Noise reducing system

Information

  • Patent Grant
  • 6419533
  • Patent Number
    6,419,533
  • Date Filed
    Wednesday, October 17, 2001
    22 years ago
  • Date Issued
    Tuesday, July 16, 2002
    21 years ago
Abstract
A noise reducing system for a personal watercraft. The system includes a pump insulating system which insulates the pump housing from the hull. More particularly, the pump insulating system includes at least one insulating attachment for connecting a pump housing to a supporting surface of a personal watercraft. Such insulating attachment includes an insulator having a portion mounted between the pump housing and the supporting surface. Advantageously, the system also includes a resonator and a shield, both mounted on the exhaust system, and an insulating material mounted inside an air intake pipe.
Description




FIELD OF THE INVENTION




The invention relates to a noise reducing system for personal watercraft.




BACKGROUND OF THE INVENTION




A personal watercraft is a new recreational vehicle which has had a resounding commercial success during the last several years. However, personal watercraft suffer from complaints of noise pollution.




Several countries, such as the United States and France are studying the possibility of passing regulations which will limit the noise of a personal watercraft to 80 DB(A) at a distance of 7.5 m. Prior art personal watercrafts usually emit more than this level. Thus, there is a need in the industry to provide a personal watercraft which emits a more tolerable level of DB(A).




Studies have showed that personal watercraft noise problems are complex because the noise comes from multiple sources and follow multiple transfer paths. Indeed, sources may be divided into three categories (i) structural noise which is related to the hull radiating noise coming from induced efforts created by the jet pump and other mechanical elements fixed to the structure (mechanical excitation); (ii) aerial noise which corresponds to the noise emitted by acoustical wave transmission produced by the muffler walls and the air intake (acoustical excitation); and (iii) direct noise such as muffler outlet or jet pump flow.




It has been shown that insulating the pump from the hull will reduce the noise coming from the pump itself and from the motor via the shaft (mechanical excitation). If has also been shown that it is possible to reduce the acoustical excitation by insulating some noise generating components.




An object of the present invention is to provide a noise reducing system which reduces the noise generated by a personal watercraft.




A further object of the invention is to provide a pump insulating system which reduces structural noise coming from the pump, and from the motor via the shaft, without substantially decreasing the performance of the pump.




As embodied and broadly described herein, the invention seeks to provide a pump insulating system for a personal watercraft having a pump housing and a supporting surface; said insulating system including a least one insulating attachment for connecting the pump housing to the supporting surface; said insulating attachment including an insulator having a portion mounted between the pump housing and the supporting surface.




The invention further seeks to provide a personal watercraft including;




a motor;




a pump;




a shaft connected between the motor and the pump;




a hull structure with a tunnel and an air intake;




a supporting surface of a wall located at one end of the hull structure;




a pump housing attached to the supporting surface;




wherein the improvement includes a pump insulating system comprising at least one insulating attachment for connecting the pump housing to the supporting surface; said insulating attachment including an insulator having a portion mounted between the pump housing and the supporting surface.




In a preferred embodiment of the present invention the novel noise reducing system for use on a personal watercraft comprises: an air intake tube having an insulating foam inside; a pump insulating system having at least one insulating attachment; said insulating attachment comprising a threaded rod, a sleeve having an aperture in which the threaded rod is inserted and at least one T-shaped rubber insulator; a muffler including a shield mounted thereon; the shield having a first polyurethane foam layer and a second composite layer; and a resonator made of moulded plastic mounted on an exhaust pipe.




Other objects and features of the invention will become apparent by reference to the following specification and to the drawings.











BRIEF DESCRIPTION OF THE DRAWINGS




A detailed description of the preferred embodiment of the invention is provided herein with reference to the following drawings, wherein:





FIG. 1

is a side elevational view of a watercraft;





FIG. 2

is an enlarged fragmentary perspective view of a pump housing wherein one insulating attachment used in the invention is shown with a sectional view taken along a mid line;





FIG. 3

is similar to

FIG. 2

except that a different circular sealing gasket is illustrated;





FIG. 4

is an enlarged perspective view of a sealing gasket having projections for insulating the attachment points;





FIG. 5

is an enlarged perspective view of a pump housing showing an exploded view of an insulating attachment constructed in accordance with a first variant;





FIG. 6

is an enlarged perspective view of the insulating attachment constructed in accordance with a first variant;





FIG. 7

is an enlarged fragmentary perspective view of a pump housing wherein one insulating attachment constructed with a second variant is shown with a sectional view taken along a mid line;





FIG. 8

is an enlarged perspective view of an exhaust pipe including a muffler shield and a resonator used in the invention;





FIG. 9

is an enlarged elevational view of the exhaust pipe illustrated in

FIG. 8

;





FIG. 10

is an enlarged perspective view of the muffler shield shown in

FIGS. 8 and 9

wherein half of the muffler shield is illustrated; and





FIG. 11

is an enlarged fragmented perspective view of an air intake tube.











In the drawings, the preferred embodiment of the invention is illustrated by way of example. It is to be expressly understood that the description and drawings are only for the purpose of illustration and as an aid to understanding, and are not intended as a definition of the limits of the invention.




DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring now to the drawings,

FIG. 1

illustrates a personal watercraft


10


comprising a hull


12


and a superstructure that includes a forward cab portion


14


and a rear seat portion


16


to support a driver and/or passenger.




The propulsion system of the watercraft


10


comprises an engine schematically represented at


18


having a shaft


20


driving a pump


22


. An air intake tube


21


is supplied for providing to the engine enough air for its operation and for allowing an air flow which eliminates fuel vapour. The pump


22


is located within a pump housing


24


that is affixed to a supporting surface


25


of a wall located at the end of the hull


12


. The hull


12


has an internal duct


26


leading from a forward inlet


28


to a rearward outlet


30


. The inlet


28


is positioned in the keel region of the hull


12


and is thus at all times below the waterline represented at


32


.




The steering of the watercraft


10


is effected by means of an outlet nozzle


34


which is mounted to be pivotable about a generally vertical axis under the control of a linkage


36


that is connected to a handlebar


38


. The pump


22


drives a jet of water through the duct


26


and rearwardly through the outlet nozzle


34


for the propulsion of the watercraft


10


.




As illustrated in

FIG. 2

, the pump housing


24


is affixed to the supporting surface


25


with at least one pump insulating attachment


38


. The insulating attachment


38


includes a threaded rod


40


, a sleeve


42


having an aperture in which the threaded rod


40


is inserted and at least one T-shaped rubber insulator


44


. The threaded rod


40


and the rubber insulator


44


are adapted to allow compression of about 5% to 30%.




A circular sealing gasket


46


is mounted between the pump housing


24


and the supporting surface


25


in order to avoid any pressure loss at their junction. The circular sealing gasket


46


has at least one projection


48


. As illustrated in

FIG. 3

, a circular sealing gasket


50


, instead of the circular sealing gasket


46


, is mounted between the pump housing


24


and the supporting surface


25


. The sealing gasket


50


has a groove


52


for defining a V shape and for increasing its flexibility. When the pressure increases in the internal duct


26


, the sealing gasket


50


then permits a higher sealing action.




As illustrated in

FIG. 4

, instead of a circular sealing gasket, a sealing gasket


54


having at least one projection


56


may be provided for installation between the pump housing


24


and the supporting surface


25


. The projection


56


has an aperture


58


allowing insertion of a pump attachment and a certain degree of flexibility. Thus, the sealing gasket


54


reduces structural noise coming from the pump


22


and seals the pump housing.




Referring now to

FIG. 5

, a pump insulating attachment constructed in accordance with a first variant is represented at


60


. The insulating attachment


60


includes a threaded rod


62


, a sleeve


64


having an aperture in which the threaded rod


62


is inserted, at least one inside insulator


66


and at least one outside insulator


68


. The inside insulator


66


and the outside insulator


68


have an aperture


70


and


72


respectively for allowing insertion of the sleeve


64


. The outside insulator


68


has also at least one aperture


74


and a crenellated surface


76


for increasing its flexibility. The inside insulator


66


has also a crenellated surface


78


.

FIG. 6

illustrates the insulating attachment


60


wherein the insulators


66


and


68


are mounted on the threaded rod


62


.





FIG. 7

illustrates an insulating attachment


80


constructed in accordance with a second variant. The insulating attachment


80


includes an insulator


82


mounted between two supporting plates


84


having a threaded rod


86


affixed thereon.




Referring now to

FIGS. 8 and 9

, an exhaust line


90


includes at least one resonator


92


, a muffler


94


and a tuned pipe


96


(schematically represented) located between the muffler


94


and the engine


18


(also schematically represented). The resonator


92


is made of moulded plastic and comprises a main-pipe


98


with at least one frequency pipe


100


mounted thereon: At the outlet, the exhaust line


90


comprises a larger resonator


102


. Because the resonator


92


is mounted perpendicularly to the exhaust line


90


, the resonator


92


does not affect the performance of the engine


18


. Indeed, the back pressure and the exhaust flow are not influenced by the resonator


92


. The exhaust line


90


comprises attachment means


104


for affixing it to the hull


12


. It is understood that the resonator


92


may have different configurations for attenuating some undesirable sound frequencies. For example, the number and the length of the frequency pipe(s)


100


may vary in order to obtain different results.




It is understood that it may be possible to use one of the sealing gasket described above in combination with one of the pump insulating attachment also described above by doing the necessary modifications if required.





FIG. 10

illustrates the muffler


94


wherein it is possible to see that it is recovered with a shield


106


comprising a first polyurethane foam layer


108


and a second composite layer


110


. More particularly the foam layer


108


is made of a foam conforming to the standard number ASTM D 3574-86 and the composite layer


110


is made of a material sold under the trademarks BARYMAT BM-1A or BARYMAT BM-1C.

FIG. 11

illustrates the air intake tube


21


having an insulating foam layer


112


mounted inside, the insulating foam layer


112


is also made of a foam conforming to the standard number ASTM D 3574-86.




The above description of the preferred embodiment should not be interpreted in any limiting manner since variations and refinements are possible which are within the spirit and scope of the present invention. The scope of the invention is defined in the appended claims.



Claims
  • 1. A vehicle comprising:a vehicle body; an engine mounted within said vehicle body; a vehicle driving system operatively connected to said engine, said vehicle driving system being constructed and arranged to create a motive force that moves said vehicle using power from said engine; a tubular air intake conduit having one end open to the atmosphere and an opposite end in communication with said engine, thereby enabling said engine to draw air into said engine via said intake conduit for use in a combustion cycle of said engine; said air intake conduit being lined at least partially along the interior surface thereof with a noise reducing material adapted to reduce engine noise passing to the exterior of said vehicle body through said air intake conduit, wherein said noise reducing material is an open-cell foam.
  • 2. A vehicle according to claim 1, wherein the open-cell foam is polyurethane.
  • 3. A vehicle according to claim 1, wherein said vehicle is a watercraft with said vehicle body comprising a hull and a deck mounted atop said hull and with said driving system comprising a pump assembly for generating and discharging a stream of pressurized water to propel said watercraft.
  • 4. A vehicle according to claim 3, wherein said watercraft is a personal watercraft.
  • 5. A vehicle according to claim 4, wherein said noise reducing material is an open-cell foam.
  • 6. A vehicle according to claim 5, wherein the open-cell foam is polyurethane.
  • 7. A vehicle according to claim 1, wherein said air intake conduit is fully lined along the interior surface thereof.
  • 8. A watercraft comprising:a hull; an engine mounted within said hull; a propulsion system operatively connected to said engine, said propulsion system being constructed and arranged to propel said watercraft using power from said engine; an exhaust system connected to said engine such that exhaust gases generated by said engine flow therethrough for discharge to the atmosphere; said exhaust system comprising a muffler covered by a shield comprising a first layer of noise reducing material and a second layer surrounding said first layer.
  • 9. A watercraft according to claim 8, wherein said noise reducing material is an insulating foam.
  • 10. A watercraft according to claim 9, wherein said insulating foam is a foam conforming to the standard number ASTM D 3574-86.
  • 11. A watercraft according to claim 10, wherein the foam is an open-cell foam.
  • 12. A watercraft according to claim 11, wherein the foam is polyurethane.
  • 13. A watercraft according to claim 8, wherein said second layer is a composite material.
  • 14. A watercraft according to claim 13, wherein said composite material is selected from the group consisting of BARYMAT BM-1A and BARYMAT BM-1C.
  • 15. A watercraft according to claim 9, wherein said second layer is formed from a composite material.
  • 16. A watercraft according to claim 15, wherein said composite material is selected from the group consisting of BARYMAT BM-1A and BARYMAT BM-1C.
  • 17. A watercraft according to claim 16, wherein said insulating foam is a foam conforming to the standard number ASTM D 3574-86.
  • 18. A watercraft according to claim 17, wherein the foam is an open-cell foam.
  • 19. A watercraft according to claim 18, wherein the foam is polyurethane.
  • 20. A watercraft according to claim 8, wherein said watercraft is a personal watercraft.
Priority Claims (1)
Number Date Country Kind
2,228,759 Feb 1998 CA
Parent Case Info

This is a continuation of application Ser. No. 09/688,818, filed Oct. 17, 2000, which is a continuation of application Ser. No. 09/490,757, filed Jan. 24, 2000 now abandoned, which is a continuation of application Ser. No. 09/020,170, filed Feb. 6, 1998 now U.S. Pat. No. 6,019,648 issued Feb. 1, 2000.

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Number Name Date Kind
2325905 Caulfield Aug 1943 A
3454129 Everett Jul 1969 A
3744589 Mellin Jul 1973 A
4258821 Wendt et al. Mar 1981 A
4263982 Feuling Apr 1981 A
4629432 Dyrkorn et al. Dec 1986 A
5234364 Ito Aug 1993 A
5310368 Kamitake May 1994 A
5460553 Craig et al. Oct 1995 A
5699749 Yamada et al. Dec 1997 A
5879211 Koyanagi Mar 1999 A
6019648 Lecours et al. Feb 2000 A
Non-Patent Literature Citations (1)
Entry
Bombardier “Sea-Doo,” Parts Catalog GSX 1996, pp. A1, A2, D4 and D5.
Continuations (3)
Number Date Country
Parent 09/688818 Oct 2000 US
Child 09/977952 US
Parent 09/490757 Jan 2000 US
Child 09/688818 US
Parent 09/020170 Feb 1998 US
Child 09/490757 US