US2099742A - Remote feed for liquid fuel - Google Patents
Remote feed for liquid fuel Download PDFInfo
- Publication number
- US2099742A US2099742A US74309634A US2099742A US 2099742 A US2099742 A US 2099742A US 74309634 A US74309634 A US 74309634A US 2099742 A US2099742 A US 2099742A
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- US
- United States
- Prior art keywords
- valve
- tank
- air
- fuel
- liquid fuel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K5/00—Feeding or distributing other fuel to combustion apparatus
- F23K5/02—Liquid fuel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2931—Diverse fluid containing pressure systems
- Y10T137/3003—Fluid separating traps or vents
- Y10T137/3009—Plural discriminating outlets for diverse fluids
- Y10T137/3012—Common actuator for control valves
Definitions
- This invention relates to forced feeds for liquid fuel and is more directly concerned with transporting fuel from a remote supply to mechanism adapted to function on the so-called instant light arrangement.
- a more particular object of the invention is to provide an instant light system with a remote main fuel tank and a novel auxiliary tank positioned near the burner.
- Another object of the invention is the provision of a novel interlocked valve arrangement on the auxiliary tank which simultaneously opens up the gas line and shuts off the air line and upon opposite movement achieves the reverse operation.
- FIG. 1 is a diagrammatic view of the general arrangement of parts embodying the present in- 'vention
- Fig. 2 is a cross-sectional view taken on a vertical diametric" section through the auxiliary tank seen in Fig, 1.
- the numeral Ill indicates generally a main fuel-supply tank having a conduit l2 for conducting the liquid fuel to an auxiliary tank shown generally at M.
- a conduit I6 is likewise provided to extend between the main fuel tank Ill and the auxiliary tank l4 and this conduit functions to conduct air or other gas under pressure between the tanks l0 and M as hereafter described.
- a pressure gauge l8 may be incorporated in the conduit l6, if this is desired.
- the main fuel tank [0 is adapted to be filled in any suitable manner as through the provision of a member 20.
- auxiliary tank [4 the details of the auxiliary tank [4 have been illustrated as including an instant or mixing valve shown generally at 22 and an air valve 24.
- the instant ligh valve or mixing valve 22 is formed with a downwardly extending flange 26 into which is threaded a tube 28 with a second tube 30 threaded or otherwise secured to the outside of the flange 26.
- the tube 30 is closed at its lower end with a plug 32 which has a screen 34 covering an aperture 36 leading to the inside of the tube 30 as illustrated.
- a wire or pin 38 is provided to extend slightly into the aperture 36 and the pin 38 is mounted in the valve stem 40, which normally effects a valve seal or cut-off as at 42 in the main body of the mixing valve 22.
- the usual packing cup 44 is employed to seal the valve stem 40 at its upper end with respect to the valve body 22.
- An operating knob 46 is secured at the top of the valve stem 49 so that the stem can be rotated to simultaneously move it towards or from the valve seal 42 and to likewise move the pin 38 into and out of substantially sealing fit with the aperture 36.
- valve seal 42 opens or closes a conduit 50 with respect to the inside of tube 28, as will be seen from the drawings, and the aperture 50 is connected with the instant burner which is of any standard type and which has not been shown.
- the air valve 24 is placed adjacent the mixing valve 22 and comprises the standard valve seat closed by valve stem 62, which has a threaded fit in the body of the air valve 24.
- valve stem 62 and the valve seat 60 permit the flow of air or other fluid under pressure to or from the interior of the tank l4 by way of a conduit 68 which is connected to the conduit l6 running back to the main fuel tank In.
- a novel feature of the invention is to provide the valve stem 62 with a gear 64 which cooperates with a gear 66 secured to the valve stem '40 of the mixing valve 22.
- the air valve 24 must be escape from the valve thereby allowing the level of the liquid fuel in the tank to rise until the liquid fuel is likewise drawn or actually forced out of the pipe 82 and valve 86 as desired.
- the auxiliary tank has been filled the device is ready for operation and air pressure is built up in the auxiliary tank by closing the gasoline valve and allowing the pressure from the main tank ID to flow to the auxiliary tank by way of conduit l6 and air valve 24.
- the operating knob 46 will then be turned to open the mixing valve 22 about turn, which will likewise remove the pin 38 very slightly from the aperture 36 so that a by the air pressure through the tube 28 past the valve seal42 out through conduit 50 to the instant burner'where it will flame to a brilliant blue light or heat due to the combined air and gasoline mixture.
- the operating knob 46 When it is desired to shut off the burner the operating knob 46 will merely be turned to close the mixing valve 22 which will simultaneously shutoff the gasoline and again open the air valve 24 thereby providing a supply of .air under pres sure in the top of chamber 14 ready for the next gasoline conduit l2. In starting the next inst'ant j light operation the operating valve 46 will be opened the ordinary turn approximately, which position the spring stop 1 0 will catch on the cam
- the main fuel supply tank can be positioned at any remote distance.
- the system provides'an auxiliary tank for mixing fuel and air and for automatically taking care of the initial mixing of these ingredients until the burner is warm enough to burn the fuel without further premixing the fuel and air.
- pure gasoline can be supplied with the auxiliary tank being reset automatically when the burner is shut off so that the burner can be re-lit at any time with the desired initial charging of mixed-air and gasoline.
- the improved system removes the danger of having the main fuel supply immediately adjacent the burner and likewise allows the various parts of the system to be placed where most convenient or accessible.
- a tank for use in a liquid-fuel system which tank contains liquid fuel and air under pressure, a mixing valve in the tank for comingling the liquid fuel and air under pressure, an air valve for controlling the supply .of air to the tank and gear means for coordinating the action ofthe mixing valve and the air valve so that the mixing valve will be open completely when the'air valve is shut and vice versa, and so both valves may be partially open at the same time.
- a tank for use in a liquid-fuel system which tank contains liquid fuel and air under pressure, a mixing valve in the tank for co-mingling the liquid fuel and air under pressure, an air valve for controlling the supply of air to the tank, and means for coordinating the action of the mixing valve and the air valve so that the mixing valve will be open completely when the air valve is shut and vice versa.
- a tank for use in a liquid-fuel system which tank contains liquid fuel and air under pressure, a mixing valve in the tank for co-mingling the liquid fuel and air under pressure, an air valve for controlling the supply of air to the tank, and means for coordinating the action of the mixing valve and the air valve so that the mixing valve will be open completely when the air valve is shut and vice versa, and a standpipe in the tank through which the liquid fuel is sup plied to the tank.
- a fuel supply system including a main tank containing liquid fuel and air under pressure, an auxiliary tank remote from the main tank, a conduit connecting the lower portion of the main tank with the lower portion of the auxiliary tank, a conduit connecting the upper portion of the main tank with the upper portion of the auxiliary tank, a conduit extending from the auxiliary tank to the place where the fuel is to be used, .a mixing valve in the auxiliary tank and connected to the last-named conduit, said mixing valve being constructed and arranged when partly open to mix and. pass the liquid fuel and air and when fully open to pass liquid fuel only, an air valve in the conduit connecting the upper portions of the tanks, and means for closing the air valve when the mixing valve is fully open and opening the air valve when the mixing valve is not fully open.
- a fuel supply system comprising a tank, a conduit for supplying liquid fuel under pressure to the lower portion of the tank, a conduit for supplying air under pressure to the upper portion of the tank, a conduit extending from the tank to the place where the fuel is to be used, a mixing valve in the tank and controlling the passage of fluids through the last-named conduit, said valve being constructed and arranged tomix and pass the air and liquid fuel when the valve is partly open, said valve passing only liquid fuel when fully open, an air valve in the conduit for supplying air under pressure to the upper portion of the tank, and means for simultaneously opening one valve and closing the other.
- a fuel supply system including a main fuel tank containing liquid fuel and air under pressure, an auxiliary fuel tank remote from the main tank, a gaseous pressure conduit connecting the tanks, a second conduit connecting the tanks and adapted to pass liquid fuel between the tanks, a gas valve in the gaseous pressure conduit adjacent the auxiliary tank, a mixing valve associated with the auxiliary tank and constructed and arranged when partly open to pass a mixture of liquid fuel and gas under pressure to the place where the fuel is to be used, and means for simultaneously fully opening the mixing valve and thereby closing the gas valve and vice versa.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
Description
A. H. KLESA REMOTE FEED FOR LIQUID FUEL Nov. .23, 1937.
2 Sheets-Sheet 1 Filed Sept. 7, 1934 Patented Nov. 23, 1937 UNITED STATES PATENT OFFICE 6 Claims.
This invention relates to forced feeds for liquid fuel and is more directly concerned with transporting fuel from a remote supply to mechanism adapted to function on the so-called instant light arrangement.
Prior to the present invention considerable development has taken place in employing liquid fuels, such as gasoline, so that they will burn instantaneously when discharged to provide light 10 or heat. Before these developments it was substantially impossible to have gasoline burn directly to produce a brilliant light or high heat,
due to the fact that the burner was not heated and because of the difliculty of instantaneously igniting gasoline unmixed with oxygen.
However the developments in advance of the present invention failed to provide a satisfactory arrangement for utilizing instant light burners with a remote fuel supply. It was necessary to place the large fuel supply tank quite close to the burner in order that the mixing valve could be directly associated with the main supply tank whereby the carry of mixed gasoline and air would be short to insure the desired character of the mixture. This arrangement of parts was obviously dangerous in many installations due to the proximity of the burner and the fuel supply, and in addition did not adapt itself to many installations in which it was extremely desirable for purposes of convenience, space or otherwise to place the fuel-supply tank at a station remote from the burner.
It is an object of the present invention to avoid and overcome the above and other difficulties of prior-known devices by the provision of an improved arrangement of parts which permit the instant light type of burner to be employed at any desired distance from the fuel supply.
A more particular object of the invention is to provide an instant light system with a remote main fuel tank and a novel auxiliary tank positioned near the burner.
Another object of the invention is the provision of a novel interlocked valve arrangement on the auxiliary tank which simultaneously opens up the gas line and shuts off the air line and upon opposite movement achieves the reverse operation.
The foregoing and other objects of the invention are achieved in the apparatus described hereafter and illustrated in the accompanying drawings, wherein Fig. 1 is a diagrammatic view of the general arrangement of parts embodying the present in- 'vention;
Fig. 2 is a cross-sectional view taken on a vertical diametric" section through the auxiliary tank seen in Fig, 1.
It should be appreciated that the principles of the invention are adapted for application in various ways, however in accordance with the patent statutes one well-known embodiment of the invention will be specifically described. In the drawings the numeral Ill indicates generally a main fuel-supply tank having a conduit l2 for conducting the liquid fuel to an auxiliary tank shown generally at M. A conduit I6 is likewise provided to extend between the main fuel tank Ill and the auxiliary tank l4 and this conduit functions to conduct air or other gas under pressure between the tanks l0 and M as hereafter described. A pressure gauge l8 may be incorporated in the conduit l6, if this is desired. The main fuel tank [0 is adapted to be filled in any suitable manner as through the provision of a member 20.
In Fig. 2 the details of the auxiliary tank [4 have been illustrated as including an instant or mixing valve shown generally at 22 and an air valve 24. The instant ligh valve or mixing valve 22 is formed with a downwardly extending flange 26 into which is threaded a tube 28 with a second tube 30 threaded or otherwise secured to the outside of the flange 26. The tube 30 is closed at its lower end with a plug 32 which has a screen 34 covering an aperture 36 leading to the inside of the tube 30 as illustrated.
In order to seal the aperture 36 in plug 32 a wire or pin 38 is provided to extend slightly into the aperture 36 and the pin 38 is mounted in the valve stem 40, which normally effects a valve seal or cut-off as at 42 in the main body of the mixing valve 22. The usual packing cup 44 is employed to seal the valve stem 40 at its upper end with respect to the valve body 22. An operating knob 46 is secured at the top of the valve stem 49 so that the stem can be rotated to simultaneously move it towards or from the valve seal 42 and to likewise move the pin 38 into and out of substantially sealing fit with the aperture 36.
The valve seal 42 opens or closes a conduit 50 with respect to the inside of tube 28, as will be seen from the drawings, and the aperture 50 is connected with the instant burner which is of any standard type and which has not been shown.
The air valve 24 is placed adjacent the mixing valve 22 and comprises the standard valve seat closed by valve stem 62, which has a threaded fit in the body of the air valve 24. The
A novel feature of the invention is to provide the valve stem 62 with a gear 64 which cooperates with a gear 66 secured to the valve stem '40 of the mixing valve 22. By this relation of parts when the operating knob 46 is turned to open valve 22, valve 24 will be closed and vice versa.
. The operation of. these parts will be hereafter deout pushing down on the plunger 12, which may be facilitated by incorporating a flange 16 on the plunger. Once the burner has warmed up suffig ciently the valve 22 can be completely opened.
7 The turning movement of the operating knob 46 in the opposite direction will not cause the plunger 12 to function as a stop in that the pin will ride up In the operation of the device liquid fuel, such as gasoline, is placed in the main tank ID by way of the member 20 and air under pressure is supplied to the tank so that gasoline will be forced to the auxiliary tank l4 thereby. When the charging of the auxiliary tank is being done the air valve 24 should naturally be closed and any air in the tank l4 can be drained therefrom by way of the relief valve 80 which includes the stand pipe 82. The valve 80 may also in use of the apparatus serve as a gasoline drain for filling lanterns etc.
In using the valve 80 for filling lanterns, etc., it
will be understood that the air valve 24 must be escape from the valve thereby allowing the level of the liquid fuel in the tank to rise until the liquid fuel is likewise drawn or actually forced out of the pipe 82 and valve 86 as desired. When the auxiliary tank has been filled the device is ready for operation and air pressure is built up in the auxiliary tank by closing the gasoline valve and allowing the pressure from the main tank ID to flow to the auxiliary tank by way of conduit l6 and air valve 24. The operating knob 46 will then be turned to open the mixing valve 22 about turn, which will likewise remove the pin 38 very slightly from the aperture 36 so that a by the air pressure through the tube 28 past the valve seal42 out through conduit 50 to the instant burner'where it will flame to a brilliant blue light or heat due to the combined air and gasoline mixture. Once the burner has been warmed up the spring stop 10. will be pushed down to allow the cam 14 on the operating knob 46 to be turned on past the stop which will permit the mixing valve to be completely opened. This complete opening of the mixing valve will completely shut the air valve 24 through the cooperating gears 64 and 66. The complete opening of the mixing valve 22 removes the end of the pin 38 from the aperture 3650 that the flow of liquid through the aperture is more than sufficient to meet the demands of the burner. As a result, the gasoline or other liquid fuel tends to seek the same level in tube 30 as the liquid outside the tube. Thus, substantially pure gasoline unmixed with air will be thereafter passed. to the warm burner which will volatilize the fuel so that it will still burn to provide the desired light and heat without premixing with air. It will be understood that once the system is operating, as just described, to pass only gasoline or other liquid fuel to the burner and the air valve 24 is closed that the air under pressure in the main tank I 0 forces the liquid fuel from the main tank to the auxiliary tank [4 as the fuel is withdrawn from the auxiliary tank and used.
When it is desired to shut off the burner the operating knob 46 will merely be turned to close the mixing valve 22 which will simultaneously shutoff the gasoline and again open the air valve 24 thereby providing a supply of .air under pres sure in the top of chamber 14 ready for the next gasoline conduit l2. In starting the next inst'ant j light operation the operating valve 46 will be opened the ordinary turn approximately, which position the spring stop 1 0 will catch on the cam By the above-described relation of mechanism 7 an improved instant light system is provided in which the main fuel supply tank can be positioned at any remote distance. The system provides'an auxiliary tank for mixing fuel and air and for automatically taking care of the initial mixing of these ingredients until the burner is warm enough to burn the fuel without further premixing the fuel and air. At this time "pure gasoline can be supplied with the auxiliary tank being reset automatically when the burner is shut off so that the burner can be re-lit at any time with the desired initial charging of mixed-air and gasoline. The improved system removes the danger of having the main fuel supply immediately adjacent the burner and likewise allows the various parts of the system to be placed where most convenient or accessible.
It should be appreciated that the invention has been described and illustrated in detail, how ever the scope of the invention is not limited thereby or thereto but is defined in the appended claims.
What I claim is:
l. A tank for use in a liquid-fuel system, which tank contains liquid fuel and air under pressure, a mixing valve in the tank for comingling the liquid fuel and air under pressure, an air valve for controlling the supply .of air to the tank and gear means for coordinating the action ofthe mixing valve and the air valve so that the mixing valve will be open completely when the'air valve is shut and vice versa, and so both valves may be partially open at the same time.
2. A tank for use in a liquid-fuel system, which tank contains liquid fuel and air under pressure, a mixing valve in the tank for co-mingling the liquid fuel and air under pressure, an air valve for controlling the supply of air to the tank, and means for coordinating the action of the mixing valve and the air valve so that the mixing valve will be open completely when the air valve is shut and vice versa.
' 3. A tank for use in a liquid-fuel system, which tank contains liquid fuel and air under pressure, a mixing valve in the tank for co-mingling the liquid fuel and air under pressure, an air valve for controlling the supply of air to the tank, and means for coordinating the action of the mixing valve and the air valve so that the mixing valve will be open completely when the air valve is shut and vice versa, and a standpipe in the tank through which the liquid fuel is sup plied to the tank.
4. A fuel supply system including a main tank containing liquid fuel and air under pressure, an auxiliary tank remote from the main tank, a conduit connecting the lower portion of the main tank with the lower portion of the auxiliary tank, a conduit connecting the upper portion of the main tank with the upper portion of the auxiliary tank, a conduit extending from the auxiliary tank to the place where the fuel is to be used, .a mixing valve in the auxiliary tank and connected to the last-named conduit, said mixing valve being constructed and arranged when partly open to mix and. pass the liquid fuel and air and when fully open to pass liquid fuel only, an air valve in the conduit connecting the upper portions of the tanks, and means for closing the air valve when the mixing valve is fully open and opening the air valve when the mixing valve is not fully open.
5. A fuel supply system comprising a tank, a conduit for supplying liquid fuel under pressure to the lower portion of the tank, a conduit for supplying air under pressure to the upper portion of the tank, a conduit extending from the tank to the place where the fuel is to be used, a mixing valve in the tank and controlling the passage of fluids through the last-named conduit, said valve being constructed and arranged tomix and pass the air and liquid fuel when the valve is partly open, said valve passing only liquid fuel when fully open, an air valve in the conduit for supplying air under pressure to the upper portion of the tank, and means for simultaneously opening one valve and closing the other.
6. A fuel supply system including a main fuel tank containing liquid fuel and air under pressure, an auxiliary fuel tank remote from the main tank, a gaseous pressure conduit connecting the tanks, a second conduit connecting the tanks and adapted to pass liquid fuel between the tanks, a gas valve in the gaseous pressure conduit adjacent the auxiliary tank, a mixing valve associated with the auxiliary tank and constructed and arranged when partly open to pass a mixture of liquid fuel and gas under pressure to the place where the fuel is to be used, and means for simultaneously fully opening the mixing valve and thereby closing the gas valve and vice versa.
ALBERT
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US74309634 US2099742A (en) | 1934-09-07 | 1934-09-07 | Remote feed for liquid fuel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US74309634 US2099742A (en) | 1934-09-07 | 1934-09-07 | Remote feed for liquid fuel |
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Publication Number | Publication Date |
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US2099742A true US2099742A (en) | 1937-11-23 |
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Application Number | Title | Priority Date | Filing Date |
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US74309634 Expired - Lifetime US2099742A (en) | 1934-09-07 | 1934-09-07 | Remote feed for liquid fuel |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2838292A (en) * | 1954-11-30 | 1958-06-10 | Aladdin Ind Inc | Fuel feeding apparatus for pressure burners |
US2989118A (en) * | 1957-03-27 | 1961-06-20 | William H Cleverdon | Methods for vaporizing and combusting volatile lower hydrocarbons |
-
1934
- 1934-09-07 US US74309634 patent/US2099742A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2838292A (en) * | 1954-11-30 | 1958-06-10 | Aladdin Ind Inc | Fuel feeding apparatus for pressure burners |
US2989118A (en) * | 1957-03-27 | 1961-06-20 | William H Cleverdon | Methods for vaporizing and combusting volatile lower hydrocarbons |
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