US1014188A - Carbureter. - Google Patents
Carbureter. Download PDFInfo
- Publication number
- US1014188A US1014188A US59958110A US1910599581A US1014188A US 1014188 A US1014188 A US 1014188A US 59958110 A US59958110 A US 59958110A US 1910599581 A US1910599581 A US 1910599581A US 1014188 A US1014188 A US 1014188A
- Authority
- US
- United States
- Prior art keywords
- air
- carbureter
- valve
- plates
- engine
- 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
Links
- 239000000446 fuel Substances 0.000 description 11
- 239000007788 liquid Substances 0.000 description 5
- 239000004215 Carbon black (E152) Substances 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 238000002156 mixing Methods 0.000 description 3
- 239000002360 explosive Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 235000002020 sage Nutrition 0.000 description 2
- 101150057833 THEG gene Proteins 0.000 description 1
- 238000012550 audit Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000012432 intermediate storage Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000037452 priming Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M9/00—Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position
- F02M9/10—Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position having valves, or like controls, of elastic-wall type for controlling the passage, or for varying cross-sectional area, of fuel-air mixing chambers or of the entry passage
- F02M9/103—Mechanical control
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S261/00—Gas and liquid contact apparatus
- Y10S261/58—Choke tube having plurality of leaves
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S261/00—Gas and liquid contact apparatus
- Y10S261/59—Choke tube leaves flexible
Definitions
- Iii-accordance with the PItSOI liT invention there is provided an air duet ul which there lodged means wherehy the etl'eetive (l'usS- will for aeeeleratingor -1'el arding the speed 'of flow of theair therethrtmgh and at an appropriate. point with relation to the aeeelerat- 30 in; means other means are provided for the injecting ot' a stream of liquid hydro-carhon into traversing relation'to the aeeelerated 'eoluiun' ot'air the liquid being at the same time sprayed so to heroineintimately 5,1nixe'd with and vaporized hy'the. air colunmJ and then ahsoi'hed therehy, so that the.
- air in the mixing zone may he; established under all 1 eonditlons otengine demand which will give the best ,iutermixture of air and hydro-carbon for the production of the explosive charge. l best; understood 7 from a eonz'siderat-ionof the following deseetioual area lot the. duel um he varied at? tailed description taken in eonnectionwith' forming apart. with the understandand adjacent parts.
- a easing 1 constituting an at its free end isthreaded for therelception plaee. but still permit its ready' removal may he employed to renderthejunction of theeover and easing fluid tightif such be neeted by a net-k 6 to a valve vasing 7- pro- .sage f) for a valve stem 10, and at the end remote from theeap the casing 7 s formed with an axial passage 11 in line with a sup cap nut 12-;
- FIG. 4 is a section on the line"
- intermediate storage chamber for the liquid hydro-carbon which hereinafter will be referred to last gasolene for conveniehce,without, however, in any manner lin1iting the inventionto the use ⁇ ofjgasolene fas the hydro-carbon em I ployed.
- This gasolene chamber 1 is shown: as provided with an axial stem 2 and a cover 3, the latter-being preferably formed with a flange 4 designed to enter theopen top of the easingl with the stem 2 transversing a een tral perforation in.
- the casing l is c0n-' with an outzstanding'flange 14, by. Whichth', eap 13 'holds the pipe tot-he valve casing.
- the valvestem is provided with a valve end 15 adapted to close the-end of the paS- 105 on the-stem arempaoed collars "16 between which engages yoke 17 formed on [one end P tented Ja n. 9,1 912.
- a central passage for the pipe '12 may be '1 65 Fig.2:is a; centralf I longitudinal section through the'air conduit Fig. 3 is 'asection on pipe ortube 22 at each suction stroke of the engine.
- the effective area of the tube 22 is reduced at the hinge connections 33 of the plates 31 and 32 because of the approach of these hinge connections to the longitudinal axis of the pipe 22 and con- 'sequently the speed ot-the air at this point is increased, and, moreover, as it passes the point of close approach to the central portions of the plates 31 and 32 theair then expands with a resultant production of subatmospheric pressure-lower than would occur itthe pipe 22avere freely open throughout.
- the screw 24 maybe moved by the screw 24 toward and from the sleeve 35 andwhemthe latter is moved bythearbor 39 controlling the valve 40 the efi'cctive opening through the tube 22 at the hinge-portion 330i the plate3l and plate 32 may" be relatively greater or smaller depending upon the adjustment-of the. sleeve 29, so that the action of the with the conditions present in the particular Other adjustments of the carbureter which engine furnished with fuel by the carbureter.
- the carbureter of'the present. invention in its practical operation is very flexible and ,may be adjusted until throttled down so that the engine speed may be reduced to a low minimum, but when the carbureter is opened up the power generated by the engine is markedly superior due to the closeapproach to the ideal explosive mixture.
- the carbureter of thepresent invention has a sufficiently wide range of adjustmentto adapt. it to any cxplosionengi-ne, and when once adjusted to the engine no further change is necessary.
- a chamber having means for the introduction 0t fuelthereinto, said chamber'having its walls receding from a point'adjacent to the point of entrance of the fuel, means for adjusting the degree of inclination of the walls with relation to the fuel inlet, and means other than the firstnamed means foralso adjusting thedegree ofinclination. ofathe walls with relation'to the fuelinlet, v
- a carburetor a chamber provided with an inletfor. fuel and two series of plates constituting the Walls of the chamber adjacent the fuel inlet, the plates of one series being'connectedend to end with the plates of the other series, a valvein the chamber, and connections between the valve and the corresponding ends of one series of plates for causing a movementof said plates by the adjustment ofthe valve.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Description
W. R. VOORHEES.
GARBURETER. APPLICATION FILED 3x50111910.
Patented J3J L9, 1912.
INVENTOR I WITNESSES ATTORNEY "55 The invention will be UN-IIITED TA E WILSON ROSS VOOR-HEES. OF
PATENT OFFICE;
PERTH. Amer, NEW JERSEY.
CARBURETER.
LOItJSta.
Specification of Letters Patent.
Applicaton fiIedDecember 27, 1910. Serial No. 599,581.
5-and State of New Jersey. have invented a new and useful Carlmreter.' following is a speeifieation. g 'lhis i1iv '1iti n1- hasreference toii'mprove- 'nients in 'earlmreters, audits ohjeet is to of which the -'an intimate adinixtureaofair and hydroearhon "gas. controllable either automatieally or by hafml. the structure being such that a liquid :h;vdro-carh(m"drawn from a suitable tank by the. suction of the engine. is spravedj intoa moving eolumnf of-air, the
speed of which whereintersecting the spray ioff hydrorearhon liquid .is readily eontrolla'hle. while-atthe; samet-une the passage i through'whieh the earhureted air'is directed to the engine uiay lie tln ot-tledior enlarged as needed.
Iii-accordance with the PItSOI liT invention there is provided an air duet ul which there lodged means wherehy the etl'eetive (l'usS- will for aeeeleratingor -1'el arding the speed 'of flow of theair therethrtmgh and at an appropriate. point with relation to the aeeelerat- 30 in; means other means are provided for the injecting ot' a stream of liquid hydro-carhon into traversing relation'to the aeeelerated 'eoluiun' ot'air the liquid being at the same time sprayed so to heroineintimately 5,1nixe'd with and vaporized hy'the. air colunmJ and then ahsoi'hed therehy, so that the.
air is suilahly euriehed. Between this mix ing portion of the (:ondmtand the intake ofthe enginethere is provided a valve, whereby the'volulne of an passing to the engine may he controlled and this will in like mau- 'nereoulrolthespeed ot' the air at the mixin; zone. It] sueh manner that when the air 'column s th'rollled to'a "reater degree the 1 45 passage for the air at the mixing zone is deereased in order that the speed of travel of the air at. this point will proportionately ini 'erease. and by properly n-oporlioning and adjusting the .parts a speed ottravel of the. air in the mixing zone. may he; established under all 1 eonditlons otengine demand which will give the best ,iutermixture of air and hydro-carbon for the production of the explosive charge. l best; understood 7 from a eonz'siderat-ionof the following deseetioual area lot the. duel um he varied at? tailed description taken in eonnectionwith' forming apart. with the understandand adjacent parts.
the line of Fig.' 2 omitting more dis- 4-4 of Fig; 2'.
a easing 1 constituting an at its free end isthreaded for therelception plaee. but still permit its ready' removal may he employed to renderthejunction of theeover and easing fluid tightif such be neeted by a net-k 6 to a valve vasing 7- pro- .sage f) for a valve stem 10, and at the end remote from theeap the casing 7 s formed with an axial passage 11 in line with a sup cap nut 12-;
formed at the-end adjacent the passage 11 sage 11 Where entering the valve casing and of a; lever 18 ex't'ending'through the neclt 6, being there mounted upon .apivot pin 19 traversing'the neck. The other end of the lever 18 from that carrying the yoke 17 enters the casing 1 and is there formed with 'be incorporated in numerous vot-hertorins while still retaining salient fea- In the drawings :Figure 1 is an elevzu taut parts; Fig. 4 is a section on the line" Referring to thedrawings, there is shown intermediate storage chamber for the liquid hydro-carbon which hereinafter will be referred to last gasolene for conveniehce,without, however, in any manner lin1iting the inventionto the use} ofjgasolene fas the hydro-carbon em I ployed. :This gasolene chamber 1 is shown: as provided with an axial stem 2 and a cover 3, the latter-being preferably formed with a flange 4 designed to enter theopen top of the easingl with the stem 2 transversing a een tral perforation in. the cover, and this stein 5 ot a nut designed to hold the cover in I desired- At one point the casing l is c0n-' with an outzstanding'flange 14, by. Whichth', eap 13 'holds the pipe tot-he valve casing. The valvestem is provided with a valve end 15 adapted to close the-end of the paS- 105 on the-stem arempaoed collars "16 between which engages yoke 17 formed on [one end P tented Ja n. 9,1 912.
when desired. Of course, suitable paekiiiigjvided with a Cap 8 with an axial guide pasv{ily,.1. i.pe '12 held to the valve casing by a. v H
provided with a central passage for the pipe '12, and the latter may be '1 65 Fig.2:is a; centralf I longitudinal section through the'air conduit Fig. 3 is 'asection on pipe ortube 22 at each suction stroke of the engine. However, the effective area of the tube 22 is reduced at the hinge connections 33 of the plates 31 and 32 because of the approach of these hinge connections to the longitudinal axis of the pipe 22 and con- 'sequently the speed ot-the air at this point is increased, and, moreover, as it passes the point of close approach to the central portions of the plates 31 and 32 theair then expands with a resultant production of subatmospheric pressure-lower than would occur itthe pipe 22avere freely open throughout. There is, therefore, an injector action on the gasolene within the pipe and this gasolene is withdrawn "from the pipe through .the end of the pipe within the tube 22, and this gasolene is directed toward the plate42 to be deflected thereby into the streams'of air passing alongside of the plate '.42,"through.the sleeve .35, with the result that the gasolene is finely divided and at once evaporated and absorbed by theg'air, to
-be'ultimatelydrawn into the engine and utilized in theusual manner.
' .The relative 'prop'ortionsof gasolen and correspondingly varying the effective area pipe at the middle" or junction por the channel through the pipe as defined by the plates 31 and. 32. Ordinarily as the' valve 40 is'opened'the effective space at the 33is increasedfto bc decreased asthe valve 40 is-moved-toward the closed 'lposition. The relation betweenthe effective opening at the hinge portion 33 of the plates- .31 and 32 and the relation thereto of the valve 40; is variable by means of the screw 24; acting on the-sleeve 29 to move it longif'tudinally of the tube 22. Since the relation of the sleeve 35 to the arbor 39 is determined by the link 37 it follows that the sleeve; 29
maybe moved by the screw 24 toward and from the sleeve 35 andwhemthe latter is moved bythearbor 39 controlling the valve 40 the efi'cctive opening through the tube 22 at the hinge-portion 330i the plate3l and plate 32 may" be relatively greater or smaller depending upon the adjustment-of the. sleeve 29, so that the action of the with the conditions present in the particular Other adjustments of the carbureter which engine furnished with fuel by the carbureter.
are desirable'arc effectedfilirough the con necting rod 44. Difiiculty is found in starting explosion engines using gasolene as a fuel, especially certain flow of air occurs through the I in very cold weather, but in the practical operation of the present invention it is found that the engine is readily started in the coldest weather without priming. The carbureter of'the present. invention in its practical operation is very flexible and ,may be adjusted until throttled down so that the engine speed may be reduced to a low minimum, but when the carbureter is opened up the power generated by the engine is markedly superior due to the closeapproach to the ideal explosive mixture. The carbureter of thepresent invention has a sufficiently wide range of adjustmentto adapt. it to any cxplosionengi-ne, and when once adjusted to the engine no further change is necessary.
bases "remote one fromthe other and joined atthe smaller ends, and that the slant or pitch of the walls of these spaces is vari-. able in accordance-with themovcments of the sleeves; 29
and .35 toward or from each other.
1: IIi afcarbureter," a chamber having means for the introduction 0t fuelthereinto, said chamber'having its walls receding from a point'adjacent to the point of entrance of the fuel, means for adjusting the degree of inclination of the walls with relation to the fuel inlet, and means other than the firstnamed means foralso adjusting thedegree ofinclination. ofathe walls with relation'to the fuelinlet, v
2. In a carbureter, achamberihaving'an ,inlet for fuel and provided with walls receding in both directions from the fuel inlet,
means for adjusting the degree'of inclin'as tion of the walls with relation tov the fuel inlet, and other means independent of the' first-named means for adjusting the degree of inclination of the walls with relation to the fuel inlet. 3. In a carbureter, a chamber having a fuel; inlet vand-adjacent thereto series of plates :hingedly connected together at their meeting ends and' hingedlycarried at their other ends, and means for causing the approach or recession of the connected ends ,of the plates of the said series toward orfrom the longitudinal axis of said'series.
44111 a carburetor, a chamber provided with an inletfor. fuel and two series of plates constituting the Walls of the chamber adjacent the fuel inlet, the plates of one series being'connectedend to end with the plates of the other series, a valvein the chamber, and connections between the valve and the corresponding ends of one series of plates for causing a movementof said plates by the adjustment ofthe valve.
5. In a carbureter, atubul'archamber, a
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US59958110A US1014188A (en) | 1910-12-27 | 1910-12-27 | Carbureter. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US59958110A US1014188A (en) | 1910-12-27 | 1910-12-27 | Carbureter. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1014188A true US1014188A (en) | 1912-01-09 |
Family
ID=3082494
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US59958110A Expired - Lifetime US1014188A (en) | 1910-12-27 | 1910-12-27 | Carbureter. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1014188A (en) |
-
1910
- 1910-12-27 US US59958110A patent/US1014188A/en not_active Expired - Lifetime
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1014188A (en) | Carbureter. | |
| US1212478A (en) | Carbureter. | |
| US1394452A (en) | Island | |
| US1260273A (en) | Carbureter. | |
| US1961083A (en) | Control device for liquid fuel burners | |
| US838085A (en) | Carbureter for explosive-engines. | |
| US907123A (en) | Carbureter. | |
| US541074A (en) | dandison | |
| US1207224A (en) | Carbureter. | |
| US1623683A (en) | Carburetor | |
| US1412000A (en) | Kerosene carburetor | |
| US1780626A (en) | Fuel mixer for internal-combustion engines | |
| US1225466A (en) | Carbureter. | |
| US1112257A (en) | Mixture-supplying apparatus for internal-combustion engines. | |
| US1205693A (en) | Carbureter. | |
| US1833196A (en) | Charge forming device | |
| US1156836A (en) | Carbureter. | |
| US1398640A (en) | Carbureter | |
| US1786283A (en) | Automatic air-inlet valve for internal-combustion engines | |
| US1239173A (en) | Carbureter. | |
| US1270558A (en) | Carbureter. | |
| US1091426A (en) | Carbureter. | |
| US1064867A (en) | Carbureter. | |
| US1314872A (en) | Cakbubeting apparatus | |
| US1184541A (en) | Carbureter. |