US308572A - Beaumont paekee - Google Patents

Beaumont paekee Download PDF

Info

Publication number
US308572A
US308572A US308572DA US308572A US 308572 A US308572 A US 308572A US 308572D A US308572D A US 308572DA US 308572 A US308572 A US 308572A
Authority
US
United States
Prior art keywords
air
cylinder
power
chamber
explosion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
Publication date
Application granted granted Critical
Publication of US308572A publication Critical patent/US308572A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression

Definitions

  • GAS ENGINE No. 308,572. Patented Nov. 25. 1.884.
  • FIG. 1 is a longitudinal sectional view, on a horizontal plane, of my improved gas-engine.
  • Fig. 2 is a vertical transverse section through the dotted line 00 a: in Fig. 1.
  • Fig. 3 is a detail View of the valves and valve mech anism appertaining to the air-cylinder.
  • Fig. 4 is a detail View of the inlet-ports and valve appertaining to the explosion-chamber; and
  • Fig. 5 is a detail View of the exhaust-port and its valve, also appertaining to the explosionchamber.
  • This invention relates to gas-engines, and has for its object to provide an engine which shall be compact, simple, and durable in its construction, and yet be of great power and general efficiency.
  • My improved gas-engine comprises a power-cylinder, A, an explosion-chamber, B, and an air-cylinder, D.
  • the partsA and B which are subjected to great heat, are surrounded by the usual water-jackets, O.
  • the power-cylinder has a piston, T, with a piston-rod, R
  • the air-cylinder has a piston, U, with a pistonrod, S, the outer ends of the two pis ton-rods Rand S being connected rigidly by a cross-head, Q, so that they and their respective pistons will move in unison with each other, and with the same length of stroke.
  • the crosshead Q is connected by a pitman, P, to the crank O of the drive-shaft N, which has a fly-wheel or balance-wheel, V, and a bevel-pinion, W, the function of which will be hereinafter described.
  • the rear end of the power-cylinder A opens'up into the explosionchamber or combustion-chamber B, to which the explosive charge is fed through the port or inlet I, while the inert products of combustion are exhausted through the port or outlet J.
  • the air-cylinder D communicates with the rear end of the power-cylinder A through a passage, E, which is provided with a valve, F, Fig.
  • the gas and air which are to form the explosive charge are fed to the explosion-chamber B through the inlet I.
  • the inlet has a valve, K, adapted to seat itself to close communication with chamber 13.
  • the inlet I has a gas-port, I, and an air-port, H, so that the gas and air will be mixed as they enter the inlet-chamber I, and before they pass, when valve K is open, therefrom into the explosion-chamber B.
  • the stem is of the inlet-Valve K is actuated by a spring in such a manner that its normal condition will be closed; but it may be opened by pressure on the projecting outer end of the spring-actuated valve-stem, in like manner as the springactuated stem Z of the exhaust-valve L, (shown in detail in Fig. 5,) the said inlet and exhaust valves K and L being respectively actuated by bell-cranks or elbow-levers G and D, in the manner hereinafter to be described.
  • the air-port H is provided with a valve, G, to prevent the escape of air after it has entered the inlet-chamber or mixing-chamber I.
  • a shaft, Y, journaled in suitable bearings, has,
  • bevel-wheel, X which meshes with the pinion V on the drive-shaft or main shaft N.
  • the relative size of the iutermeshing wheels W and X is such that shaft Y will make one complete revolution to every two revolutions of shaft N 5 or, in other words, shaft Ywill make one complete revolution for every four strokes of the pistons T and U.
  • a cam, Z for actuating the bell-crank M, by which valve H is operated
  • another disk or cam A for actuating the igniting device m, which maybe of any approved construction
  • This outward stroke of piston T is what I call the power-stroke, and it imparts a one-half revolution to the drive-shaft N
  • the outward stroke of piston U valve H in the air-inlet G is open, and air-cylinder D takes in a charge of air while piston T is completing the power-stroke.
  • the charge of air in the air-cylinder is forced through the passage E into the power-cylinder, as has already been described, sweeping out the inert pro ducts of combustion, while the power-piston is moving back to the starting-point near the explosion'chamber. This completes one revolution of shaft N and one half-revolution of shaft Y.
  • an air duct or passage connecting the power-cylinder and the air-forcing apparatus having its inlet into the former bent or deflected parallel to the axis of the power-cylinder, substantially as and for the purpose herein shown and described.
  • the head the main shaft or crank-shaft, the coun- IO ter-shaft having cam-wheels or eccentrics, and

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Description

2 Sheets- Sheet- 1.
(No Model.)
B. PARKER.
GAS ENGINE.
' Patented Nov. 25,1884. l 0 oh l VENTORi WITNESSES: Z$d.f'
2 .ATTORNEYS;
Rs. Plwlvmhugnpller. Walh'mghn. D. c.
(No Model.)
2 Sheets-Sheet 2. B. PARKER.
GAS ENGINE. No. 308,572. Patented Nov. 25. 1.884.
WITNESSES:
A'TORNEYS.
@Umrrno STATES PATENT Fries.
BEAUMONT PARKER, OF HIGHLAND, KANSAS, ASSIGN OR TO LElVIS C. PARKER, OF YONKERS, NEIV YORK.
GAS-ENGINE.
SPECIFICATION forming part of Letters Patent No. 308,572, dated November 25, 1884,
Application filed May 14, 1884. (N model.)
To all whom it may concern.-
Be it known that I, BEAUMONT PARKER, of Highland, in the county of Doniphan and State of Kansas, have invented certain new and useful Improvements in Gas-Engines; and I do hereby declare that the following is a full, clear, and exact description of theinvention, which will enable others skilled in the art to which it appertains to make and use the same, reference being had to the accompanying drawings, which form a part of this specification, and in which Figure 1 is a longitudinal sectional view, on a horizontal plane, of my improved gas-engine. Fig. 2 is a vertical transverse section through the dotted line 00 a: in Fig. 1. Fig. 3 is a detail View of the valves and valve mech anism appertaining to the air-cylinder. Fig. 4 is a detail View of the inlet-ports and valve appertaining to the explosion-chamber; and Fig. 5 is a detail View of the exhaust-port and its valve, also appertaining to the explosionchamber.
Similar letters of reference indicate corresponding parts in all the figures.
This invention relates to gas-engines, and has for its object to provide an engine which shall be compact, simple, and durable in its construction, and yet be of great power and general efficiency.
To this end my improvement consists in the construction and combination of parts, which will be hereinafter more fully described and claimed.
My improved gas-engine comprises a power-cylinder, A, an explosion-chamber, B, and an air-cylinder, D. The partsA and B, which are subjected to great heat, are surrounded by the usual water-jackets, O. The power-cylinder has a piston, T, with a piston-rod, R, and the air-cylinder has a piston, U, with a pistonrod, S, the outer ends of the two pis ton-rods Rand S being connected rigidly by a cross-head, Q, so that they and their respective pistons will move in unison with each other, and with the same length of stroke. The crosshead Q is connected by a pitman, P, to the crank O of the drive-shaft N, which has a fly-wheel or balance-wheel, V, and a bevel-pinion, W, the function of which will be hereinafter described. The rear end of the power-cylinder A opens'up into the explosionchamber or combustion-chamber B, to which the explosive charge is fed through the port or inlet I, while the inert products of combustion are exhausted through the port or outlet J. The air-cylinder D communicates with the rear end of the power-cylinder A through a passage, E, which is provided with a valve, F, Fig. 3, which will open 011 pressure against it in the direction of the powercylinder, but will be closed or seated against its seat by pressure in the opposite direction or from the power-cylinder through the passageE in the direction of the air-cylinder. The mouth of the passage E, where it opens up into the power-cylinder at its end, is flush with the side of the same, so that a jet of air forced through the passage E from the air-cylinder D in the direction of the arrow will be injected into the power-cylinder A, near one side of the same, up against the piston T,where the current of injected air will be deflected back along the other side of the cylinder and into'l'the explosion-chamber, as indicated by arrows, thus effectually clearing the powercylinder of the inert products of combustion resulting from the explosion of the charge. The gas and air which are to form the explosive charge are fed to the explosion-chamber B through the inlet I. (Shown in detail in Fig. 4, by reference to which it will be seen that the inlet has a valve, K, adapted to seat itself to close communication with chamber 13.) The inlet I has a gas-port, I, and an air-port, H, so that the gas and air will be mixed as they enter the inlet-chamber I, and before they pass, when valve K is open, therefrom into the explosion-chamber B. The stem is of the inlet-Valve K is actuated by a spring in such a manner that its normal condition will be closed; but it may be opened by pressure on the projecting outer end of the spring-actuated valve-stem, in like manner as the springactuated stem Z of the exhaust-valve L, (shown in detail in Fig. 5,) the said inlet and exhaust valves K and L being respectively actuated by bell-cranks or elbow-levers G and D, in the manner hereinafter to be described. The air-port H is provided with a valve, G, to prevent the escape of air after it has entered the inlet-chamber or mixing-chamber I. The
A shaft, Y, journaled in suitable bearings, has,
at one enda bevel-wheel, X, which meshes with the pinion V on the drive-shaft or main shaft N. The relative size of the iutermeshing wheels W and X is such that shaft Y will make one complete revolution to every two revolutions of shaft N 5 or, in other words, shaft Ywill make one complete revolution for every four strokes of the pistons T and U. Upon sh aft Y are suitably fastened a cam, Z, for actuating the bell-crank M, by which valve H is operated, another disk or cam A, for actuating the igniting device m, which maybe of any approved construction, and a third double cam, 13, the ofiice of which is to actuate the alternately-operating valves K and L through the medium of the bell-cranks G and D, which have already been described, and have their fulcrums in an arm, E, suitably fastened to the frame of the machine. It will thus be seen that the several valves are actuated once for every four strokes of the two connected pistons.
Having in the foregoing described the con- 'struction of my improved gas-engine, I shall now proceed to describe its operation, which is as follows: Assume both pistons to be at the end of the instroke, or in position nearest to the explosion chamber; now ignite the charge with which the explosion-chamber has been filled through the inlet or mixing-chamber I, and both pistons will move outward simultaneously--the one T impelled by the gases which result from the explosion, and the other, U, because its rod S is connected to piston-rod R by the cross-head Q. This outward stroke of piston T is what I call the power-stroke, and it imparts a one-half revolution to the drive-shaft N During the outward stroke of piston U valve H in the air-inlet G is open, and air-cylinder D takes in a charge of air while piston T is completing the power-stroke. On the next or returnstroke of the two pistons the charge of air in the air-cylinder is forced through the passage E into the power-cylinder, as has already been described, sweeping out the inert pro ducts of combustion, while the power-piston is moving back to the starting-point near the explosion'chamber. This completes one revolution of shaft N and one half-revolution of shaft Y. On the return-stroke of the powerpiston a fresh charge of gas and air has been fed into the explosion-chamber through its inlet I, the valve K of which is open at this stage, while the products of combustion have been exhausted through port J, the valve L of which was open, but is closed by its spring at the same time that inlet-valve K is opened by its cam B and lever C. At the next explosion we have the third stroke of piston T, which is the second power-stroke; but as the piston U in air-cylinder D moves outward with this stroke, Valves F and Hare closed, and there is a vacuum created in the air-cylinder. During the next or fourth movement of the pistons in the direction of the explosion-chamber. the charge of gas and air, which has been fed into the explosion-chamber for the next explosion, will be compressed by the power-piston, which is impelled on its returnstroke by the vacuum in the air-cylinder and piston U, which actuates the crank-shaft N through pitman P and cross-head Q, and thus imparts sufficient momentum to the fly-wheel to effectually compress the fresh charge in the explosion-chamber. This compressure of the explosive charge is thus brought about by the direct action of atmospheric pressure against the air-piston in conjunction with the momentum of the fly-wheel. This brings us to the completion of the fourth stroke of the pistons, when one revolution of: shaft Y has been completed, and the several operating parts and their actuating mechanism have resumed the position at which they were at the startingpoint.
Havingthus described my invention, I claim and desire to secure by Letters Patent of the United States- 1. In a gas-engine, the combination of the power-cylinder, the air-cylinder arranged parallel to the same, the two pistons adapted to move in unison with each other, the explosionchamber, the feed and exhaust valves and the mechanism for operating the same, and the passage leading from the air-cylinder to the open end of the powercylinder and deflected to adapt it to force the current of air passing through it parallel to the axis of the power-cylinder and against the piston of the same, substantially as and for the purpose set forth.
2. In a gas-engine provided with an airforcing apparatus for cleaning out the inert products of combustion from the power-cylinder and combustion-chamber, an air duct or passage connecting the power-cylinder and the air-forcing apparatus, having its inlet into the former bent or deflected parallel to the axis of the power-cylinder, substantially as and for the purpose herein shown and described.
3. In a gas-engine, the combination, with a power-cylinder and an air-cylinder located parallel to each other, of a cross-head connecting the piston-rods of both cylinders, a crank-shaft connected by a pitman with the said cross-head, a longitudinal shaft operated by the said crank-shaft or main shaft and equipped with a series of cam-wheels or ecvalves and to receive motion from the camvalves, all constructed, combined, and arwheels or eccentrics, substantially as herein ranged to operate substantially in the manner described, for thepurpose shown and setforth. and for the purpose herein shown and de- 4. In a gas-engine, the combination of the 1 scribed. 15 5 power-cylinder, explosion-chamber, air-cylin- In testimony that I claim the foregoing as der, passage connecting it with the power-cylmy own I have hereunto affixed my signature inder, inlet and exhaust ports, valves, the pisin presence of two witnesses.
? tons connected rigidly to a common cross- BEAUMONT PARKER.
head, the main shaft or crank-shaft, the coun- IO ter-shaft having cam-wheels or eccentrics, and
the levers actuated thereby and operating the XVitnesses:
J. CARPENTER, J. R. STEARNS.
US308572D Beaumont paekee Expired - Lifetime US308572A (en)

Publications (1)

Publication Number Publication Date
US308572A true US308572A (en) 1884-11-25

Family

ID=2377738

Family Applications (1)

Application Number Title Priority Date Filing Date
US308572D Expired - Lifetime US308572A (en) Beaumont paekee

Country Status (1)

Country Link
US (1) US308572A (en)

Similar Documents

Publication Publication Date Title
US308572A (en) Beaumont paekee
US708236A (en) Gas-engine.
US731995A (en) Internal-combustion engine.
US791071A (en) Rotary explosive-engine.
US581385A (en) Gas or vapor engine
US588672A (en) wordsworth
US359920A (en) Gas-engine
US558943A (en) gardner
US754929A (en) Internal-combustion engine for cycles.
US335971A (en) Gas-engine
US622047A (en) l holden
US1439958A (en) Internal-combustion engine
US1335325A (en) Assigetob
US702430A (en) Internal-combustion engine.
US724239A (en) Compounding gas-engine.
US367184A (en) campbell
US704060A (en) Internal-combustion engine.
US756458A (en) Gas-engine.
US636478A (en) Gas-engine.
US412883A (en) Griffin
US596352A (en) Compound gas-engine
US767549A (en) Gas-engine.
US691083A (en) Compound explosive-engine.
US644295A (en) Vapor or gas engine.
US1219982A (en) Internal-combustion engine.