AU5812786A - Axial shaft piston engine - Google Patents

Axial shaft piston engine

Info

Publication number
AU5812786A
AU5812786A AU58127/86A AU5812786A AU5812786A AU 5812786 A AU5812786 A AU 5812786A AU 58127/86 A AU58127/86 A AU 58127/86A AU 5812786 A AU5812786 A AU 5812786A AU 5812786 A AU5812786 A AU 5812786A
Authority
AU
Australia
Prior art keywords
pistons
shaft
piston
cam
cylinder
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.)
Abandoned
Application number
AU58127/86A
Inventor
Cahill Robert Charles
Vickery Lyn
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.)
Cahill Robert C
Original Assignee
CAHILL R C
VICKEREY L
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 CAHILL R C, VICKEREY L filed Critical CAHILL R C
Priority to AU58127/86A priority Critical patent/AU5812786A/en
Publication of AU5812786A publication Critical patent/AU5812786A/en
Abandoned legal-status Critical Current

Links

Landscapes

  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

AXIAL SHAFT PISTON ENGINE This invention relates to a mechanism which may be used as an internal combusion piston engine or positive displacement piston pump or compressor -in which the output shaft is co-axial with the pistons and in which the reciprocating movement of the pistons is transformed into rotational movement of the shaft (and vice versa) by means of one or more cylinder cams mounted on the shaft and acting with rollers attached to the pistons.
Conventional piston engines and pumps utilize a piston(s) - connecting rod - crankshaft arrangement in which the direction of the piston movement is at right angles to the axis of crankshaft rotation. This results in complexity in terms of parts, high reciprocating mass, side thrust on pistons, complexity of manufacture of crankshaft and crankcase assemblies, comparative large physical size per unit capacity and difficulty in balancing reciprocating masses, particularly in single cylinder units.
The objects of this invention are to reduce physical size for a given capacity, simplify the manufacture of the major structural parts, reduce the number of parts, simplify the balancing of reciprocating masses, and increase mechanical efficiency.
The objects of this invention are achieved by arranging the pistons and shaft co-axially, with the shaft running through the centre of the pistons.
The pistons and cylinders are arranged such that the pistons move inwards and outwards in their cylinders concurrently under the effects of the gas pressures in the combustion chambers and act, via rollers mounted in a yoke attached to extensions of the pistons, on the cylinder cam which is mounted on, and forms part of, the axial output shaft. This in turn produces torque in the shaft.
Conversely, in the pump configuration, torque applied to the shaft rotates the cylinder cam which acts on the rollers and causes the pistons to reciprocate in their respective cylinders. FEATURES
30 The features that distinguish this mechanism from other piston engines are as follows;
1/ The use of a cylinder cam instead of a crankshaft. 2/ Output shaft co-axial with piston movement.
OPERATION
The following details the operation, of the engine.
FIGURES 1A, IB & 1 C show the mechanism as an internal combustion engine (see also schematic diagrams FIG 2 & 3).
Two pistons (1) & (2) (FIG IB), reciprocate in cylinders (3) & (*r). Each of which is enclosed at its end by an end cap (5) &(6) (FIGS 1 A δc 1C) which 40 together with the top end of the piston (1) & (2), forms the combustion chambers (7) & (8).
A shaft (9) runs axially through the centres of the end caps and the pistons and carries a specially shaped cylinder cam (10) at its centre.
The cam (10) is straddled by double rollers (11)(12) & (1-0(13) (FIG IB) which are mounted in yokes (2 ) & (25) attached to an extension of each piston (1) & (2), thus causing the pistons to reciprocate longtitudinally as the shaft (9) and cam (10) rotate.
FIGURES 2 & 3 are schematic representations of the mechanism. The fuel air mixture enters, via a carburettor and valve (16) FIG 2, into the 50 space (15) formed by the pistons around the cam as the pistons move outward. Movement of the pistons inward due to the further rotation of the cam results in the valve (16) closing and the fuel air mixtures starts to compress in space (15). When the pistons approach their inner most position, the induction port (17) is uncovered by the pistons and the pressurised charge transfers from the space (15), via the transfer ports (18) into the combustion chambers (7) _c (8).
Further rotation of the shaft and cam causes the pistons to again move outward, covering the induction ports (17) and the exhaust ports (19) and compressing the fuel air charge in the combustion chambers (7) & (8).
At the appropriate time, the spark plug (20) ignites the fuel thus causing a gO pressure build up in the combustion chambers (7) & (8) and the pistons to be forced inwards. This imparts a force to the cam (10) via the rollers (11) & (13) and causes the cam to rotate and impart torgue to the shaft (9).
Further inward motion of the pistons uncovers the exhaust ports (19) thus allowing the burn't gases to escape ready for the induction of a fresh charge of fuel and air. As the shaft rotates further, the inlet ports (17) open and the cycle repeats.
Torque reaction on the pistons (1) & (2) is opposed by flat linear roller bearings (27) acting between the piston yokes (24) & (25) FIGURE Ψ forming part of the piston extension, and the centre section engine casing, (26) FIG 4.
70 The foregoing describes the operation when the mechanism is used as a power producing device.
CYLINDER CAM VARIATIONS
Whilst the foregoing description relates to drawings which show a two lobe cam (10), giving one inwards and one outwards piston stroke per revolution of the shaft (9), a multi lobe cam may be used to give more strokes per shaft revolution.
FIG 6., shows a four lobe cylinder cam which will give two inward and two outward strokes of the pistons (1) & (2) per revolution when mounted on th shaft (9) in place of the two lobe cam - FIG 5. This will provide two power
80 pulses per revolution of the shaft, hence increasing torque, when used in the
SUBSTITUTE SHEET i
internal combustion engine configuration or two pumping strokes per revolution when used in the pump configuration.
MECHANISM AS A PUMP DEVICE
The operation when used as a pump is as follows.
FIGURE 7 depicts one end i.e. one pumping chamber for simplicity. When the shaft (9) is turned by external means, the cylinder cam (10) rotates and causes the psitons (1) & (2), by means of the rollers (12) & (14), to move inwards and draw fluid (gaseous or liquid) through the valve (21) into the annular space (7). Further rotation of the shaft (9) causes the pistons (1) & (2) 90 by means of the rollers (11) & (13) to move inwards and force the fluid from the space (7) out of the valve (22).
A further application of this configuration would have one chamber used as an internal combustion power producing piston engine (as in FIG 3) and the other chamber used as a pump.
SUBSTITUTE SHEET

Claims (1)

  1. The claims defining the invention are as follows;
    1/ An engine having its output shaft axialiy through the centre of the pistons and cylinders and shaft torque being produced by means of pistons acting on one or more single or double lobe cylinder cams mounted on and forming part of the shaft.
    2/ An internal combustion engine having two combustion chambers, one at the outer extremity of each of the two opposed pistons each of which moves inwards and outwards in cylinders concurrently and each acting via rollers 1 0 attached to an extension of each piston, on a cylinder cam located between the pistons and mounted on and forming part of the axial output shaft so as to cause rotation of the shaft when pressure is applied to the pistons.
    3/ Application of a piston - cam - shaft arrangement described in claims 1 & 2 in a fluid pump (liquid or gaseous) or compressor utilizing an axial drive shaft passing through the centre of the pistons and cylinders and driven by external means.
    4/ Combination compressor/ pump & internal combustion engine utilizing the piston - cam - shaft arrangements described in claims 1 & 2. Using one end i.e., piston and cylinder (claims 1 & 2), as power producing section and the 20 opposite piston & cylinder as a fluid pump or compressor (claim 3).
    SUBSTITUTE SHEET
AU58127/86A 1985-01-31 1986-01-31 Axial shaft piston engine Abandoned AU5812786A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU58127/86A AU5812786A (en) 1985-01-31 1986-01-31 Axial shaft piston engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU909485 1985-01-31
AU58127/86A AU5812786A (en) 1985-01-31 1986-01-31 Axial shaft piston engine

Publications (1)

Publication Number Publication Date
AU5812786A true AU5812786A (en) 1986-08-26

Family

ID=25613373

Family Applications (1)

Application Number Title Priority Date Filing Date
AU58127/86A Abandoned AU5812786A (en) 1985-01-31 1986-01-31 Axial shaft piston engine

Country Status (1)

Country Link
AU (1) AU5812786A (en)

Similar Documents

Publication Publication Date Title
US3945359A (en) Rotor engine
US6739307B2 (en) Internal combustion engine and method
US4022167A (en) Internal combustion engine and operating cycle
USRE30565E (en) Internal combustion engine and operating cycle
AU738469B2 (en) Reciprocating rotary piston system and pressure pump and internal combustion engine using the same
US3256866A (en) Internal combustion engine
US4077365A (en) Expansible chamber apparatus
US4038949A (en) Rotary-radial internal combustion engine
US5146880A (en) Radial cylinder machine
EP0320171A1 (en) Power transmission apparatus
US4214557A (en) Pivoting wall type, four stroke, internal combustion, rotary engine
US4553503A (en) Rotary piston machine
US6601547B2 (en) Axial piston rotary power device
WO1986004637A1 (en) Axial shaft piston engine
JP3377968B2 (en) Internal combustion rotary engine and compressor
AU5812786A (en) Axial shaft piston engine
AU684008B2 (en) Spherical piston radial action engine
JPH08177511A (en) Cam type engine
KR940003525B1 (en) Rotary engine
KR100336159B1 (en) Combustion Motor
US7584726B2 (en) Two-stroke opposite radial rotary-piston engine
EP1085182A1 (en) Internal combustion rotary engine
KR100213733B1 (en) An internal combustion engine
CA2308129A1 (en) Gas and air engine
KR920000990B1 (en) Rotary engine