US970153A - Combustion-engine plant for submarine craft. - Google Patents

Combustion-engine plant for submarine craft. Download PDF

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US970153A
US970153A US34275706A US1906342757A US970153A US 970153 A US970153 A US 970153A US 34275706 A US34275706 A US 34275706A US 1906342757 A US1906342757 A US 1906342757A US 970153 A US970153 A US 970153A
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air
cylinder
cylinders
working
combustion
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US34275706A
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Paul Winand
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders

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  • afour-stroke cycle engine might be operated without an air pump, the air being drawn in from thev atmosphere directly by the pistons o't' the exigirle; in such a case however the pressure duc to compression would be less and the economy o't tuel less than when using some ot' the cylinders as air pumps. Moreover the power obtained would be less since the cylinders used as pumps will take in air at every revolution while in vthe working cylinders the pistons will likewise draw in air in the usual fashion.
  • T he other cylinders are arranged to work as above with a larger charge, lilling the cylinders at a higher pres- Isure1 and they are used for obtaining a higher rate ol' speed.
  • both this set ol' cylinders and the other set may be working at the same time and thus the highest rate of power and of speed may be obtained it' desired.
  • Yi'hen running at the surface i. c. with air, the cylinders ⁇ ol the iirst. set, or some ot' them, are used as air pumps for the other set, when a higher rate than the cruising speed is desired.
  • the power thus'attainable is naturally less than that. attainable when working under exclusion ot' the atn'iospheric air. This however is an advantage as a high rate of speed is not practicable with a submarine cral't running at the surface.
  • cylinder 2 serves as t-he working cylinder and cylinder 1 as the air vpump or charging pump.
  • the piston of cylinder l draws in air through the two-Way cock 3 and the valve et, and, on the return stroke, forces it through the valve 5 and two-way cock 6 to the cylinder 2, intov which it enters through the ports 7, when the piston of cylinder 2 approaches the outermost limit of its stroke.
  • the'piston of cylinder 2 has drawn in air through the two- Way cock 8 and valve 9, which air at this juncture fills the cylinder, under atmospheric pressure.
  • both cylinders serve as working cylinders.
  • either the one o-r the other cylinder may serve as the Working cylinder.
  • cylinder 1 may serve as the Working cylinder
  • cylinder 2 runs entirely idle.
  • oxygen is admitted through the pipe land receptacle 14; the cock 6 is so set that residual gases from the cylinder may enter the receptacle through t-he valve 5, and the cock 3 is so set that a. mixture of residual gases and oxygen may enter the cylinder from the receptacle through the valve y 4.
  • a portion ofthe residual gases isv not returned to the cylinder, but escapes through the valve 15, which is so loaded that-the cylinder 1 after the suction stroke,
  • a combustion engine plant for submarine craft comprising a'multiple combustion-engine, a pressure receptacle for storing under pressure an oxygenating ele- 'ment, connections for supplying the explosive charge to one of the cylinders at a pressure of the charge before compression equal or nearly equal to that of the atmosphere and for cutting off the supply to the other cylinder so that the engine may operate at reduced -power (as, for instance, at cruising speed), and connections for supplyin g air to the second cylinder, when a greater amount of poWeris desired and pumping air therefrom into the explosive charge of the first cylinder at a pressure of the charge before compression greater than that of the atmosphere; substantially as described.
  • a combustion engine plant for submarine craft comprising a multiple cylinder combustion engine, connections for supplying fuel to the several cylinders thereof, connections for supplying atmospheric air to said cylinders, connections for supplying under-pressure an artificial oxygenating .elementth-ereto, a connection between individual cylinders, and cut-offs for all of said4 connections; whereby'- the several cylinders- ,may all operate conjointlyl asexpolosion cylinders either with air or with the arti- 'In testimony whereof I have axed my ciaI oxygenating element as the oxidizer signature, in presence of two witnesses.
  • any individual eylinder may serve I PAUL' WINAND' as an air pump to convey air under com- witnesseses: y pression into the explosion chamber of any BESSIE F. DUNLAP,

Description

P. WINAND.
OOMBUSTIUN ENGINE PLANT FOB SUBMARINB CRAFT.
APPLIUATION FILED 11011.19. 190e.
970,153. Patented sp1.13,191o.
WI77VESSES f [NVE/V701?" @www 41m/mgm PAUL WINAND, 0F COLOGNE, GERMANY.
COIVIBUSTION-ENGINE PLANT FOR SUBMARINE CRAFT.
Specification of Letters Patent. Patented Sept. 1.3, 1910.
Application filed November 9, 1906. Serial No. 342,757.
To atl whom rit may concern:
.Be it known that I, PAUL VINAND, englneer, a subject of 'the King ot' Belgium, resident at l Sudermannstrasse, Cologne-oxithe-Rhine, Germany, have invented certain new and useful Improvements in Combustion-Engine Ilants for' Submarine Craft; and I do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use. the same. i
In submarine boats it is important in or der to save room and weight to produce the power' required by means ot' an engine having the smallest possible dimensions.
inasmuch as, for operating combustion engines during submersion of the boat, the atniospheric air is replaced by oxygen or by substances rich in oxygen which are kept or preparel under a pressure higher than that of the atmosphere, there is advantage in using engines working on the two-stroke cycle or engines working on the tounstroke cycle in the cylinders of which greater' combustible 'charges are introduced than correspond to the amounts taken by the cylinders under atmospheric pressure. In this way a greater power than with the ordinary four-stroke cycle engine is obtained and turthermore the air pump, otherwise needed for introducing the required amount ot air, is dispensed with since the required substances are taken from their receivers under pressure. When working at the surface, and therefore with atmospheric air, some of the cylinders olf such an engine are used in carrying out my invention as air pumps for feeding to the other cylinders the amount of air required. and the use of special air pumps is thus dispensed with., In this case the power required is usually less than when working during submersion.
It is true that afour-stroke cycle engine might be operated without an air pump, the air being drawn in from thev atmosphere directly by the pistons o't' the exigirle; in such a case however the pressure duc to compression would be less and the economy o't tuel less than when using some ot' the cylinders as air pumps. Moreover the power obtained would be less since the cylinders used as pumps will take in air at every revolution while in vthe working cylinders the pistons will likewise draw in air in the usual fashion. As compared with one of the ordinary kind, an engine working as above described, that is with a larger' charge than that which would/till the cylinder under atmospheric pressure works 'with less economy ot' fuel, although with more power, if the pressure of the compression 1s the same in both. Now as the power needed for cruising speed is considerably less than that for the speed required in action, l. arrange some ot' the cylimlers to work in the ordinary way with a high rate ot' compression and with the best economy attainable, in order to use them at cruising speed as well when running during submersion as when running at the surface. T he other cylinders are arranged to work as above with a larger charge, lilling the cylinders at a higher pres- Isure1 and they are used for obtaining a higher rate ol' speed. when rainning din'- ing submersion both this set ol' cylinders and the other set may be working at the same time and thus the highest rate of power and of speed may be obtained it' desired. Yi'hen running at the surface i. c. with air, the cylinders` ol the iirst. set, or some ot' them, are used as air pumps for the other set, when a higher rate than the cruising speed is desired. The power thus'attainable is naturally less than that. attainable when working under exclusion ot' the atn'iospheric air. This however is an advantage as a high rate of speed is not practicable with a submarine cral't running at the surface.
In applying this method to engines Work ing on the two-stroke cycle, special air pumps may be needed when working with atmospheric air it it is desired to reduce as nun-.h as possible the ditfcrence between the power attainable at the surface and that attainable when during sulanersion, because for a given size of cylinder the amount of air needed is twice as large as for cylinders working on the four-stroke cycle. Never theless there will generally be an advantage in usingbesides the special air pumps some ot' the eylindci's as air pumps. It will also be of advantage to have as above one set of the cylinders operated with a pressure of charge before compression equal or nearly lequal to the atmospheric pressure, in order to use them with the best economy for the cruising speed and to haveY another set `of cylinders operated withla. pressure of charge higher'th'an the atmospheric to be used for obtaining higher speeds. When Working at the surface the iirst setr is supair pumps and by the special air pump.
The latter is thus assisted in its action by the first set of cylinders of the engine.
The accompanying drawing illustrates the application of my invention to a combustion engine of the four cycle type.
At full output and when Working with air, cylinder 2 serves as t-he working cylinder and cylinder 1 as the air vpump or charging pump. In'such case, the piston of cylinder l draws in air through the two-Way cock 3 and the valve et, and, on the return stroke, forces it through the valve 5 and two-way cock 6 to the cylinder 2, intov which it enters through the ports 7, when the piston of cylinder 2 approaches the outermost limit of its stroke. ln the meantime, the'piston of cylinder 2 has drawn in air through the two- Way cock 8 and valve 9, which air at this juncture fills the cylinder, under atmospheric pressure. To this air is added that whichis forced in through the ports 7 by the piston of cylinder 1, so that the cylinder 2 is iilled with air under a pressure higher than that of theatmosphere. rlhe combustible enters through the valved port l0 either simultaneously with or later than the air, and the exhaust gases escape from the cylinder 2 through the valve 11 and tWoway cock 12. At decreased output, the cylinder 1 may alone operate. This is effected by reversing the two-way cock 6 and admitting the combustible through the valved port 13. l The exhaust gases Will then escape A V,through the receptacle 14 and valve 15.
At full load, and when atmospheric air is excluded, both cylinders serve as working cylinders. At decreased load, either the one o-r the other cylinder may serve as the Working cylinder. In the latter case, for instance, cylinder 1 may serve as the Working cylinder While cylinder 2 runs entirely idle. In this event, oxygen is admitted through the pipe land receptacle 14; the cock 6 is so set that residual gases from the cylinder may enter the receptacle through t-he valve 5, and the cock 3 is so set that a. mixture of residual gases and oxygen may enter the cylinder from the receptacle through the valve y 4. A portion ofthe residual gases isv not returned to the cylinder, but escapes through the valve 15, which is so loaded that-the cylinder 1 after the suction stroke,
evo-,153
is filled with a mixture lhaving atmospheric pressure, Which takes the place of the air that would otherwise be drawn in. For increased output, 4the cylinder 2 is brought into operation, and its mode of operation is entirely analogous to that of cylinder l.
The loading of the valve is, of course, so
chosen, that the mixture of residual gases and oxygen, admitted through 8 and .9, at the end of the outstroke of the piston, fills the cylinder at the same pressure as that of the air when the cylinder Was Working With It will be understood that the specific construction of the individual parts per se shown in the drawing, is not claimed herein, but only the general combinations set forth in the claims, the speciiic construction of the individual parts being presented in the drawing merely as illustrative of many others that might be employed for the same 2. A combustion engine plant for submarine craft, comprising a'multiple combustion-engine, a pressure receptacle for storing under pressure an oxygenating ele- 'ment, connections for supplying the explosive charge to one of the cylinders at a pressure of the charge before compression equal or nearly equal to that of the atmosphere and for cutting off the supply to the other cylinder so that the engine may operate at reduced -power (as, for instance, at cruising speed), and connections for supplyin g air to the second cylinder, when a greater amount of poWeris desired and pumping air therefrom into the explosive charge of the first cylinder at a pressure of the charge before compression greater than that of the atmosphere; substantially as described.
3. A combustion engine plant for submarine craft, comprising a multiple cylinder combustion engine, connections for supplying fuel to the several cylinders thereof, connections for supplying atmospheric air to said cylinders, connections for supplying under-pressure an artificial oxygenating .elementth-ereto, a connection between individual cylinders, and cut-offs for all of said4 connections; whereby'- the several cylinders- ,may all operate conjointlyl asexpolosion cylinders either with air or with the arti- 'In testimony whereof I have axed my ciaI oxygenating element as the oxidizer signature, in presence of two witnesses. for the fuel, and whereby, when operating with air any individual eylinder may serve I PAUL' WINAND' as an air pump to convey air under com- Witnesses: y pression into the explosion chamber of any BESSIE F. DUNLAP,
other cylinder; substantially as described. LOUIS VANDORN.
US34275706A 1906-11-09 1906-11-09 Combustion-engine plant for submarine craft. Expired - Lifetime US970153A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3365014A (en) * 1965-08-11 1968-01-23 Cummins Engine Co Inc Combination vehicle engine and self-powered air compressor
US3507119A (en) * 1968-10-24 1970-04-21 Alfred Karl Kayser Oscillating rotor jet engine
US3894520A (en) * 1974-03-13 1975-07-15 Thermo Electron Corp Charge forming device with fuel vaporization
US4248198A (en) * 1977-12-01 1981-02-03 Motor Und Turbinen-Union Freidrichshafen Gmbh Multi-cylinder diesel engine
US4864979A (en) * 1987-05-25 1989-09-12 Karl Eickmann Combustion engine
US20140123958A1 (en) * 2012-11-02 2014-05-08 GM Global Technology Operations LLC Piston compound internal combustion engine with expander deactivation

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3365014A (en) * 1965-08-11 1968-01-23 Cummins Engine Co Inc Combination vehicle engine and self-powered air compressor
US3507119A (en) * 1968-10-24 1970-04-21 Alfred Karl Kayser Oscillating rotor jet engine
US3894520A (en) * 1974-03-13 1975-07-15 Thermo Electron Corp Charge forming device with fuel vaporization
US4248198A (en) * 1977-12-01 1981-02-03 Motor Und Turbinen-Union Freidrichshafen Gmbh Multi-cylinder diesel engine
US4864979A (en) * 1987-05-25 1989-09-12 Karl Eickmann Combustion engine
US20140123958A1 (en) * 2012-11-02 2014-05-08 GM Global Technology Operations LLC Piston compound internal combustion engine with expander deactivation
US9080508B2 (en) * 2012-11-02 2015-07-14 GM Global Technology Operations LLC Piston compound internal combustion engine with expander deactivation

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