US1291032A - Explosion-engine. - Google Patents

Explosion-engine. Download PDF

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US1291032A
US1291032A US16498017A US16498017A US1291032A US 1291032 A US1291032 A US 1291032A US 16498017 A US16498017 A US 16498017A US 16498017 A US16498017 A US 16498017A US 1291032 A US1291032 A US 1291032A
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cylinder
piston
pistons
engine
explosion
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US16498017A
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Isidor Lesem
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

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  • vcrossfhead 16 Secured to the piston .rod 12V outside of the cylinder 1 is a vcrossfhead 16.v "Fast to the cross head V16 at opposite ends thereof are rods 17 extending outside ofthe cylinder 1 and entering the cylinder 4 through free openings in the reduced end 5 thereof so that said end of the cylinder 4 is openv to the-atmosphere through said free openings.
  • the rods 17 are ultimately secured to a ,piston 18 within' the cylinder 4.
  • the piston 18 is similar and reciprocable in opposition to the piston 10, but is in substantially air tight relation to the inner walls of the cylinder 4.
  • the cylinder 14 is provided with an inlet-pipe 19 for fuel with a self closing valve 20 opening toward the cylinder on the side of the piston 15 toward the cylinder 1.
  • An explosion engine comprising a relat1vely large cylinder with lboth ends open to the atmosphere, a smaller power cylinder, a pa1r of plstons in each cylinder with the pistons of each pair movable simultaneously in opposite directions and each piston of one pair connected with the corresponding pistons of the other pair, the power cylinder having means for supplying it with 180 explosive charges and igniting said charges, whereby the pistons in the larger cylinder produce a vacuum between them when they are moved one away from the other to cause the bodily propulsion of the engine and the return of all the pistons to initial position after being displaced therefrom on the power strokes of the pistons in the power cylinder.v

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Description

l. LESEM. ExPLosloN ENGINE.
APPLICATION FILEDAPRJT. 1.91.7.
Patented Jan. 14, 1919.
[s'a'dorA Lede/WNVENTR,
ATTO R N EY UNITED sTATEs PATENT OFFICE..
ISIDOR LESEM, WICHITA, KANSAS.
EXPLOSION-ENGINE.
To all whom 'it may concern:
Be it known that I, IsIDoR LEsEM, a citizen of the United States, residing at Wichita, in the county lof Sedgwick and State of Kansas, have invented a new and useful Explosion-Engine, of which the following is a specification.
This invention has reference to explosion engines and itsY object is to provide a selfstarting engine having no heavy inertia parts, thus adapting the engine particularly .and the oppositely reciprocating pistons are in turn actuated by other reciprocating pisa tons in an explosion engine and driven byf'v the expansive force of explosions obtained`-- from explosive mixtures of air and hydrocarbon. The impulse given to one of the second ,set of pistons by the effect of the ignited explosive mixtureserves through a suitable pump structure to compress the aseous fuel into a storage tank from which 1t is -fed to the explosion chamber of the engine to be there ignited, while the exhaust gases of combustion are so directed as to impact against the surrounding atmosphere in a direction `to aid in the propulsion of the vehicle. Furthermore, the engine may be so mounted that it may be pointed in different directions tolcause the propulsion of the vehicle in correspondingly different directions.
The invention will be best understood from a consideration of the following detailed description, taken in connection with the accompanying drawings forming part of this speci cation. with the further under.- standing that while the drawings show a ractical form of the invention. the latter 1s not confined to anystrictconformity with the showing of the drawings, but may be Specieation of Letters Patent.
Application mea April 27, 1917.A serial No. 164,930.
Patented J an. 14,
changed and modified so long as suchchanges and modifications come Within the scope of the appended claims.
In` the drawings Figure 1 is a longitudinal diametric l section of an engine embodying the invention, but omitting parts common tolexplosion engines, and, therefore, needing no illustration.
Fig. 2 is a view of the explosion cylinder portion of Fig. 1 with the section taken at right angles to that of Fig. 1.
Fig. 3 is a more or less schematic view of a mounting for the engine upon the vehicle.
Referring to the drawings there is shown a cylinder 1 in one end of which thereis inclosed a concentrically disposed cylinder 2 of considerably smaller internal diameter than the cylinder 1 and terminating .at a head 3 between the opposite ends of the cylinder 1. Fast to that end of the cylinder 1 remote from the cylinder 2 is another cylinder 4 joined to the cylinder 1 `by a \cylinder 1.
That end ofthe cylinder 4 remotefrom the cylinder v1 is'somewhatcontracted, as indicated atti. to a mouth opening 71 at the extreme end of the cylinder 4 remote from th'e cylinder 1.
Within the internally larger end f of the cylinder 1 is a piston 8 which may follow explosion engine prati'ce, and this piston is fast to one end of a piston rod -9 extend- `ing into the cylinder 4 and there carrying another piston 10. the two pistons fitting the respective cylinders in a substantially airtight manner. but both free to reciprocate l together in the respective cylinders.
Within the small cylinder 2 is anothery piston 11 on a piston rod 12 carried through what may be termed the outer end ,of the cylinderl 2 and entering, through a Astniling box 13'int'o another cylinder 11 spa-"ed from from the cylinder 4. Within the cylinder loov 14 the piston rod12 carries a piston 1'5 l recipronlble with the piston rod within the cylinderA 14, but engaging the inner walls of the cylinder in substantially air tight relation thereto.
Secured to the piston .rod 12V outside of the cylinder 1 is a vcrossfhead 16.v "Fast to the cross head V16 at opposite ends thereof are rods 17 extending outside ofthe cylinder 1 and entering the cylinder 4 through free openings in the reduced end 5 thereof so that said end of the cylinder 4 is openv to the-atmosphere through said free openings. The rods 17 are ultimately secured to a ,piston 18 within' the cylinder 4. The piston 18 is similar and reciprocable in opposition to the piston 10, but is in substantially air tight relation to the inner walls of the cylinder 4. The cylinder 14 is provided with an inlet-pipe 19 for fuel with a self closing valve 20 opening toward the cylinder on the side of the piston 15 toward the cylinder 1.
Near the end of the cylinder 14 adjacent to the cylinder 1 is an outlet port 21 communicating with a valve casing'22 containing a valve 23. The valve caslng 22rk opens into one end of a storage chamber 24, the other end of which is connected by a valve casing 25 to an inlet port 26 opening into the cylinder 1 adjacent tothe head 3. The casing 22 contains a valve 27 opening toward the port 26.
The valve 23 is provided with a valve stem 28 connected to one end of a rock leverA 29, the other end of which is connected to a valve stem 30 carrying the valve 27.
The cylinder 1 .carries a spark plug 31 in vposition to-ignite an explosive charge between the piston'y 8 and the piston 11 and head 3.
. The cylinder 1 containing the piston 8 has exhaust ducts 32 leading therefrom and the cylinder 2 ata point coincident with the end of the power stroke of the piston 11 has exhaust ducts 33. These exhaust ducts unite adjacent to the reduced portion 5 of the cylinder 4 and terminate in bell mouths 34 opening in the same direction as the mouth of the cylinder 4. The ducts 33l are located' at any desired point in the length of the cylinder 2 that the stroke of thepiston'll mayA demand. y
' When the engine is first prepared for running-a fuel mixture is pumped into the chamber 24 through a suitable nipple 35,'
this being 'accomplished by means of a hand pump or otherwise, whereby several charges are compressed into the chamber 24which therefore constitutes a fuelreservoir.
The pressure of the stored fuel causes the v opening of the valve 27 and the-charging of the explosin chamber within the cylinder 1 between the piston 8 andthe head 3.
' When equilibrium yis established the valve 27 automatically closes. y
Now. on passing a spark through thespark plug, 31, the explosion mixture in the explosion chamber is lgnited, and, assuming that the partsV have been in the position shown in Fig. 1, the expansion of the ignitedl vmixture is exerted suddenly and with great force against the piston 8, reacting upon the head 3, of but little smaller area than the piston 8,'with the result that the piston 8 is driven `toward the cylinder 4, and since the piston 10 is ixed to the piston-8 through the piston rod k9, it is moved with great rapidity toward the mouth 7.
At the same time the explosive force is -cylinder 14.
`As soon as the pistons 8 and 11 reach the ends of their power strokes,o the exhaust ducts 32 and 33 are opened by being over ridden by the pistons and the gases of combustion pass from the cylinders 1 and 2 into the ducts 32 and 33: and are discharged through the mouths 34 against the surrounding a1r,"thus imparting a propelling movement tothe engine and structure carryin 1t in the same direction that a propelling'e ort is caused by the power stroke of the piston 10.
The separation of the two 4pistons 10 and 18 because of their opposite travel establishes a vacuum in the cylinder `4 between these two pistons. During the power stroke of the piston 11 a fuel charge has been drawn into the cylinder 14.
Now, when the exhaust takes place the pressure due to the explosion is greatly reduced, being near to, if not actually below atmospheric pressure, and then the atmospheric pressure immediately and forcefully returns the two pistons 10 and 18l to the first or intermediate position, as soon as the force of the explosion is exhausted. When the two pistons 8 and 11 are returned to their first position, there is again formed a small explosion chamber and the piston 15 is forced toward its first position,'thereby closin the valve 20 and opening the valve 22 an forcing ya charge into the chamber or reservoir 24. This maintains lthe ressure within the reservoir 24, while permitting a fresh charge to enter the exploson chamber,
whereupon a spark. passing the terminals of their presence would only serve to confuse an understanding of the salient features ot the invention.
Since the pistons 10 and 18 on their separation produce a vacuum, and since it is diiicult to wholly prevent leakage about the pistons 10 and 18, a check valve 41 is provided in the cylinder 4f'so that in case air should leak into the space between the pistons 10 and 18 on their separation, it will be forced out through the check valve 14 when the istons again move into their position of clise approach.
In Fig. 3 there is indicated a. small portion 36 of an air ship or other vehicle. On the vehicle 36 there are provided bearings 37 for a swivel stud 38 carrying a yoke 39 in line with the swivel spindle 38.
Mounted at the free ends of the legs of the yoke 39 is a cylinder 4 which is provided with trunnions 40 for the purpose. By suitable supports the engine may be turned and tilted at various angles from a straight line of propulsion, so that the vehicle may be lifted or depressed or driven straight ahead, as may be desired.
By the provision of a suitable number of.
engines distributed about the vehicle it is possible to direct the propelling impulses wherever desired to drive the vehicle straighty ahead, or to turn the vehicle in any desired direction.
Reference is herein made to another application Serial No. 112,793, led by me on August 2, 1916, for an explosion engine, in which application features are described which are similar to certain features herein shown'and described.
What is claimed is 1. An explosion engine comprising a cylinder inclosing an explosion chamber and provided With oppositely movable power pistons, a cylinder alined with-thefirstnamed cylinder and open at both ends to the atmosphere, oppositely movable pistons within the second .cylinder and connected to respective pistons of the first-named cylinder for simultaneous opposite movements, and the production of a vacuunr between them when movin apart, and means for directing explosive c arges into the eX- plosion Ychamber of the first-named cylinder and there igniting them.
2. An explosion engine comprising an explosion cylinder with pistons of dierent Vareas therein and movable simultaneously in opposite directions, another cylinder of larger area carried by the rst-named .cyl-
inder and open to the atmosphere at both ends, pistons within the second-named ycy-linder simultaneously movable in opposite directions with ,one piston connected to the larger piston in the first cylinder and the other piston' connected to the Asmaller piston in the first cylinder, means for directing explosive charges to the space between thc two pistons in the rst-named cylinder, and
means for there igniting the charges.
directions with one piston connected to the.
larger piston in the first cylinder and the other piston connected to the smaller piston in the first cylinder, means for directing explosive charges to the space between the Atwo pistons in the first-named cylinder, and
means for there igniting the charges, the engine also being provided with a pump for directing explosive charges to the explosion chamber of the first-named piston and connected to the smaller one of the pistons in the first-named cylinder.
4. An explosion engine provided with a power piston and cylinder inclosing it, another cylinder in line with the first-named cylinder and open to the atmosphere at both ends, a piston within the second cylinder connected to the first-named piston for actuation thereby, and means for establishing avacuum on the side of the second-named plston remote from the open end of the cyl- `inder containing it, said means comprising a piston in the second-named cylinder, and a piston in the 'first-named cylinder connected therewith for the actuation of the second piston in the second cylinder by the eiiect of an explosion in the first-named cylinder acting on the second-named piston therein, with the movement of the secondnamed piston in the second-named cylinder opposlte to the movement of the first-named piston in the second-named cylinder.
5.. An explosion engine comprising two cylinders each with a pair of pistons there- 1n, one of the cylinders having one of its pistons of smaller diameter than the other piston, with the pistons of each' cylinder movable simultaneously in opposite directions, and each piston in one cylinder connected to 'a corresponding piston inl the other cylinder, o ne cylinder havin means for the introduction and ignition o an explos1ve mlxture between its pistons and the other cylinder being open to the atmosphere at both ends.
u 6. An explosion engine comprising a relat1vely large cylinder with lboth ends open to the atmosphere, a smaller power cylinder, a pa1r of plstons in each cylinder with the pistons of each pair movable simultaneously in opposite directions and each piston of one pair connected with the corresponding pistons of the other pair, the power cylinder having means for supplying it with 180 explosive charges and igniting said charges, whereby the pistons in the larger cylinder produce a vacuum between them when they are moved one away from the other to cause the bodily propulsion of the engine and the return of all the pistons to initial position after being displaced therefrom on the power strokes of the pistons in the power cylinder.v
7. An explosion engine comprising a lar e' .a pump for storing the fuel in the storage means having connections with the smaller power piston foractuation thereby.
8. An explosion engine comprising a relatively large cylinder with the ends open, a smaller power cylinder in line therewith and connected thereto, two oppositely movable pistons in the large cylinder, two oppositely movable pistons in the power cylinder with one of the pistons of greater area than the other, a piston rod connecting the larger piston in the power cylinder with that piston lin the first-named cylinder t0- ward the outer end thereof, a piston rod connected to the smaller power piston and extending beyond the end of the power cylinder remote from the first-named cylinder, connections between the piston rod of the smaller piston and the second piston in the Witnesses:
larger cylinder, a pump with a piston therein in line with the power cylinder with the piston of the pump connected to the piston rod of the smaller power piston, a storage reservoir between the pump and the power cylinder with the storage reservoir connected to the pump and also connected to the power cylinder to deliver explosive charges thereto between the two pistons in the power cylinder, and valves and `actuating means therefor to cause vthe pump to de-- liver' charges of fuel to the reservoir and the reservoir to deliver charges to the power cylinder at each stroke of the engine.
9. An explosion engine for air ships and other 'like vehicles, comprising'a cylinder with reciprocatory pistons therein and with the cylinder having the ends open to the atmosphere, an explosion engine cylinder and pistons carried by the'rst-named cylinder in line therewith, with the pistons of the second cylinder separately connected to respective pistons of the first-named cylinder for the reciprocation of/the pistons simultaneously in opposite directions, and a mounting for the engine connected to the irst-named cylinder. with said mounting movable about different axes for presenting the open end of the first-named cylindervin directions with respect to an air ship on which the engine is mounted for causing impulses delivered to the engine to propel the air ship in directions corresponding to tle angular relation of the engine to the air s 1p.
In testimony, that I claim the foregoing as my own, I have hereto ailixed my signature in the presence of two witnesses.
ISIDOR LESEM.
E. S. WONELL, J. T. MCCALL.
US16498017A 1917-04-27 1917-04-27 Explosion-engine. Expired - Lifetime US1291032A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2496710A (en) * 1942-03-09 1950-02-07 Daniel And Florence Guggenheim Fuel controlling apparatus for longitudinally movable combustion chambers
US2499401A (en) * 1946-06-28 1950-03-07 James H Madden Jet-propelled aircraft with tiltable jet units
US2526714A (en) * 1946-05-31 1950-10-24 Fred M Varney Manually supported and selfpropelled pulling device
US2536597A (en) * 1946-09-05 1951-01-02 Daniel And Florence Guggenheim Recoil-operated feeding apparatus for a combustion chamber used in aerial propulsion
US2875576A (en) * 1959-03-03 Endres

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2875576A (en) * 1959-03-03 Endres
US2496710A (en) * 1942-03-09 1950-02-07 Daniel And Florence Guggenheim Fuel controlling apparatus for longitudinally movable combustion chambers
US2526714A (en) * 1946-05-31 1950-10-24 Fred M Varney Manually supported and selfpropelled pulling device
US2499401A (en) * 1946-06-28 1950-03-07 James H Madden Jet-propelled aircraft with tiltable jet units
US2536597A (en) * 1946-09-05 1951-01-02 Daniel And Florence Guggenheim Recoil-operated feeding apparatus for a combustion chamber used in aerial propulsion

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