US2153350A - Auxiliary air intake for internal combustion engines - Google Patents
Auxiliary air intake for internal combustion engines Download PDFInfo
- Publication number
- US2153350A US2153350A US155715A US15571537A US2153350A US 2153350 A US2153350 A US 2153350A US 155715 A US155715 A US 155715A US 15571537 A US15571537 A US 15571537A US 2153350 A US2153350 A US 2153350A
- Authority
- US
- United States
- Prior art keywords
- carburetor
- internal combustion
- auxiliary air
- combustion engines
- opening
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
-
- 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
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/13—Special devices for making an explosive mixture; Fuel pumps
- F02M2700/1305—Auxiliary air supply devices for carburettors
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- 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
- Y10S55/00—Gas separation
- Y10S55/28—Carburetor attached
Definitions
- My invention relates to auxiliary air intakes for internal combustion engines, and its principal object is to provide means whereby an additional supply of pure air may under certain conditions be admitted to the intake manifold of the engine independently of the supply of gaseous mixture furnished by the carburetor, the amount of additional air being primarily controlled by the accelerator mechanism with its associated butterfly valve.
- Another object of my invention is to provide a device of the character referred to which is seeondarily controlled by the temperature of the engine.
- a further object of my said invention is to provide a device of the character referred to which is constructed as a unitary structure adapted to be inserted between the co-acting flanges of the carburetor and the intake manifold, so that it may be easily and quickly applied to an engine without any changes or modifications of the existing parts.
- Figure 2 is a transverse section taken on line 2-2 of Figure 1.
- Figure 3 is a longitudinal section of my device taken on line 3-3 of Figure 2 and drawn to an enlarged scale.
- Figure 4 is a plan view of the same in section on line 44 of Figure 3, and
- Figure 5 is a section on line 5--5 of Figure 3 illustrating certain details of the device.
- I designates the body of an engine provided with the usual intake manifold 2 and exhaust manifold 3, while 4 indicates the lower. portion of a down-draft carburetor of conventional construction.
- a member 5 Between the flange ll of the carburetor and the coacting flange 2
- is an elongated opening or slot 52 into which is inserted, by pressure or other means, the inner end 6
- the body 6 in its central portion is of cylindrical shape formed from a tube of such dimensions that when its inner end is flattened, as at 6
- the screen 63 may be held in position in various ways such as the overturned or 10 beaded edge 64 shown.
- Journaled in openings in the body 6 is a transverse shaft 1 which passes diametrically through the opening and carries a butterfly valve 1
- a lever 12 one end of which is connected by a rod 13 to a lever 8, the latter forming a part of the ordinary accelerator mechanism which controls the butterfly valve 42 of the carburetor and is operated through the accelerator rod 8
- the lever 12 has an extension H to which is connected one end of a helical tension spring 15, the other end of which is secured to a pin Hi carried'by a bracket 65 upon the body 6. It will be seen that by this arrangement depression of the accelerator rod 8
- thermostatic devices there is provided upon the shaft 9 the lever 92 having a slot 93 in which engages the free end
- the thermostat shown is of the type in which the spiral uncoils with rise of temperature, but obviously my 5 device may be adapted for use with other forms of thermostat.
- the screen 43 of wire mesh is inserted in a rebate in the upper surface of the member so as to be clamped between the said member and the flange 4
- An auxiliary air inlet device for internal combustion engines comprising a gasket adapted to flt between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
- An auxiliary air inlet device for internal combustion engines comprising a gasket adapud to flt between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening, the cylindrical bore merging gradually into said slot; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
- An auxiliary air inlet device for internal combustion engines comprising a gasket adapted to fit between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening, the cylindrical bore merging gradually into said slot and the said opening being closed by a dust screen; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Description
April 4, 1939. E STIMAC 2,153,350
AUXILIARY AIR INTAKE FOR UZ'E'ITRNAL COMRUS'TTON ENGTNFS Filed July 26, 1937 PatantedApnQlM,
UNITED STATES PATENT OFFICE Emil Stimac, Detroit, Mich.
Application July 26. 1937, Serial No. 155,715
3 Claims. (Cl. l23- -119) My invention relates to auxiliary air intakes for internal combustion engines, and its principal object is to provide means whereby an additional supply of pure air may under certain conditions be admitted to the intake manifold of the engine independently of the supply of gaseous mixture furnished by the carburetor, the amount of additional air being primarily controlled by the accelerator mechanism with its associated butterfly valve.
Another object of my invention is to provide a device of the character referred to which is seeondarily controlled by the temperature of the engine.
A further object of my said invention is to provide a device of the character referred to which is constructed as a unitary structure adapted to be inserted between the co-acting flanges of the carburetor and the intake manifold, so that it may be easily and quickly applied to an engine without any changes or modifications of the existing parts.
With these and other objects in view, I will now describe a preferred embodiment of my invention with reference to the accompanying drawing, in which- Figure 1 is a fragmentary front elevation of an engine showing my device applied thereto.
Figure 2 is a transverse section taken on line 2-2 of Figure 1.
Figure 3 is a longitudinal section of my device taken on line 3-3 of Figure 2 and drawn to an enlarged scale.
Figure 4 is a plan view of the same in section on line 44 of Figure 3, and
Figure 5 is a section on line 5--5 of Figure 3 illustrating certain details of the device.
Like characters designate corresponding parts throughout the several views.
Referring more particularly to Figures 1 and 2 of the drawing, I designates the body of an engine provided with the usual intake manifold 2 and exhaust manifold 3, while 4 indicates the lower. portion of a down-draft carburetor of conventional construction. Between the flange ll of the carburetor and the coacting flange 2| of the intake manifold is inserted a member 5, the shape of which in general corresponds to that of the said flanges including openings 5| through which the usual connecting bolts are designed to pass. Within the face of the member 5| is an elongated opening or slot 52 into which is inserted, by pressure or other means, the inner end 6| of the tubular body 6.
The body 6 in its central portion is of cylindrical shape formed from a tube of such dimensions that when its inner end is flattened, as at 6|, the flattened portion will flt tightly into the opening 52 in the member 5, while the outer end of the body is flared or bell-mouthed, as indicated at 62, so as to form an inlet opening of relatively large area which is protected from the entrance of dust and dirt by a wire mesh screen 63. The screen 63 may be held in position in various ways such as the overturned or 10 beaded edge 64 shown. Journaled in openings in the body 6 is a transverse shaft 1 which passes diametrically through the opening and carries a butterfly valve 1| designed, when required, to provide a total closure for the body. To the shaft 1 is secured a lever 12, one end of which is connected by a rod 13 to a lever 8, the latter forming a part of the ordinary accelerator mechanism which controls the butterfly valve 42 of the carburetor and is operated through the accelerator rod 8| by any of the usual means well known in the art. The lever 12 has an extension H to which is connected one end of a helical tension spring 15, the other end of which is secured to a pin Hi carried'by a bracket 65 upon the body 6. It will be seen that by this arrangement depression of the accelerator rod 8|, opening the butterfly valve 42, will also tend to open the valve H, the relative movement and timing of the two vales being adjustable by various means such as the series of openings 83 in the lever B in which the rod I3 may selectively engage.
It is well known that in order to obtain the best results as regards increase of power and. economy of fuel in a device of this character, the amount of additional air admitted must be varied more or less according to the temperature of the engine,
and with this in view I have incorporated in my device a butterfly valve 9| mounted upon a shaft 9 which is adapted to be operated by any of the well known thermostatic devices. In the present example there is provided upon the shaft 9 the lever 92 having a slot 93 in which engages the free end |0| of a thermostat ill, the said thermostat being in the form of a bimetallic spiral having its inner extremity fixed to a pin I02 carried upon a bracket I03 secured to the exhaust manifold 3 as shown in Figures 1 and .2. The thermostat shown is of the type in which the spiral uncoils with rise of temperature, but obviously my 5 device may be adapted for use with other forms of thermostat. By the arrangement shown, increase of temperature in the engine causes opening of the valve 9|, the latter being normally held in closed position by a helical tension spring ll. one end of which is connected to an extension '4 upon the lever 92, while the other end is secured to a pin 06 carried by the bracket 65.
It will be observed from the foregoing description and by reference to the drawing that I have provided a device which is eminently adapted to the purpose set forth, and while I have herein shown a preferred embodiment of my invention, it will be understood by those skilled in the art to which the same relates that various modifications may be made in detail as required in order to adapt the device to engines of various makes and operating characteristics, so that the proper adjustment for each individual engine and its associated carburetor will result in a considerable increase in power and economy of operation.
In order to insure proper mixing of gas and air issuing from the carburetor, the screen 43 of wire mesh is inserted in a rebate in the upper surface of the member so as to be clamped between the said member and the flange 4| of the carburetor.
Having thus described my said invention, what I claim and desire to secure by Letters Patent of the United States is:
1. An auxiliary air inlet device for internal combustion engines comprising a gasket adapted to flt between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
aisasso 2. An auxiliary air inlet device for internal combustion engines comprising a gasket adapud to flt between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening, the cylindrical bore merging gradually into said slot; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
3. An auxiliary air inlet device for internal combustion engines comprising a gasket adapted to fit between the opposed flanges of a carburetor delivery conduit and of a manifold intake conduit, said carburetor delivery conduit being controlled by a throttle valve the said flange having an opening continuous with the bores of said conduits, and having an elongated slot substantially circumferentially disposed with respect to said opening; a cylindrical member having one end flattened and secured within said slot and having at the other end a bell-mouthed inlet opening, the cylindrical bore merging gradually into said slot and the said opening being closed by a dust screen; a butterfly valve pivotally mounted within said member and operatively connected to the throttle valve operating mechanism of the carburetor; and a second butterfly valve similarly mounted within said member and operated by a thermostatic element mounted adjacent the exhaust manifold of the engine.
EMIL- STIMAC.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US155715A US2153350A (en) | 1937-07-26 | 1937-07-26 | Auxiliary air intake for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US155715A US2153350A (en) | 1937-07-26 | 1937-07-26 | Auxiliary air intake for internal combustion engines |
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US2153350A true US2153350A (en) | 1939-04-04 |
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US155715A Expired - Lifetime US2153350A (en) | 1937-07-26 | 1937-07-26 | Auxiliary air intake for internal combustion engines |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613658A (en) * | 1946-01-15 | 1952-10-14 | Carter Carburetor Corp | Charge forming device |
US2884954A (en) * | 1957-03-25 | 1959-05-05 | Frederick S Roberts | Gasoline economizer valve |
US3168085A (en) * | 1963-06-26 | 1965-02-02 | William M Stelter | Carburetion optimization structure |
US3452521A (en) * | 1967-05-05 | 1969-07-01 | Aloys L Remacle | Air filter with supplemental air inlet |
US4019476A (en) * | 1975-03-31 | 1977-04-26 | Ackley Donald M | Vaporizer apparatus |
US4083337A (en) * | 1975-07-16 | 1978-04-11 | Nippon Soken, Inc. | Air-fuel ratio adjusting system |
US4476819A (en) * | 1982-03-15 | 1984-10-16 | Szloboda David Tibor | Fuel economy device |
WO1985001317A1 (en) * | 1983-09-23 | 1985-03-28 | Sonex Research Inc. | Process for carrying out radical-enhanced combustion in i.c. engine |
US4574764A (en) * | 1982-04-23 | 1986-03-11 | Earle John L | Fuel vaporization method and apparatus |
US6431141B1 (en) * | 2000-04-27 | 2002-08-13 | Daimlerchrysler Corporation | Secondary wide open throttle induction system |
US20130269584A1 (en) * | 2010-07-27 | 2013-10-17 | Keum Dae Choo | Polar vessel having a derrick |
US9205894B2 (en) | 2010-11-04 | 2015-12-08 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Sealed derrick structure for polar vessels |
US9297545B2 (en) | 2010-11-04 | 2016-03-29 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Damper structure for a sealed derrick |
US9377369B2 (en) | 2010-11-19 | 2016-06-28 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Temperature and pressure monitoring system of sealed derrick structure |
US9862474B2 (en) | 2010-07-27 | 2018-01-09 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Ventilation apparatus of a drillship |
US11105238B2 (en) * | 2019-12-06 | 2021-08-31 | Hyundai Motor Company | Device for screening NOX sensor |
-
1937
- 1937-07-26 US US155715A patent/US2153350A/en not_active Expired - Lifetime
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613658A (en) * | 1946-01-15 | 1952-10-14 | Carter Carburetor Corp | Charge forming device |
US2884954A (en) * | 1957-03-25 | 1959-05-05 | Frederick S Roberts | Gasoline economizer valve |
US3168085A (en) * | 1963-06-26 | 1965-02-02 | William M Stelter | Carburetion optimization structure |
US3452521A (en) * | 1967-05-05 | 1969-07-01 | Aloys L Remacle | Air filter with supplemental air inlet |
US4019476A (en) * | 1975-03-31 | 1977-04-26 | Ackley Donald M | Vaporizer apparatus |
US4083337A (en) * | 1975-07-16 | 1978-04-11 | Nippon Soken, Inc. | Air-fuel ratio adjusting system |
US4476819A (en) * | 1982-03-15 | 1984-10-16 | Szloboda David Tibor | Fuel economy device |
US4574764A (en) * | 1982-04-23 | 1986-03-11 | Earle John L | Fuel vaporization method and apparatus |
WO1985001317A1 (en) * | 1983-09-23 | 1985-03-28 | Sonex Research Inc. | Process for carrying out radical-enhanced combustion in i.c. engine |
US6431141B1 (en) * | 2000-04-27 | 2002-08-13 | Daimlerchrysler Corporation | Secondary wide open throttle induction system |
US20130269584A1 (en) * | 2010-07-27 | 2013-10-17 | Keum Dae Choo | Polar vessel having a derrick |
US9376199B2 (en) * | 2010-07-27 | 2016-06-28 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Polar vessel having a derrick |
US9862474B2 (en) | 2010-07-27 | 2018-01-09 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Ventilation apparatus of a drillship |
US9205894B2 (en) | 2010-11-04 | 2015-12-08 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Sealed derrick structure for polar vessels |
US9297545B2 (en) | 2010-11-04 | 2016-03-29 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Damper structure for a sealed derrick |
US9377369B2 (en) | 2010-11-19 | 2016-06-28 | Daewoo Shipbuilding & Marine Engineering Co., Ltd. | Temperature and pressure monitoring system of sealed derrick structure |
US11105238B2 (en) * | 2019-12-06 | 2021-08-31 | Hyundai Motor Company | Device for screening NOX sensor |
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