Turbine rotor assembly for a rotor-type carburetor

• US 4,725,385 A
• Filed: 08/22/1986
• Issued: 02/16/1988
• Est. Priority Date: 06/30/1986
• Status: Expired due to Fees

• Current Assignee: KWIK Products International Corporation
• Original Assignee: KWIK Products International Corporation
• Inventors: Hubbard, Elbert M., Diener, Rudolf
• Primary Examiner(s): Miles, Tim
• Application Number:
  US06/899,666
• Time in Patent Office: 543 Days
• Field of Search: 261/88, 261/89
• US Class Current: 261/88
• CPC Class Codes: F02B 1/04 with fuel-air mixture admission into cylinder
• CPC Class Codes: F02D 35/0053 by means of a carburettor
• CPC Class Codes: F02D 35/0069 Controlling the fuel flow only F02D35/0076, F02D35/0084 take precedence
• CPC Class Codes: F02M 1/16 Other means for enriching fuel-air mixture during starting; Priming cups; using different fuels for starting and normal operation
• CPC Class Codes: F02M 17/16 Carburettors having continuously-rotating bodies, e.g. surface carburettors
• CPC Class Codes: F02M 69/06 characterised by the pressurisation of the fuel being caused by centrifugal force acting on the fuel
• CPC Class Codes: F02M 7/08 using pumps
• CPC Class Codes: F02M 7/133 Auxiliary jets, i.e. operating only under certain conditions, e.g. full power means for enriching charge at high combustion-air flow F02M7/04; means for enriching charge on sudden throttle opening, i.e. at acceleration F02M7/06
• CPC Class Codes: F02M 71/00 Combinations of carburettors and low-pressure fuel-injection apparatus

Abstract

An injection molded plastic turbine rotor for a rotor-type carburetor is assembled by simply pressing together upper and lower generally cylindrical sections. When joined in this manner the two sections form in the assembled rotor an internal circumferential seal between the two sections, and an internal passageway system which defines a centrifugal pump mechanism within the turbine rotor. In an alternate embodiment, the rotor includes a third plastic section which is captively retained within the rotor, between the upper and lower sections thereof, and is adapted to lockingly receive an end portion of a fuel supply tube inserted downwardly through a central opening formed through the upper section.

Claims

1. A rotor-type carburetor comprising:

a first generally cylindrical rotor section having an anular recess extending axially inwardly from one end portion thereof;

a second generally cylindrical rotor section having an annular end portion complementarily received in said annular recess of said first rotor section;

means defining a circumferential seal between said first and second rotor sections within said annular recess of said first rotor section; and

wherein said annular end portion has an upper end, and wherein said seal-defining means include an O-ring carried by said upper end.

2. A rotor-type carburetor comprising:

a first generally cylindrical rotor section having an annular recess extending axially inwardly from one end portion thereof;

a second generally cylindrical rotor section having an annular end portion complementarily received in said annular recess of said first rotor section;

means defining a circumferential seal between said first and second rotor sections within said annular recess of said first rotor section; and

wherein said first rotor section has an upper end portion having formed therethrough an axially extending central passage adapted for installation therein of a fuel supply tube, the interior surface of said axially extending central passage having formed thereon a radially inwardly projecting sharp-edged annular portion configured to sealingly engage the inserted fuel supply tube.

3. A rotor-type carburetor comprising:

a first generally cylindrical rotor section having an annular recess extending axially inwardly from one end portion thereof;

a second generally cylindrical rotor section having an annular end portion complementarily received in said annular recess of said first rotor section;

means defining a circumferential seal between said first and second rotor sections within said annular recess of said first rotor section; and

wherein said first rotor section has a central axial passage extending downwardly through its upper end and adapted to receive a fuel supply tube, said central axial passage being conically outwardly flared in a downward direction, and wherein said first and second rotor sections define within said rotor apparatus a frustroconically shaped passage having a base portion communicating with the lower end of said central axial opening, an annular side portion which circumscribes said central axial opening and flares conically upwardly from said base portion;

an upper annular passage positioned at and communicating with the upper end of said frustoconically shaped annular passage; and

an annular fuel discharge passage positioned radially outwardly of said upper annular passage, said apparatus further comprising orifice means intercommunicating said upper annular passage with said annular fuel discharge passage.

4. The apparatus of claim 3 wherein the radially inner surface of said upper annular end portion of said second rotor section has a circumferentially spaced plurality of radially inwardly projecting ribs which divide said annular side portion of said frustroconically shaped annular passage into a plurality of separate passages each intercommunicating said upper annular passage with said base portion of said frustroconically shaped passage.

5. The apparatus of claim 3 wherein said second rotor section has a radially outwardly projecting flange which engages the inner surface of said annular recess of said first rotor section, said flange having a circumferentially spaced series of fuel discharge openings formed therethrough.

6. A rotor-type carburetor comprising:

a first generally cylindrical rotor section having an annular recess extending axially inwardly from one end portion thereof;

a second generally cylindrical rotor section having an annular end portion complementarily received in said annular recess of said first rotor section;

means defining a circumferential seal between said first and second rotor sections within said annular recess of said first rotor section; and

wherein said first rotor section has a central axial passage extending downwardly through its upper end, and wherein said apparatus further comprises means associated with the inner surface of said central axial passage for enhancing the rotational acceleration of fuel therein during rotational acceleration of said turbine rotor apparatus.

7. The apparatus of claim 6 wherein said fuel acceleration-enhancement means include at least one axially extending rib projecting radially inwardly from the inner surface of said central axial passage.

8. A rotor-type carburetor comprising:

a first generally cylindrical rotor section having an annular recess extending axially inwardly from one end portion thereof;

a second generally cylindrical rotor section having an annular end portion complementarily received in said annular recess of said first rotor section;

a third rotor section having a generally frustroconical configuration with a central passage formed axially therethrough, said third rotor section being captively retained within said rotor apparatus between said first and second sections thereof and defining with said first and second sections a first frustroconically shaped internal passage in said apparatus which circumscribes the axis thereof.

9. The apparatus of claim 8 wherein said first rotor section has a central axial passage extending downwardly through an upper end portion thereof;

said rotor apparatus further comprises a fuel supply tube extending downwardly through said central axial passage and having a lower end portion press-fitted into said central passage of said third rotor section; and

said third rotor section and said frustroconically shaped internal passage each have a side portion which tapers radially inwardly in an upward direction.

10. The apparatus of claim 9 wherein said fisrt and second rotor sections define within said rotor aparatus:

a second frustroconically shaped passage circumscribing said central axial passage, communicating with said first frustroconically shaped passage, and having an upwardly and radially outwardly tapered side portion;

an upper annular passage positioned at and communicating with the upper end of said second frustroconically shaped passage;

and an annular fuel discharge passage positioned radially outwardly of said upper annular passage; and

and wherein said rotor apparatus further comprises orifice means intercommunicating said upper annular passage with said annular fuel discharge passage.

11. The apparatus of claim 10 wherein the upper and lower ends of said third rotor section have annular chamfers formed thereon adjacent said central passage extending through said thrid rotor section.

12. A rotor type carburetor comprising:

a first rotor section having a first inlet passageway extending axially therethrough and having a first face;

a second rotor section having a second face disposed adjacent the first face;

annular seal means positioned between the first and second faces to form a centrifugal pressure chamber for fuel to establish a fuel pressure within the chamber proportional to the rotational velocity of the rotor;

dosing orifice means sized to pass a predetermined dose of fuel proportional to the fuel pressure from the chamber for ingestion by an engine;

the first and second faces cooperatively defining the pressure chamber in such a manner that the chamber has a volume substantially less than the total volume of the first and second rotor sections combined.

13. The rotor type carburetor of claim 12 wherein the rotor further includes turbine blades attached to one of the sections whereby the rotor may be disposed in an intake air passageway and rotated by induction air to an engine.

14. The rotor type carburetor of claim 13 wherein:

the rotor is disposed for rotation about a vertical axis with the induction air passing downwardly through the air passageway,

the second rotor section is disposed below the first and is supported for rotation by a thrust bearing at the lower end thereof,

a stationary fuel inlet tube extends downwardly through the center of the first rotor section to a point adjacent the second face, and

the pressure chamber extends from the lower end of the fuel inlet tube upwardly and outwardly to the dosing orifice which is located substantially above the lower end of the inlet tube to permit the establishment by gravity of a fuel level within the rotor equal to a level outside the rotor when the rotor is at rest.

15. The rotor type carburetor of claim 14 wherein the turbine blades are attached to the first rotor section and are largely disposed at a height between the lower end of the inlet tube and the dosing orifice, and said carburetor further comprises:

fuel spray edge means formed on the rotor and disposed below the turbine blades, and

fuel passageway means for transporting fuel from the dosing orifice means to the spray edge means.

16. A turbine rotor assembly for a rotor-type carburetor or the like, said turbine rotor assembly being rotatable about an axis and comprising:

(a) means defining a first annular passage positioned within said assembly, circumscribing said axis, and adapted to receive fuel supplied to said assembly during rotation thereof;

(b) means defining a second annular passage positioned within said assembly, circumscribing said axis radially outwardly of said first annular passage and adapted to discharge fuel from said assembly;

(c) orifice means carried within said assembly and intercommunicating said first and second annular passages; and

(d) means, positioned in said first annular passage upstream from said orifice means relative to the rotational direction of said assembly, for blocking a substantial radial portion of said first annular passage along a relatively small circumferential portion thereof.

17. The assembly of claim 16 wherein said first annular passage has a circumferential bypass portion extending beneath said blocking means and configured to cause fuel in said first annular passage to bypass said orifice means during rotational deceleration of said turbine rotor assembly.

18. The assembly of claim 17 wherein said turbine rotor assembly includes a first section which carries said blocking means, and a second section, extending into said first section, in which is formed said bypass portion of said first annular passage, said second section having a lip thereon which partially defines said bypass portion, said lip having formed therein a notch which receives a portion of said blocking means to thereby correctly position said blocking means relative to said orifice means.

19. A method of assembling the turbine rotor portion of a rotor-carburetor, comprising the steps of:

(a) providing a first section of the turbine rotor having therein an annular recess;

(b) providing a second section of the turbine rotor having thereon an annular boss;

(c) inserting said annular boss into said annular recess; and

(d) forming a circumferential seal within said annular recess between said annular boss and said first turbine rotor section.

20. The method of claim 19 wherein said annular boss has an outer end, and wherein said seal-forming step (d) includes positioning an O-ring on said outer end of said annular boss prior to the performance of said inserting step (c).

21. The method of claim 19 wherein said providing steps (a) and (b) are performed by providing plastic first and second turbine rotor sections.

22. The method of claim 19 wherein said first rotor section has an annular lower end portion, and said method further comprises the step of operatively securing a spray ring to said annular lower end portion.

23. The method of claim 22 wherein said securing step is performed in such a manner that an axial portion of said spray ring extends downwardly beyond said annular lower end portion of said first rotor section when spray ring is secured thereto.

24. A method of assembling the turbine rotor portion of a rotor-carburetor having a centrally disposed fuel supply tube, said method comprising the steps of:

(a) providing a first section of the turbine rotor having an axis, an axially extending internal boss, an annular recess circumscribing said internal boss, and a central opening extending axially through said internal boss;

(b) providing a second section of the turbine rotor having an axis, an annular boss circumscribing said last-mentioned axis and having an interior base portion;

(c) providing a third section of the turbine rotor having a central opening formed therethrough;

(d) inserting said annular boss into said annular recess;

(e) interposing said third section between said internal boss and said interior base portion; and

(f) inserting an end portion of the fuel supply tube inwardly through said central opening of said first section and into press-fitting engagement with the surface of said central opening of said third section.

25. The method of claim 24 further comprising the step of forming a circumferential seal within said annular recess between said annular boss and said first turbine rotor section.

26. The method of claim 25 wherein said annular boss has an annular end portion, and wherein said seal-forming step includes operatively positioning an O-ring on said annular end portion prior to the performance of said inserting step (d).

27. A method of rotationally retarding the bladed turbine rotor portion of a rotor-type carburetor upon shut-down of an engine in which the carburetor is installed, the turbine rotor having upper and lower opposite end portions rotatably carried, respectively, by upper and lower support structures, the rotating turbine rotor blades creating a downward force on the rotor during engine operating and a lifting force thereon when air inflow to the engine ceases, said method comprising the steps of:

(a) axially slidably mounting the opposite upper and lower end portions of the turbine rotor, respectively, in the upper and lower support structures;

(b) configuring the turbine rotor to permit axial play thereof between the upper and lower support structures; and

(c) providing said turbine rotor with a surface positioned and configured to frictionally engage one of said supporting structures when said turbine rotor lifts during air flow shut-down to the engine.

28. A rotor type carburetor comprising:

a cylindrical barrel forming a passageway of air to be driven into an engine,

upper and lower support spiders attached to the cylindrical barrel and extending into the passageway,

a fuel inlet tube extending from the upper support spyder toward the lower support spyder along the axis of the passageway and connected to a supply of fuel,

a rotor supported by bearing means on the lower spyder for rotation about the fuel inlet tube, the rotor including;

a generally cylindrical first member having an axial bore therethrough for receiving the fuel inlet tube, and a lower face;

a generally cylindrical second member having means on the lower end for cooperative engagement with the bearing means on the lower support spyder for rotatably supporting the rotor for rotation about the axis and an upper face disposed adjacent the lower face of the first member;

an annular seal formed between the first and second member to form a fuel pressure chamber between the adjacent faces communicating with the fuel inlet tube, for establishing fuel pressure upon rotation of the rotor due to centrifugal forces;

a fuel dosing orifice formed in one of the members at a point spaced radially from the axis of the rotation and substantially above the lower end of the fuel inlet tube for providing fluid communication from the fuel pressure chamber to the exterior of the chamber;

the lower and upper faces being conformed to form a fuel passageway within the pressure chamber from the lower end of the fuel inlet tube to the dosing orifice of substantially reduced volume when compared to the total available volume;

a plurality of turbine blades formed on a cylindrical third member disposed around the first and second members;

a circumferential spray edge formed on the lower end of the third member below the turbine blades for atomizing fuel applied thereto as the rotor rotates due to air passing through the barrel and over the turbine blades; and

the third member defining a fuel passageway from the dosing orifice to the spray edge.

29. The rotor type carburetor of claim 28 further comprising:

a fourth annular member mounted on the inlet tube and disposed in spaced relationship between the first and second members, the fourth annular member projecting radially outwardly from the fuel inlet tube to extend the passageway formed by the annulus between the tube and the first member outwardly from the tube before communicating with the pressure chamber.

30. The rotor type carburetor of claim 28 wherein:

the first and third members are formed of the same molded component, joined near the upper end of the third component, and

the dosing orifice means is a radial passageway through the second member.

31. The rotor type carburetor of claim 28 further characterized by an annular sliding seal rotating with the first member and engaging the fuel inlet tube, the sliding seal having a very small area of contact and being formed by an injection molded plastic.

32. The rotor type carburetor of claim 28 wherein the third annular member includes a metallic tension band disposed around the lower end thereof which also forms the spray edge.

33. The rotor type carburetor of claim 28 wherein the dosing orifice is formed by a synthetic ruby inset secured in a passageway extending through one of said first and second members.