tank.
- 30. A method of assembling a watercraft, the method comprising the steps of:installing a fuel tank having an opening formed therein into a hull of a watercraft; assembling a power unit to the hull; selecting a fuel tank opening housing having connections corresponding to the power unit; installing the fuel tank opening housing into the fuel tank opening; and installing a fuel line between the housing and the power unit.
- 31. The method of claim 30, further comprising the steps of:providing at least two power units, the at least two power units requiring providing a plurality of fuel tank opening housings, each fuel tank opening housing having connections corresponding to a respective one of the plurality of power units; selecting one of the plurality of power units to assemble to the hull; and selecting the corresponding one of the plurality of fuel tank opening housings to install into the fuel tank opening.
US Referenced Citations (21)