GB2027122A - Reciprocating Piston Machines - Google Patents
Reciprocating Piston Machines Download PDFInfo
- Publication number
- GB2027122A GB2027122A GB7918284A GB7918284A GB2027122A GB 2027122 A GB2027122 A GB 2027122A GB 7918284 A GB7918284 A GB 7918284A GB 7918284 A GB7918284 A GB 7918284A GB 2027122 A GB2027122 A GB 2027122A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- cylinder
- axis
- machine according
- valve
- 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.)
- Granted
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F01B3/0032—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis having rotary cylinder block
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F01B3/0082—Details
- F01B3/0085—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/02—Surface coverings of combustion-gas-swept parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/11—Thermal or acoustic insulation
- F02B77/13—Acoustic insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J10/00—Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
- F16J10/02—Cylinders designed to receive moving pistons or plungers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/08—Ceramics; Oxides
- F05C2203/0804—Non-oxide ceramics
- F05C2203/0856—Sulfides
- F05C2203/086—Sulfides of molybdenum
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/08—Ceramics; Oxides
- F05C2203/0865—Oxide ceramics
- F05C2203/0882—Carbon, e.g. graphite
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/042—Expansivity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2253/00—Other material characteristics; Treatment of material
- F05C2253/12—Coating
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
In a two or four-stroke I.C. engine or a pump the pistons 8 are fixed to an inclined member 6a and reciprocate in cylinders 9, rings 19 mounted on and movable laterally of the pistons during reciprocation providing sealing with the cylinders. A rotary inlet and exhaust valve 30 is rotatable relative to the cylinder block 1 by belt gearing 32b, sealing rings and strips (35, 36), Figs. 5a to 5d (not shown), providing sealing around the valve passages 32, 33 at the valve periphery. Details are given of materials for the piston and valve seating rings, the block 1 and the valve 30. Exhaust gases are discharged through a chamber 42 containing sound deadening material 43 behind a perforated plate 46. <IMAGE>
Description
SPECIFICATION
Piston and Cylinder Machines
This invention relates to a piston and cylinder machine, e.g. an engine or pump.
According to the invention, there is provided a machine comprising:
a cylinder having a straight sided bore spaced from a first axis,
a piston assembly including a piston which is disposed within said cylinder bore to form a chamber therein, the piston assembly further including a connecting portion connected to the piston and restraining means for resisting any tendency for the piston to move in relation to the cylinder about the first axis,
an inclined member mounted for relative rotation between the inclined member and the cylinder to occur about the first axis, the inclined member being inclined to the first axis along a second axis and the said connecting member being engaged with the inclined member such that said relative rotation of the cylinder and the inclined member is accompanied by reciprocation of the piston within the cylinder, and
a rotary valve which communicates with said chamber and between which and said cylinder there is relative rotation about an axis parallel to or coincident with said first axis.
For a better understanding of the invention, and to show how the same may be carried into effect, reference will now be made, by way of example, to the accompanying drawings, wherein Figure 1 is a diagrammatic partly sectional elevation of an engine,
Figures 2 and 3 are a sectioned side view and a sectioned plan view respectively of a piston used in the engine of Figure 1,
Figure 3 is a sectioned side view of a part of a modified piston,
Figure 5a is a perspective view of a valve used in the engine of figure 1,
Figures Sb to 5d are explanatory diagrams relating to figure 5a, and
Figure 6 is a series of diagrams showing the operating sequence of a valve used in the Figure 1 engine.
The engine of figure 1 comprises a cylinder assembly including a cylinder block 1 formed with an axiaily extending hollow shaft portion la. The shaft portion 1 a is mounted in bearings 2 and 3 so that the whole cylinder assembly can rotate about an axis X. The cylinder block 1 is enclosed in a stationary casing 4 having a hollow projecting portion 5 which extends inwardly from one end of the casing and which forms a housing for the bearings 2 and 3. Part of the portion 5 defines a cylindrical surface 5a of which the axis y is inclined to the axis x. A piston assembly 6 is supported on this surface by way of a bearing 7 such that the piston assembly can rotate about axis y.The piston assembly comprises a connecting member 6a which is mounted at its centre on the bearings 7 and which has three
radially extending portions to each of which is
attached a piston 8, each piston being disposed
within a respective cylinder bore 9 in the cylinder block 1. Rotation of the cylinder assembly about the axis X is accompanied by rotation of the piston assembly about'the axis Y and, since axes X and Y are inclined to one another, such rotation is further accpmpanied by reciprocation of each piston relative to its respective cylinder bore.
As mentioned there are three pistons and correspondingly, the cylinder block has three bores, these being arranged equidistant about axis of rotation X. In figure 1 to better illustrate the construction, only two pistons and two bores are shown spaced at 1 800 whereas in fact there are three and they are spaced at 1 200 intervals.
As shown in figures 2 and 3, each piston 8 comprises a part defining a sloping piston crown
10 and a spigot 11 which extends back from the crown 10 and is attached by screws 12 to the connecting member 6a. Disposed around the spigot 11 between the connecting member 6a and the crown 10 is a cylindrical member 13 of which the end next to the crown 10 is reduced in diameter so as to form shoulder which, with the rear of the crown 10, defines a circular recess 14.
A short way back from this end of the member
13, there is an annular flange 1 3a and round the member 13 there is a further cylindrical member 1 3b which has the same external diameter as the flange 1 3a, and which extends from the other end of the member 1 3 up to a short distance from the flange 1 3a such that there is defined a groove or channel 15 between the flange 1 3a and member 1 3b. In this groove 15 there is disposed a ringshaped member 1 6 with clearance between the inner surface of the ring-shaped member 1 6 and the floor of the groove 15 so that the member 16 can move as a whole laterally with respect to the member 13.In one and only one of the pistons 8, the groove 15 and member 16 are as shown in figure 3, that is with two opposite "flats" and only sufficient clearance between the flat portions of the inner surface of the member 1 6 and the flat portions the floor of the groove 1 5 to allow sliding movement. Thus, for this piston 8, the movement of the member 1 6 with respect to the member 13 is restricted to the directions towards and away from the axis Y in figure 1. Fitted closely around the member 16 such that there is clearance between it and the member 13, is a collar 1 7 which is formed with a recess 18 8 for receiving a continuous piston ring 9 (i.e. a ring which is continuous all around its circumference instead of being split as in conventional piston rings) and with an inwardly directed flange 20 which extends into the recess 14.Between the flange 20 and that wall of the recess 14 which is formed by the shoulder of the member 13 there is disposed a thrust bearing spacer annulus 21 to take the thrust exerted by the piston ring 1 9 via the collar 17. The piston ring 19 has an external periphery in the shape of an equatorial region of a sphere of diameter equal to that of the cylinder bore. An ignition plug 22 is screwed into a threaded bore formed in the piston crown 10 such that the plug can ignite fuel/air mixture within the cylinder. It will be appreciated from a consideration of figure 1 that, as each piston 8 reciprocates with respect to its cylinder, it moves along an arcuate path such that its distance from axis X changes during the reciprocation.This change in distance is taken up by the lateral movability as a whole of the ring-shaped member 16 and hence also of the collar 17 and piston ring 19, each as a whole, with respect to the member 13. The limitation of this movement, for one of the pistons, to the direction towards and away from the axis X ensures that the piston assembly is restrained from rotation in relation to the cylinder block and the pistons remain substantially central within the cylinder bores.
Each piston crown 10 and/or the end surface of
each cylinder could be coated with ceramic
material to reduce heat loss from the combustion
chamber.
The construction of the piston may be modified
in various ways. For example, instead of having
the relatively complex internal structure shown in
figures 2 and 3, it could comprise a simple main
body part 41 and a removable crown 42 as shown in figure 4, the body part 41 being shaped
such that between it and the crown 42 there is
formed a groove 43 for the piston ring 44. The
floor of the groove is circular but with two
opposite "flats", i.e. the same shape as the groove
15 in figure 3. Then, for one of the pistons, there
is provided an intermediate ring-shaped member
44 which also has two opposite "flats" on its
internal surface which mate with the flats of the floor of the groove 43 and limit the relative
movement of the piston ring 44 of this piston to the directions towards and away from the axis X
in figure 1.The intermediate ring 44 is not
provided in the other pistons so that, here, the
piston ring can move in all directions laterally with
respect to the piston.
Instead of being continuous, the piston ring
could be split at a point on its circumference in the manner of a conventional piston ring. Then it is
preferred that the split should follow a diagonal,
cranked or other tortuous path across the width of the ring so as to reduce the possibility of gas
leakage through the split. The piston ring 1 9 could be made of synthetic plastics material or
metal, or metal which is coated with synthetic
material or plated with another metal. The main criteria is that the material forming the surface which contacts the cylinder should be compatible with the cylinder material or the material of the cylinder liner if these are provided.If the chosen ring material is such that allowing for relative coefficients of expansion of this material and the cylinder material and the different temperature rises which they may undergo during operation of the engine, the ring material will expand more than the cylinder, it may be necessary to give the ring a composite construction. For example, each piston ring 19 may consist of two concentric rings one within the other and bonded or shrunk together the outermost ring being profiled to form the equatorial zone of a sphere of a diameter equal to the diameter of the cylinder.Then, to maintain a constant sealing clearance between the profiled ring and the cylinder, the coefficients of expansion of the two rings and the cylinder are chosen so that the following condition applies: D1x1t1=D2x2t2+2wx3t3 where t1 , t2 and t3 are the respective temperature rises of the cylinder and the inner and outer rings during operation of the engine, D1 and D2 are the diameters of the cylinder bore and the inner ring respectively and,
x,=coefficient of expansion of cylinder
x2=coefficient of expansion of inner ring
x3=coefficient of expansion of outer ring
w=radial thickness of inner ring.
The function of the inner ring could be taken over by the collar 17, ia the ring itself being made in one piece and of material having a coefficient of expansion x3 and the material of the collar 1 7 having a coefficient x2.
A combined rotary inlet and exhaust valve 30 is mounted in a valve housing formed in the cylinder block 1. The valve has a tubular extension 31 which passes through and is rotatabie in the hollow shaft 1 a of the cylinder block.
Referring to figure 5a as well as figure 1, the valve itself comprises a cylindrical member with ports 32 and 33 formed therein. Port 32 leads from the interior of the tubular extension 31 to one position on the cylindrical surface of the valve and the port 33 leads from another position on this surface to the end of the valve furthest from the extension 31. A port 34 in the wall of each cylinder leads to the valve so that each cylinder port 34 communicates periodically with each of the ports 32 and 33. Fuel/air mixture is made available to the port 32 via the interior of the extension 31 and exhaust gases are emitted via port 33.That end of the extension 31 which protrudes from the end of the cylinder block shaft portion 1 a is fitted with a toothed pulley wheel 32a which is coupled via two toothed belts 32b and two intermediate pulleys 32c to a puiley 32d which is fitted to the shaft portion 1 a. The pulleys 32c are of such relative size that the valve 30 is rotated at one and a half times the speed of the cylinder block. To maintain the belts in position on the pulleys 32a 32c and 32d and to prevent the belts from jumping teeth on the pulleys and thereby changing the relative positions of the different pulleys, spring mounted idler pulleys (not shown) are arranged to press on the outer surfaces of the belts at appropriate positions near the other pulleys.
Because of the relative speeds of the cylinder block and valve, gas is induced, compressed and ignited, expanded and exhausted in each cylinder once per two revolutions of the system, the
positions on the surface of the valve where the
ports 32 and 33 open being such as to give
correct timing of these functions. Figure 6 shows
the relative positions of the rotary valve as each
cylinder moves into the top dead centre position.
It requires two revolutions after the first position
shown i.e. ignition in cylinder 1, for the valve to be
again in the correct position for ignition in cylinder
1.
At each end of the valve 30 there is a groove
containing a spring ring 35. Extending between
the two rings 35, one on that side of each of the
ports 32 and 33 which is furthest from the other
port and one between the two ports, are
lengthwise grooves each containing a sealing
strip 36, each end of each strip being engaged
with the adjacent ring 35 so as to allow
differential expansion of the rings and strips while
enabling the strips to be maintained in position
and to be sprung outwardly by the rings 35
against the surface of the valve housing formed in
the cylinder block. For example, the strips may be
engaged with the rings by the means shown in
figures Sh and 5c. Each ring is split, the ends at
the split being stepped as shown in figure 5d. The
rings and strips provide "piston ring" type sealing
between the valve and the valve housing.As an
alternative to what is shown, the rings and strips
could be mounted in grooves in the internal
surface of the valve housing and arranged to
spring inwardly onto the valve, in which case only
two strips are necessary.
The carburettor 37 is stationary and
communicates with the inlet passage through the
tubular extension 31 of the rotary valve via a
rotating seal, inlet gases passing through the inlet
passage in the valve and into the cylinder port 34.
The valve remains open during the induction
stroke and is closed during the compression and
ignition stroke. The exhaust passage 33 in the
valve communicates with the cylinder port 34
during the exhaust stroke.
The engine drive shaft 38 has a hollow,
enlarged end 39 which is fixed by means of a
flange 40 to the cylinder block around the valve
housing therein. Fixed within the casing 4, around
the enlarged end 39, is a partition plate 41 which bounds one side of a chamber 42 containing
sound deadening material 43 such as glass or
wire wool. The other side of the chamber is abounded by a plate 44 fixed to shaft 38. The
diameter of the plate 44 is such that there is left a
gap all round the periphery of the chamber.
Exhaust gases pass from the port 33 into the
hollow end 3a of shaft 38 and then via radial ports
45 in this end to the chamber 42 where they pass
over the sound deadening material 43 and thence
to the exterior via the open periphery of the
chamber. The sound deadening material 43 is
held in place by a dished member 46 made of
perforated metal for example.
Various alternative exhaust systems could be
used instead of the particular one shown. For
example, a stationary exhaust manifold may
communicate with the port 33 by way of a sliding or labyrinth seal, there then being provided a stationary silencer which may be remote from the engine, or the plate 41 in the illustrated arrangement could be replaced by a shallow cylindrical dish fixed to the shaft portion 39 instead of to the casing 4 so that the whole of the silencer system rotates with the shaft.
The ignition plugs 22 communicate cyclically with an electrical contact 22a fixed to the casing.
The ignition make and break (not shown) is operated on a single lobe cam from an extension to the shaft carrying the idler timing pulleys or gears 32 which if arranged to rotate at valve speed i.e. 12 times engine speed will produce a spark at each revolution of the valve and ignite consecutively cylinders 1,2 and 3 as shown in figure 5.
The rotary valve and its housing are made of material of a similar coefficient of expansion, for
example aluminium alloy, one valve sealing surface being coated with a high temperature synthetic polymer, or a metal mixed with synthetic polymer, graphite, molybdenum disulphide or other lubricative material, the other hardened by anodising or having a coating of metal, ceramic or synthetic polymer compatible with the mating surface. The coated surfaces may be sprayed, for example, by means of a plasma arc gun, with particles of the coating material or alternatively the coating may be plated or deposited chemically or mechanically onto the valve sealing surface. The coating is sufficiently thin to ensure that over the temperature range to which the valve is subjected the sealing clearance between the valve and its housing remains substantially constant.
Air cooling ducts may be formed in the cylinder block comprising for example three parallel holes intermediate to the cylinder bores and adjacent to the rotary valve which communicate with a series of radial holes passing to the outer periphery of the block, thus air is centrifuged out through the radial holes and drawn in along the parallel holes.
Furthermore, instead of or in addition to tnis
illustrated means for preventing circumferential
movement of the pistons relative to the cylinders
about the axis of rotation of the engine by
restricting the piston ring movement, i.e. the flat
parallel portions in the piston and the
correspondingly shaped intermediate member as
shown in Figure 3, the piston rotor and cylinder
block could be coupled together by way of a linear
bearing arrangement as disclosed in UK Patent
specification No.1,511,232 for example, the
arrangements comprising the members 103, 104
and such illustrated in figure 10 of the drawings
of that specification.
Instead of being as shown, the cylinder block of
the engine could rotate about axis Y and the
pistons about axis X.
Furthermore, instead of the piston(s) and
cylinder(s) rotating it could be the member 5 in
figure 1 which rotates, the member 5 instead of
being formed as part of the engine casing being
coupled to an engine output shaft for example to rotate with it. It will be appreciated that the basic operation of the engine is still the same since it is the relative rotation of the member 5 and the piston/cylinder assembly which produces or which is produced by the reciprocation of the pistons in the cylinders. Machines wherein the support member rotates and the piston/cylinder assembly does not are disclosed in specification No. 1,511,232 and the present invention includes the modification of any of those machines to include a rotary valve of the kind disclosed herein.
It may of course be necessary to modify the arrangement for driving the rotary valve and/or to modify its speed of rotation.
The construction illustrated could be adapted to form a pump. For example the ignition plugs carburettor and exhaust silencer system could be discarded and a drive motor provided to rotate the shaft 38.
The engine could be adapted for two-stroke operation by changing the relative speed of the valve 30 and cylinder block. Then the valve 30 could be modified so that it controls only the flow of fuel/air mixture into each cylinder, the exhaust gases being emitted via an exhaust port in the cylinder which is uncovered by the piston as it moves to the outer limit of its reciprocation. Also, there could then be a number of cylinders other than three.
With four-stroke operation there could be only one cylinder without substantial modification of valve 30 or, with such modifications, a number of cylinders other than one or three.
For example the valve could have more than one pair of ports or there could be more than one valve displaced along axis X. Particularly where member 5 rotates while cylinder block 1 is fixed, the axis of valve 30 could be displaced from axis
X, for example there could be a respective valve adjacent each cylinder and arranged to serve only that cylinder. For a three cylinder engine only one of the pistons rings is restricted in its lateral movement with respect to its associated piston, the other two rings being able to move in all directions laterally so as to take up the relative sideways changes in position which occur between the associated pistons and cylinders. In an engine having other than three cylinders it may be possible for say two of the piston rings to be restricted in the direction in which they move this depending upon the geometry of the relative movement between piston and cylinder assemblies of the engine concerned.
The piston crown 10 could have a shape other than that shown for example it could be flat and perpendicular to the piston axis.
Claims (15)
1. A machine comprising:
a cylinder having a straight sided bore spaced from a first axis,
a piston assembly including a piston which is disposed within said cylinder bore to form a chamber therein, the piston assembly further including a connecting portion connected to the piston and restraining means for resisting any tendency for the piston to move in relation to the cylinder about the first axis,
an inclined member mounted for relative rotation between the inclined member and the cylinder to occur about the first axis the inclined member being inclined to the first axis along a second axis and the said connecting member being engaged with the inclined member such that said relative rotation of the cylinder and the inclined member is accompanied by reciprocation of the piston within the cylinder, and
a rotary valve which communicates with said chamber and between which and said cylinder there is relative rotation about an axis parallel to or coincident with said first axis.
2. A machine according to claim 1, wherein the rotary valve comprises a rotary member having at least one port therein, the member being in contact with an engine part which has a port therein and being able to rotate with respect to said engine part such that the ports periodically communicate with one another.
3. A machine according to claim 2, wherein said member and said engine part are made of material having substantially the same coefficient of thermal expansion and at least one of the said member and said engine part, on a surface thereof which is in contact with the other, has a coating of non-metallic lubricative material.
4. A machine according to claim 3, wherein said coating has been made by spraying said surface with metallic particles at high temperature to form a rough bonding coat and then the surface is sprayed with the lubricative material.
5. A machine according to claim 2, including elongate spring members mounted between said rotary member and said engine part to provide sealing therebetween.
6. A machine according to claim 2, wherein the rotary member is cylindrical and the said engine part comprises a hollow member within which the rotary member is mounted.
7. A machine according to claim 6, wherein said engine part is a cylinder block, portions of which define said cylinder.
8. A machine according to claim 1, wherein said inclined member is fixed and said cylinder is arranged to rotate about said first axis, the piston assembly being coupled to the incined member for rotation about said second axis.
9. A machine according to claim 1, wherein the piston assembly includes a piston ring disposed around said piston, the piston ring having a periphery in the shape of an equatoral region of a sphere of radius equal to that of the cylinder and the ring being able to move as a whole laterally with respect to the piston.
10. A machine according to claim 9, wherein said restraining means comprises means for restricting the lateral movement of said piston ring with respect to the piston to the directions substantially radial to the said second axis.
11. A machine according to claim 10, wherein the piston comprises a peripheral recess of which the floor has two opposite flat portions, and wherein said restraining means comprises a ringshaped member which has two flat internal surface portions corresponding to those of the floor of said recess and which is engaged in said groove.
12. A machine according to claim 9 wherein at least the surface of said piston ring is made of synthetic plastics material.
13. A machine according to claim 9, wherein the piston ring has a composite construction consisting of two concentric ring-shaped members shrunk or bonded together and consisting of material of differing coefficients of expansion to obtain an effective overall coefficient of expansion such that the piston ring and said cylinder expand by substantially the same amount during operation of the machine.
14. A machine according to claim 1, wherein there are three cylinders spaced around said first axis and said piston assembly comprises three pistons disposed within respective ones of said cylinders, the machine being constructed as a four cycle internal combustion engine and said valve being arranged to rotate about said first axis at one and a haif times the speed of the engine and to communicate alternately with the three cylinders.
15. A piston and cylinder machine substantially as hereinbefore described with reference to the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7918284A GB2027122B (en) | 1978-05-25 | 1979-05-25 | Reciprocating piston machines |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2978879 | 1978-05-25 | ||
GB7918284A GB2027122B (en) | 1978-05-25 | 1979-05-25 | Reciprocating piston machines |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2027122A true GB2027122A (en) | 1980-02-13 |
GB2027122B GB2027122B (en) | 1982-08-25 |
Family
ID=26260085
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7918284A Expired GB2027122B (en) | 1978-05-25 | 1979-05-25 | Reciprocating piston machines |
Country Status (1)
Country | Link |
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GB (1) | GB2027122B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4518642A (en) * | 1983-04-15 | 1985-05-21 | International Jensen Incorporated | Loudspeaker diaphragm and method for making same |
EP0288440A1 (en) * | 1987-04-07 | 1988-10-26 | Alberto Orzi | Rotary axial piston internal combustion engine |
WO1994010443A1 (en) * | 1992-10-30 | 1994-05-11 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
US5636561A (en) * | 1992-10-30 | 1997-06-10 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
EP1412617A1 (en) * | 2001-07-25 | 2004-04-28 | Shuttleworth Axial Motor Company Limited | Improvements relating to axial motors |
WO2005012692A1 (en) * | 2003-07-25 | 2005-02-10 | VOGLAIRE, Hélène | Multicylinder barrel-type engine |
CN113464517A (en) * | 2021-05-24 | 2021-10-01 | 青岛张氏上佳科技有限公司 | Noise reduction type piston rod |
-
1979
- 1979-05-25 GB GB7918284A patent/GB2027122B/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4518642A (en) * | 1983-04-15 | 1985-05-21 | International Jensen Incorporated | Loudspeaker diaphragm and method for making same |
EP0288440A1 (en) * | 1987-04-07 | 1988-10-26 | Alberto Orzi | Rotary axial piston internal combustion engine |
WO1994010443A1 (en) * | 1992-10-30 | 1994-05-11 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
WO1994010442A1 (en) * | 1992-10-30 | 1994-05-11 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
US5636561A (en) * | 1992-10-30 | 1997-06-10 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
EP1412617A1 (en) * | 2001-07-25 | 2004-04-28 | Shuttleworth Axial Motor Company Limited | Improvements relating to axial motors |
EP1412617A4 (en) * | 2001-07-25 | 2004-11-03 | Shuttleworth Axial Motor Compa | Improvements relating to axial motors |
US7117828B2 (en) | 2001-07-25 | 2006-10-10 | Shuttleworth Axial Motor Company Limited | Axial motors |
WO2005012692A1 (en) * | 2003-07-25 | 2005-02-10 | VOGLAIRE, Hélène | Multicylinder barrel-type engine |
CN113464517A (en) * | 2021-05-24 | 2021-10-01 | 青岛张氏上佳科技有限公司 | Noise reduction type piston rod |
CN113464517B (en) * | 2021-05-24 | 2023-09-15 | 青岛张氏上佳科技有限公司 | Noise reduction type piston rod |
Also Published As
Publication number | Publication date |
---|---|
GB2027122B (en) | 1982-08-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |