Ensign Carburetor Co. v. Zenith-Detroit Corp.

36 F.2d 684, 4 U.S.P.Q. (BNA) 3, 1929 U.S. App. LEXIS 2239
CourtCourt of Appeals for the Second Circuit
DecidedDecember 9, 1929
DocketNo. 50
StatusPublished
Cited by13 cases

This text of 36 F.2d 684 (Ensign Carburetor Co. v. Zenith-Detroit Corp.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Second Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Ensign Carburetor Co. v. Zenith-Detroit Corp., 36 F.2d 684, 4 U.S.P.Q. (BNA) 3, 1929 U.S. App. LEXIS 2239 (2d Cir. 1929).

Opinion

MANTON, Circuit Judge.

This suit is for infringement of a patent granted to Ensign on August 26, 1924, on an application filed September 30, 1916, for a carburetor. The carburetor is used for mixing liquid fuel and air in proper proportions to provide combustible mixture for use in the engine cylinders. By the reciprocation of the piston cylinders, a stream of air is drawn through the carburetor and creates a suction. As tbe [685]*685stream passes through the carburetor, it picks up the necessary amount of liquid fuel to provide the air-fuel mixture desired. The carburetor of the appellant’s patent provides fuel reservoirs for two different fuels. The upper reservoir is for gasoline, to be used only in starting, and the lower reservoir is for kerosene, which is intended to be used as the main fuel. At the bottom a reservoir is provided for water, which is added to the mixture when kerosene is used.

Appellant’s carburetor has a down-flow jet, as distinguished from the up-flow jet, but operates on the same principle. The fuel level maintained within the reservoir is slightly below the top edge 65 of the tube 2. When the engine is stationary, there will be no fuel flow from the reservoir over the edge 65 of the tube 2, but when the engine is in operation, the suction produced by it in the vortex or mixing chamber reduces the pressure at the jet and in the suction tube. The result is the higher pressure on the surface of the fuel in the reservoir forces the fuel to flow through the openings 7 and passage 64, the tube 2, and the jets 2" into the vortex chamber, where it is mixed with the air entering through the main inlet 22 to form the desired combustible mixture for the engine. This is illustrated on Mg. 1 of the drawings. The air-bleeding of the jet of appellant’s patent is through the air opening or openings 26, shown in Mg. 1, which is connected through the normally closed valve 27 with the suction chamber. The valve is automatically actuated by the suction in the suction chamber. As the suction increases, and this is due to the increased engine speed, the valve 27 is automatically raised to permit air to enter through it into the suction chamber, thereby reducing the suction in that chamber and in the suction tube 2, and preventing the enriching of the air-fuel mixture which would otherwise result from the increased suction.

The novelty of the patent in suit resides in the interconnecting of the three air openings 22, 26, and 32, so as to maintain constant pressure relations between them, and therefore uniform air-fuel mixture, irrespective of any pressure changes that might be imposed by the main air inlet by the application to it of an air strainer. In a carburetor the rate of flow of fuel through the jet is dependent upon the pressure difference between the jet and the fuel reservoir, and therefore anything that changes the pressure at one of these points, without changing it correspondingly at the other will alter the rate of flow of the fuel, and alter the proportion of fuel to air in the mixture. If the main air inlet is restricted by placing over it an air strainer or in any other way, the pressure within the main air pipe inlet and at the jet will be reduced. If the fuel reservoir is maintained at atmospheric pressure through its air vent, there will be an increase in the fuel propelling pressure difference, and therefore the rate of fuel flow and the mixture will become richer. If air is fed under pressure to the air inlet as by a supercharger, the pressure at the jet will be increased, and the fuel propelling pressure difference decreased, thereby thinning the mixture.

These difficulties were appreciated in the art and had been overcome by the expedient of connecting the fuel reservoir vent to the main air inlet, or doing what is referred to as interconnecting or balancing the air openings of the carburetor. By the use of such balancing system, the fuel propelling pressure difference, and therefore the composition of the mixture, are maintained substantially constant, irrespective of changes of pressure imposed by the main air inlet. Different engine speeds and loads were found to interfere with the uniformity of the mixture; for increase in the engine suction increased the amount of fuel fed in proportion to the air, therefore enriching the mixture, and it became necessary to add more air to the mixture at high speeds.

This problem admittedly was solved before the patent in suit. Mrst, as disclosed in the Krebs patent, No. 734,421, it was solved by supplying the mixing chamber at a point beyond the fuel jet, and gradually increasing the volume of air as the speed of the engine increased, thereby compensating for the increased supply of fuel; second, it was oyercome by supplying air to the fuel before its delivery into the mixing chamber of the carburetor, so that the gradually increasing quantity of fuel would be compensated by mixing it with a correspondingly increasing volume of air, which is known as air-bleeding the fuel jet. The appellant adopted this air-bleeding arrangement in the design of the carburetor constructed under the patent in suit. The third solution was a compensating jet arrangement, which consists in combining with the gradually 'increasing delivery of fuel, a compensating stream of air and fuel which'stream becomes leaner with the speed of the engine. See patent to Baverey, No. 908,953. This compensating jet arrangement is employed in the appellee’s carburetor. Therefore the problem of compensating for the tendency of the carburetor to deliver a mixture of increasing richness as the speed [686]*686of the engine increased, had been successfully solved before the invention of the patent in suit.

In the appellant’s patent, the liquid fuel reservoir has a vent opening to the atmosphere and is provided with a constant level device, which maintains the level in the reservoir and in the nozzle. The orifice or jet of the nozzle is slightly above the level in the reservoir. When the engine is idle, there will be no flow of fuel through the jet; but, when the motor is running, the suction produced by it draws air through the air inlet past the jet, and reduces the pressure at that jet below atmospheric. The pressure difference which is thus produced between the jet and the fuel reservoir causes the fuel to flow through the jet at a rate dependent upon the pressure difference and to mix with the air • stream on the way to the cylinder. The appellant argues that the need of a clarifier which would strain the air, supply it to a carburet- or, and protect it and the engine, and which would not produce an unbalanced condition in the carburetor, and thereby disturb the mixture ratio, with consequent inefficient results, presented a problem entirely different and independent from that previously presented by reason of the tendency of combustible mixture to become enriched as the demands of the engine increased; that it matters not how perfectly the earburetion maintained, the desired fuel ratio, by compensating for the tendency of the mixture to increase in riehness with the speed of the engine, would be unbalanced when the air cleaner is applied to the intake.

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Bluebook (online)
36 F.2d 684, 4 U.S.P.Q. (BNA) 3, 1929 U.S. App. LEXIS 2239, Counsel Stack Legal Research, https://law.counselstack.com/opinion/ensign-carburetor-co-v-zenith-detroit-corp-ca2-1929.