US1312040A

US1312040A - Henri

Info

Publication number: US1312040A
Authority: US
Publication date: 1919-08-05
Anticipated expiration: 1936-08-05

Description

H. MERCIER.

AUTOMATIC THROTTLE FOR HIGH-COMPRESSION MOTORS;

APPLICATION FILETI MAR. 28.1919.

Patented Aug. 5, 1919.

III/

ED STATES PATENT OFFICE.

HENRI MERCIER, OI PARIS, FRANCE.

AUTOMATIC THROTTLE FOR HIGH-COM PQESSION MOTORS.

iam,

Specification of Letters Eatent.

Patented Aug. 5,1919.

Application filed larch 28, 1919, Serial No. 285,924.

' To all whom it may concern:

tors, intended to work at difi'erent altitudes,

and particularly tothe motors of aircraft and to certain automobile motors.

The object of the invention is to permit the construction of high compression mo tors possessing the maximum output at the same altitude at which it is considered that they ought to work most ordinarily, while obviating the disadvantages of high compression when these motors have to work at lower altitudes.

It is known that in order to mitigate these disadvantages, it suflices to create a loss of charge which reduces the tension of the gases supplying the motor. This result is obtained by operating, for example, a butterfly valve placed in the suction pipe of the motor, and it is thus, generally,- that the flying pilot-s proceed, in orderto ease down,

on the ground, their high compression motors. Such o 'eration-is however, not very accurate, it emands a certain amount of attention on the part of the pilots, and if it be not done correctly, the explosions become shattering and dangerous. In consequence of these disadvantages, the designers of motors are unable, for the sake of safety, to provide for as great compression of the charge as would be desirable in order to insure the maximum of their output at high altitudes. V

By the use of the throttle device, constructed according to the present invention,

the flying ilots do not have to concern themselves with anything during flight, and the designers are able to provide for as great a compression of the charge within the motors as is desirable.

The invention consists in placi an automatic throttle in the direction 0 the sucdiagrammatically and by one of the forms of the invention.

tion pipe of the motor, this throttle being such that its operation remains, within certain limits, independent of the variations of the atmospheric density.

The accompanying drawings represent, way of example,

lFigure 1 shows in longitudinal section, the automatic throttle. 4

Fig. 2 is a section on the line AA. of the same throttle.

In these figures, 1 represents the body of the throttle, 2 is the pipe connecting it to the suction pipe of the motor, 3 is anauxiliary butterfly valve adapted to be operated by hand, 4: is the pipe for connection to the carbureter, which is, in this case, preferably an automatic one.

-'lhe body of the throttle is divided into three chambers 5, 6, 7, by two division walls 8 and 9 which are perforated, provided with guide sockets 10 and i1 and it is closed at its end by a bottom 12.

l A cylindrical slide valve or piston 13 is adapted to slide with slight friction in the sockets 10 and 11 and is terminated at both til Ill

ends by covers 14 and '15 and its cylindrical walls are pierced with openings 16 of a special form,

A spring 17 suitably tensioned, holds the slide valve 13- up against the bottom 12.

The chamber 5- communicates with the motor, the chamber 6 communicates with the carbureter and the chamber 7 is filled with oil and communicates by a narrow'pipe 18 with a reservoir 19 artly full of oil and artly full of air. T e oil may be replaced by glycerin or by any other suitable liquid.

The reservoir 19 is provided with a cock 20 opening into the outer atmosphere. The reservoir 19 may be surrounded by a heat retaining jacket 21 and an electrical heating circuit 22.

,The working 'of a; throttle applied, for

exam 1e, to an airship motor, is as follows: Let the throttle be supposed to be in the position shown in thedrawing and the airship resting on the ground. The cock- 20 is opened, and then If it has not already been so the spring 17*is tensioned to exert upon the bottom 14 a force equal to the difference of the pressures which the surrounding atmosphere exerts upon this same bottom and which the lessdense atmosphere would exert at the altitude considered.

The motor is then started up. Under these conditions, and under the action of the suction of the motor, the slide valve 13 thrust forward by' the atmospheric pressure 5 moves toward the left of the figure. The

openings 16 put the chamber 6 into throttled communication with the chamber 5, and

. the restriction of the gaseous current passing through the openings 16, which is controlled 10 by the spring 17, is such that the high compression motor has its compression reduced and works normally notwithstanding the excess of surrounding atmospheric density.

If, at this moment, the airship is to leave the earth to rise to the considered altitude, the slide valve, thrust forward less and less by the decreasing atmospheric pressure, will return gradually toward the right under the action of the spring 17 the motor, the pressure of which is reduced, slows down more and more and ends even by ceasing to work. But it will no longer be the same if, before leaving the earth, the flying pilot closes the cock 20. By this simple operation, he renders the working of the throttle and at the same time that of the motor, independent of the atmospheric density from the earth up to the considered altitude. In reality the volume of .air, which-is relatively important, thus inclosed in the reservoir 19, and incapable of escaping, exerts upon the bottom 15, through the medium of the oil the pressure necessary to the correct working of thethrottle and this pressure remains invariable when the airship attains high altitudes.

In order to take into account'variations of I temperatures which would have the effect of causing the tension of the volume of air inclosed in the reservoir 19 to vary in a certain measure, a heat retaining jacket 21 may be provided and even a heating circuit 22 worked by-the lighting dynamo of the airship, the intensity of the current being con trolled by a temperature regulator.

The object of providing a butterfly valve 3 worked by hand is to enable the motor to have its compression reduced by creating a supplementary loss of charge and, consequently, to enable the motor to be rotated 50 at a lower speed. This butterfly valve serves likewise in case of the failure of the automatic system. Y

The provision of a volume of oil transmitting to the slide valve or'piston 13, through a narrow pipe 18, the pressure exerted by the air in the'reservoir'19, has for its object to avoid leakages of air and also to stop the oscillatory. movements. of an alternating kind which the slide valve or piston 13 might acquire under. the action of the intermittent suctions of-the motor.

The invention is not limited to'the constructional forms described, and in particular the spring may be so arranged that the pressure in the reservoir is capable of assuming all values greater or less than the pressure indicated by way of example in the present specification. A partial or total vacuum may be created and maintained in the reservoir 19 by any method, or on the contrary, the reservoir may be supplied under pressure. The necessary thrust upon the volume of oil may be obtained, independently of the atmospheric density, by any suitable means, other than the pressure of a gas, as for example by mechanical means such as centrifugal force.

I claim:

1. An automatic throttle for high compression motors, interposed between the motor and its carbureter, comprising a slide valve controlling the admission of gas from the carbureter to the motor, a spring acting on one side of said valve and tending to maintain the same closed, an air confiner communicating with the other side of the valve, whereby the air pressure tends to move the valve in the opposite direction against the tension of the spring and to open the same.

2. An automatic throttle for high compression motors, interposed between the motor and its carbureter, comprising a slide valve controlling the admission of gas from the carbureter to the motor, a spring acting on one side of said valve and tending to maintain the same closed, an air confiner communicating with the other side of the valve, whereby the pressure tends to move the valve in the opposite direction against 10 the tension of the spring and open the same, and means for controlling the pressure in said confiner.

3. An automatic throttle for high compression motors, interposed between the inotorand its carbureter, comprising a slide valve controlling the admission of gas from the carbureter to the motor, a spring acting on one side of said valve and tending to maintain the same closed, an air confiner communicating with the other side. of the valve, whereby the pressure tends to move the valve in the opposite direction against the tension of the spring and open the same, and means for regulating the temperature in the confiner.

4. An automatic throttle for high compression motors interposed between the motor and carbureter, comprising a slide valve controlling the admission of gas from 12 the carbureter to the motor, means tending to maintain said valve closed, said means acting on one end of the valve, an air confiner, and a fluid interposed between the air confiner and the oppsite end of the valve,

whereby the pressure of the air is transmitted through the fluid to move the valve in the opposite direction.

5. An automatic throttle for high compression motors interposed between the Lemme motor and carburetor, comprising a slide valve controlling the admission of gas from the carburetor to the motor, means tending to maintain said wrive closed, said means acting on one end of the valve, an air con-"- finer, and a fluld mterposed between the ear confiner and the opposite end of the valve,

whereby the pressure of theair is transmitted'through the fluid to move the valve in the opposite direction, and means for es 10 tabli shing and destroying communication between the air confiner-and the atmosphere. In testimony WhGI'BOfI afiix my. si

atu-re. k HENRI MER IER.