US1531066A - Engine construction - Google Patents

Engine construction Download PDF

Info

Publication number
US1531066A
US1531066A US593898A US59389822A US1531066A US 1531066 A US1531066 A US 1531066A US 593898 A US593898 A US 593898A US 59389822 A US59389822 A US 59389822A US 1531066 A US1531066 A US 1531066A
Authority
US
United States
Prior art keywords
piston
cylinder
ports
engine
combustion
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
US593898A
Inventor
Brice John Francis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US593898A priority Critical patent/US1531066A/en
Application granted granted Critical
Publication of US1531066A publication Critical patent/US1531066A/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
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2720/00Engines with liquid fuel
    • F02B2720/13Two stroke engines with ignition device
    • F02B2720/136Scavenging or charging channels or openings

Definitions

  • My invention relates to an engine construction and aims to provide certain new and useful improvements in connection with a device of this character, and more particularly in connection with an internal combustion engine.
  • the combustible charge is admitted into the working chamber by ports at one side of the cylinder and the products of combustion are allowed to escape through ports on the opposite side of the cylinder, a baffle plate being provided upon the top of the piston to prevent as far as possible the intermixture of the fresh gas with the spent gas.
  • a baffle plate being provided upon the top of the piston to prevent as far as possible the intermixture of the fresh gas with the spent gas.
  • Figure 1 is a sectional side view of an engine of the type stated and showing the parts in the position which they assume at the end of the firing stroke.
  • Figure 2 is a view showing the disposition of the parts at the beginning of the firing stroke.
  • Figures 3 and 4L are transverse sectional views taken along the lines 3-3 and 4 4: of Figure 1.
  • the reference numeral 11 indicates the cylinder mounting an igniting device in the nature of a spark plug 12, and being preferably provided with a jacket 13 for cooling purposes.
  • a crank case 14 within which a crank shaft 15 is rotatably mounted, the latter having one of the ends of the connecting rod 16 attached to its body, the opposite end of said connecting ro'd being attached to the piston 17 which is slidably mounted within the cylinder.
  • I-Iowever it will be seen that contrary to conventional construction I provide a bypass through which the compressed fuel charge is introduced into the cylinder by mounting a series of vanes 20 extending radially inward within the enlarged lower end of the cylinder, and thus spaces 21 are provided between the piston yin its lowermost position and the inner wall of the chamber, and it is through these spaces that CTA the compressed fuel charge flows, the same being introduced at a series of different points in the circumference of the cylinder, as has been shown in Figure 1.
  • vanes 2O serve another purpose in that they confine the body of the piston 17 and, consequently, the rings 22 carried thereby are prevented from springing clear of the grooves with which they are associated when the piston is in its lowermost position.
  • the lower end of the piston 17 is in the nature of a skirt 25, reduced in diameter to furnish a clearance which is of sufficient width so that when the piston is in its outermost or upper position shown, in Figure 2 it will permit of air iowing through the exhaust ports 23 around this lower end of the piston and so into the spaces 21, where it will form a cushion, separating the fuel charge in the base from the spent gases of the exhaust when the return of the piston to its lowermost position unc-overs the upper ends of the spaces 21, as in Figure 1.
  • An engine construction including in combination a cylinder formed with exhaust ports and intake passages, the latter being arranged below the former, a piston movable within said cylinder and/'adapted to cover said openings, a reduced skirt porti-on adjacent the lower end of said piston whereby to permit communication between sa-id openings, and a flow of 'Huid from the first into the second upon said piston being in its upper position.
  • a construction including in combination a cylinder formed with transfer ports symmetrically disposed around the entire wall of the cylinder adjacent to the end of the working chamber nearest to the crank shaft, exhaust ports symmetrically disposed around the entire circumference of the cylinder wall adjacent to said transfer ports, a piston movable within said cylinder and adapted to uncover the exhaust ports and subsequently the transfer ports near the end of its stroke nearest to the crank 'shaft and to cover said ports in rever e order upon its return, a skirt portion of reduced diameter adjacent to the lower end of said piston adapted to permit communication between the exhaust ports and transfer ports and a flow of fluid from the first into the second at the time when said piston is near the end of its stroke furthest from the crank shaft.
  • a cylinder having a base portion of enlarged diameter, inwardly extended radial ribs within said enlarged base portion, the inner edges of said ribs being in line with the cylinder wall, a piston movable within said cylinder adapted to override the upper ends of the spaces between said ribs, and a skirt portion of reduced diameter adjacent to the lower end of said piston adapted to inder having exhaust ports and intake ports permit communication between the exhaust each arranged in a circumferential row ports and transfer ports and a flow of fluid therein, means for directing communication l0 from the first into the second at the time between the ports, including a piston formed 5 when said piston is near the end of its stroke With a skirt, said piston skirt having an anfurthest from the crank shaft. nular depression formed therein at its base. 4.
  • engine construction including a cyl- JOI-IN FRANCIS BRICE.

Description

lMarch 24. 1925.
J. F. BRICE ENGINE CONSTRUCTION Filed oct. 11, 1922.
IN VEN T01? Jhn/ Eri By A TTHNEYS WIM/8858 Patented Mar. 24, 1925.
UNITED STATES PATENT OFFICE.
ENGINE CONSTRUCTION.
Application filed October 11, 1922.
To all whom 'it may concern:
Be it known that I, JOHN FRANcis Baron, a citizen of the United States, and a resident of the township of Bensalem, in the county of Bucks and State of Pennsylvania, have invented a new and Improved Engine Construction, of which the following is a full, clear, and exact description.
My invention relates to an engine construction and aims to provide certain new and useful improvements in connection with a device of this character, and more particularly in connection with an internal combustion engine.
In the usual internal combustion engine of the two-cycle type, the combustible charge is admitted into the working chamber by ports at one side of the cylinder and the products of combustion are allowed to escape through ports on the opposite side of the cylinder, a baffle plate being provided upon the top of the piston to prevent as far as possible the intermixture of the fresh gas with the spent gas. Such construction limits the total area of cross-section of the ports thereby limiting the rapidity with which the cylinder is charged and exhausted and thus, in turn, limiting the revolution speed of the engine. It will also be seen that the paths traversed by the incoming and outgoing gases are irregular and unsyinmetrical to a degree and in ways not ascertainable but evidently not conductive to the best results in operation.
It is an object of my invention to provide, by a. new and simple arrangement of ports, very much larger openings for both the admission of the charge and the exhaust of the products of combustion, thus permitting much higher revolution speeds.
It is a further object of my invention to insure by a symmetrical construction that the paths of the incoming and outgoing gases shall be at all phases of operation symmetrical with respect to the axis of the cylinder thereby insuring regularity of operation and greater eiiciency.
It is a further object of my invention to separate the fresh from the spent gases by a cushion of inert gases so as to prevent, on the one hand, preignitioii of the fresh charge and to prevent, on the other hand, wastage Seria1 No. 593,898.
of zhe fresh charge through the exhaust por.
Reference is had to the attached sheets of drawings asl illustrating one practical embodiment of my invention, and it will be seen in these drawings that,
Figure 1 is a sectional side view of an engine of the type stated and showing the parts in the position which they assume at the end of the firing stroke.
Figure 2 is a view showing the disposition of the parts at the beginning of the firing stroke.
Figures 3 and 4L are transverse sectional views taken along the lines 3-3 and 4 4: of Figure 1.
In these views the reference numeral 11 indicates the cylinder mounting an igniting device in the nature of a spark plug 12, and being preferably provided with a jacket 13 for cooling purposes. Further, it willbe noted in the embodiment illustrated that I have shown a crank case 14: within which a crank shaft 15 is rotatably mounted, the latter having one of the ends of the connecting rod 16 attached to its body, the opposite end of said connecting ro'd being attached to the piston 17 which is slidably mounted within the cylinder.
I wish it understood that the foregoing features are merely shown for the sake of illustrating my invention, and the same may be varied and rearranged in any manner desired, it being, of course, noted that in view of the fact that the engine .is of a twocycle type that an intake pipe 18 is connected to the crank case, and serves to introduce a fuel mixture thereinto, this fuel mixture in the usual manner being compressed within the crank case and being introduced into the combustion chamber 19 of the cylinder at the completion of the power stroke.
I-Iowever, it will be seen that contrary to conventional construction I provide a bypass through which the compressed fuel charge is introduced into the cylinder by mounting a series of vanes 20 extending radially inward within the enlarged lower end of the cylinder, and thus spaces 21 are provided between the piston yin its lowermost position and the inner wall of the chamber, and it is through these spaces that CTA the compressed fuel charge flows, the same being introduced at a series of different points in the circumference of the cylinder, as has been shown in Figure 1.
Also, aside from the foregoing, the vanes 2O serve another purpose in that they confine the body of the piston 17 and, consequently, the rings 22 carried thereby are prevented from springing clear of the grooves with which they are associated when the piston is in its lowermost position.
Moreover, contrary to conventional construction, it will be noted that a series of radial ports 23 are provided above the upper ends of the spaces 21, and these ports serve as discharge openings for the products of combustion, and it is obvious that, due to the fact that the same are arranged radially substantially around the entire circumference of the cylinder, these products of combustion will be discharged in the quickest possible time so that the incoming charge of unexploded fuel will not be mixed with a relatively large proportion of the same.
Thus in operation, assuming that the parts are in the position shown in Figure 1 in which the crank shaft 15 is rotating in a clockwise direction, and in which compressed fuel mixture is in the crank case 14, it will be obvious that, due to the fact that the upper edge of the piston 17 is uncovering the upper ends of the spaces 2 1, this compressed fuel mixture will flow 1n the manner indicated by the arrows in Figure 1, in other words, into the combustion chainber 19, it being noted that I deflect this fuel mixture centrally upward, preferably, by utilizing a baffle in the nature of a circular tapered boss 24, carried upon the upper end of the piston and centrally positioned with respect thereto.
Upon the piston moving upward and outward the fuel mixture will be 'further coinpressed, and, upon the parts reaching the position shown in Figure 2, the plug 12 will ignite this charge and serve to thro-w the piston downwardly and inwardly, and, due to the pressure exerted by the products of combustion, it will be obvious that, upon the upper edge of the piston clearing the upper edge of the port openings 23, these products of combustion will be forced through these ports incident to the deiiecting action exerted by the boss 24.
Further, it is to be noted that the lower end of the piston 17 is in the nature of a skirt 25, reduced in diameter to furnish a clearance which is of sufficient width so that when the piston is in its outermost or upper position shown, in Figure 2 it will permit of air iowing through the exhaust ports 23 around this lower end of the piston and so into the spaces 21, where it will form a cushion, separating the fuel charge in the base from the spent gases of the exhaust when the return of the piston to its lowermost position unc-overs the upper ends of the spaces 21, as in Figure 1.
Thus the fuel charge is sucked through the pipe 18 during the upward or compression stroke of the piston, and, upon the crank case having been nearly filled with this mixture, inert gas is subsequently introduced into the upper ends of the spaces 21 Where it will form a protective cushion so positioned as to enter the working cylinder ahead of the fuel mixture when the latter is subsequently transferred, compressed and introduced directly into the combustion chamber in the manner aforementioned.
I would state in conclusion that while the illustrated example constitutes a practica-1 embodiment of my invention I do not limit myself strictly to the exact details herein illustrated since manifestly the same can be considerably varied without departing from the spirit of the invention as defined in the appended claims.
Claims:
1. An engine construction including in combination a cylinder formed with exhaust ports and intake passages, the latter being arranged below the former, a piston movable within said cylinder and/'adapted to cover said openings, a reduced skirt porti-on adjacent the lower end of said piston whereby to permit communication between sa-id openings, and a flow of 'Huid from the first into the second upon said piston being in its upper position.
2. In an internal combustion engine of two-cycle type, a construction including in combination a cylinder formed with transfer ports symmetrically disposed around the entire wall of the cylinder adjacent to the end of the working chamber nearest to the crank shaft, exhaust ports symmetrically disposed around the entire circumference of the cylinder wall adjacent to said transfer ports, a piston movable within said cylinder and adapted to uncover the exhaust ports and subsequently the transfer ports near the end of its stroke nearest to the crank 'shaft and to cover said ports in rever e order upon its return, a skirt portion of reduced diameter adjacent to the lower end of said piston adapted to permit communication between the exhaust ports and transfer ports and a flow of fluid from the first into the second at the time when said piston is near the end of its stroke furthest from the crank shaft.
3. A cylinder having a base portion of enlarged diameter, inwardly extended radial ribs within said enlarged base portion, the inner edges of said ribs being in line with the cylinder wall, a piston movable within said cylinder adapted to override the upper ends of the spaces between said ribs, and a skirt portion of reduced diameter adjacent to the lower end of said piston adapted to inder having exhaust ports and intake ports permit communication between the exhaust each arranged in a circumferential row ports and transfer ports and a flow of fluid therein, means for directing communication l0 from the first into the second at the time between the ports, including a piston formed 5 when said piston is near the end of its stroke With a skirt, said piston skirt having an anfurthest from the crank shaft. nular depression formed therein at its base. 4. In engine construction including a cyl- JOI-IN FRANCIS BRICE.
US593898A 1922-10-11 1922-10-11 Engine construction Expired - Lifetime US1531066A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US593898A US1531066A (en) 1922-10-11 1922-10-11 Engine construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US593898A US1531066A (en) 1922-10-11 1922-10-11 Engine construction

Publications (1)

Publication Number Publication Date
US1531066A true US1531066A (en) 1925-03-24

Family

ID=24376660

Family Applications (1)

Application Number Title Priority Date Filing Date
US593898A Expired - Lifetime US1531066A (en) 1922-10-11 1922-10-11 Engine construction

Country Status (1)

Country Link
US (1) US1531066A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745390A (en) * 1952-05-15 1956-05-15 West Bend Aluminum Co Two-cycle internal combustion engine with improved fuel induction means
US2838035A (en) * 1956-02-01 1958-06-10 Cheminol Corp Internal combustion engine
US4058104A (en) * 1975-04-23 1977-11-15 Automation Equipment, Inc. Hydrostatic bearing piston for a two-cycle engine
US4109622A (en) * 1975-12-16 1978-08-29 Kawasaki Jukogyo Kabushiki Kaisha Two stroke engines
US9151213B2 (en) * 2012-03-29 2015-10-06 Makita Corporation Internal combustion engine, in particular two-stroke internal combustion engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745390A (en) * 1952-05-15 1956-05-15 West Bend Aluminum Co Two-cycle internal combustion engine with improved fuel induction means
US2838035A (en) * 1956-02-01 1958-06-10 Cheminol Corp Internal combustion engine
US4058104A (en) * 1975-04-23 1977-11-15 Automation Equipment, Inc. Hydrostatic bearing piston for a two-cycle engine
US4109622A (en) * 1975-12-16 1978-08-29 Kawasaki Jukogyo Kabushiki Kaisha Two stroke engines
US9151213B2 (en) * 2012-03-29 2015-10-06 Makita Corporation Internal combustion engine, in particular two-stroke internal combustion engine

Similar Documents

Publication Publication Date Title
US1967682A (en) Internal combustion engine
US1486583A (en) Internal-combustion engine
US1531066A (en) Engine construction
US2041708A (en) Combustion engine
US2497781A (en) Forced draft air-cooling system for internal-combustion engines
US1664782A (en) Internal-combustion engine
US1829391A (en) Rotary internal combustion engine
US1789190A (en) Internal-combustion engine
US2204296A (en) Scavenging of the cylinders of twostroke internal combustion engines
US2088215A (en) Multicylinder two-stroke-cycle diesel engine
US884853A (en) Internal-combustion engine.
US1812379A (en) Engine port construction
US1912574A (en) Engine
US2573989A (en) Internal-combustion engine operated on the two-stroke cycle
US1442596A (en) Rotary two-cycle superinduction engine
US2635593A (en) Two-stroke internal-combustion engine
US1744446A (en) Two-cycle internal-combustion engine
US1799498A (en) Aeroplane engine
US1777827A (en) Two-cycle internal-combustion engine
US1960597A (en) Cylinder of two-stroke internal combustion engines
US2859739A (en) Two-cycle scavenging system
US1356730A (en) Internal-combustion engine
US1423578A (en) Two-cycle internal-combustion engine
US1370542A (en) Internal-combustion engine
US1502609A (en) Internal-combustion engine