In re Saurer

118 F.2d 719, 28 C.C.P.A. 1021, 49 U.S.P.Q. (BNA) 78, 1941 CCPA LEXIS 55
CourtCourt of Customs and Patent Appeals
DecidedMarch 31, 1941
DocketNo. 4424
StatusPublished
Cited by1 cases

This text of 118 F.2d 719 (In re Saurer) is published on Counsel Stack Legal Research, covering Court of Customs and Patent Appeals primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
In re Saurer, 118 F.2d 719, 28 C.C.P.A. 1021, 49 U.S.P.Q. (BNA) 78, 1941 CCPA LEXIS 55 (ccpa 1941).

Opinion

Jackson, Judge,

delivered the opinion of the court:

This is an appeal from a decision of the Board of Appeals of the United States Patent Office, affirming that of the Primary Examiner rejecting, in view of the prior art, claim 6, the only claim, of an application for a patent for improvement in the method of and apparatus for forming the explosive mixture in direct injection high speed internal combustion engines.

The claim reads as follows:

6. The method of forming the explosive mixture in a self-igniting direct injection high speed internal combustion engine, in which the piston is provided in its head with a toroidal combustion chamber having a restricted opening, the method comprising compressing air between the piston and the cylinder head and forcing it towards the opening in the piston head, injecting a quantity [1022]*1022of .fuel into the cylinder qver the top of the piáton as the piston approaches the head of the cylinder to form a partly mixed fuel combustion charge and reduce the ignition lag by the rapid heating of the fuel in the counter-current of hot air, continuing the fuel injection into the toroidal combustion chamber until the piston approaches the end of its compression stroke, compressing the partly mixed fuel charge and air between the piston and the cylinder head, and forcing the partly mixed charge into ithe toroidal combustion chamber to be completely mixed therein, the fuel being discharged from the nozzle at the beginning of injection in a relatively flat continuous veil across the inflow of air and continued in both the cylinder and the combustion chamber and impinging at the beginning of injection against the air as it flows over the piston head toward the restricted opening therein, and the partly mixed fuel charge and air above the piston head flowing over the piston head toward the restricted opening therein, entering the combustion chamber in the piston head crosswise to the flow of the fuel from the nozzle into the combustion chamber, and entering and whirling within the combustion chamber to complete the mixing of the fuel charge.

The references relied on are:

French, 1,708,056, April 9, 1929;
Saurer (British), 421,101, December 13, 1934;
Saurer (British), 448,758, June 15, 1936.

In the words of the examiner:

The alleged invention relates to a method of forming explosive mixtures in high-speed fuel injection internal combustion engines of the precombustion chamber type. The precombustion chamber is formed in the piston head in the form of a recess, with a restricted opening establishing communication between the precombustion chamber and the cylinder space or the main combustion chamber.

The drawings of the application reproduced below show the type of device in which the method of the appealed claim is carried out: In the drawings the reference numerals are read as follows: Numeral 1 indicates the piston which travels in the cylinder 2; a precom-bustion chamber 3, called by the appellant because of its shape a toroidal combustion chamber, is in the head of the piston; this cham[1023]*1023ber communicates with the compression space between the piston and the cylinder head 6 through restricted opening 5; the fuel nozzle body 1 is retained in the cylinder head by a plug 8; the stem 10 of the mushroom fuel injection valve 11 is slidably within a central bore 9 of the nozzle body, the valve being held normally to its seat against the thin annular tip of the nozzle body by a spring 12; fuel enters through duct 13 into the chamber containing the spring thence through longitudinal grooves 14 in the stem 10 to the valve tip. The fuel injection nozzle 7 placed in line with the axis of opening 5 discharges a substantially flat disk-shaped fuel jet.

In Fig. 1 the piston is shown in a position approaching the top •dead center, but is not close enough to the cylinder head to permit the nozzle to enter the precombustion chamber 3. In Fig. 2 the piston is shown to have reached its highest position with the fuel injection nozzle 11 within the chamber 3.

As indicated by arrows in the drawings, as the piston rises on its compression stroke air is forced into the chamber 3 and is deflected by the walls of the chamber to create a whirling turbulence therein. Before the nozzle tip enters the opening of chamber 3, at a predetermined time fuel injection is started and the fuel jet meets and mixes with the air in the main combustion chamber before it enters into chamber 3. This is shown in Fig. 1. As the compression stroke of the piston continues the nozzle tip enters the chamber 3 and the flat disk-shaped fuel jet so intimately mixes with the whirling air and fuel mixture in the chamber that complete combustion is said to occur during the time of the combustion process.

The object of appellant’s alleged invention is to secure formerly unattainable reduction of ignition lag and unpredictable efficiency in fuel combustion. The manner in which this is said to be accomplished is contained in the following portion of the application:

* * * The fuel injected in the form of a relatively flat conical film or veil, produced by a film nozzle at the beginning of the injection and while the nozzle opening is still outside of the combustion chamber in the piston, that is, in the first part of the injection, meets the combustion air above the piston head in counter-flow, while in the second part of the injection, which takes place after the nozzle enters the combustion chamber, the fuel continues to be injected in the combustion chamber crosswise with respect to the air eddy, and thereby the shortest ignition lag is attained with complete combustion. Because of the high position of the injection orifice and the early commencement of injection required by high speed engines it follows that the injector during the initial stages of injection has not yet entered the combustion chamber provided in the piston head but sprays the fuel against the heated air as it flows over the piston head toward the central restricted opening. As the piston then approaches further toward the top dead center position, the nozzle enters the combustion chamber in the piston and sprays the fuel within the combustion chamber crosswise to the current of entering air and to the eddy formed within the chamber. By the operation of the engine in this manner, that is, with the injection beginning before the nozzle enters the combustion chamber and con-[1024]*1024tinning after the nozzle has entered the combustion chamber, it becomes possible to attain smooth operation of the engine and completely smoke-free combustion, even in small spray injection engines.

The earlier British patent- discloses a device substantially similar to that of the present application. In this patent a multi-jet tip in an atomizing nozzle is provided. The later British patent contains a drawing Fig 1 which is identical even to the reference numerals with Fig. 2 herein. This patent discloses a nozzle with a flat tip through which, while the engine is in operation, the fuel issues as a mist hi the shape of a flat cone, thus plainly suggesting, if not actually providing for, a nozzle tip producing a flat “veil shape” fuel jet. Neither of the British patents shows a specific timing for the fuel injection.

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Related

Application of Arthur E. Middleton and Donald C. Reynolds
319 F.2d 552 (Customs and Patent Appeals, 1963)

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Bluebook (online)
118 F.2d 719, 28 C.C.P.A. 1021, 49 U.S.P.Q. (BNA) 78, 1941 CCPA LEXIS 55, Counsel Stack Legal Research, https://law.counselstack.com/opinion/in-re-saurer-ccpa-1941.