U.S. patent number 3,797,464 [Application Number 05/205,197] was granted by the patent office on 1974-03-19 for balanced rotary combustion engine.
Invention is credited to Harold G. Abbey.
United States Patent |
3,797,464 |
Abbey |
March 19, 1974 |
BALANCED ROTARY COMBUSTION ENGINE
Abstract
A rotary internal combustion engine of symmetrically balanced
construction. The engine includes a stator having a circular
chamber provided with a pair of diametrically-opposed combustion
cavities having igniters therein. Concentrically mounted within the
stator is a rotor having at least one pair of lobes. The stator
chamber is effectively divided into two distinct sections by means
of gas-separating vanes which are disposed at diametrically-opposed
positions along an axis at right angles to the common axis of the
combustion cavities, the gas-separating vanes continuously engaging
the surface of the rotor. Associated with each vane is an exhaust
port through which spent gases are forced out by a lobe advancing
toward the vane, and an air-gas intake port through which a fuel
mixture is admitted for compression by a lobe moving away from the
vane.
Inventors: |
Abbey; Harold G. (East Orange,
NJ) |
Family
ID: |
22761212 |
Appl.
No.: |
05/205,197 |
Filed: |
December 6, 1971 |
Current U.S.
Class: |
123/229;
418/248 |
Current CPC
Class: |
F01C
1/3566 (20130101); F02B 2075/027 (20130101) |
Current International
Class: |
F01C
1/356 (20060101); F01C 1/00 (20060101); F02B
75/02 (20060101); F02b 053/08 () |
Field of
Search: |
;123/8.09,8.33
;418/248,243-251 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Husar; C. J.
Claims
I claim:
1. A rotary internal combustion engine comprising a rotor
concentrically-disposed within a stator having a circular chamber,
said rotor being formed with at least one pair of lobes whose
crests engage the inner wall of the chamber, concave zones being
formed in the space between the lobes, each lobe having a cavity
formed in the crest thereof, said stator including:
A. first and second gas-separating vanes mounted at
diametrically-opposed positions and adapted continuously to engage
the surface of the rotor;
B. an intake port adjacent each separating vane at a position
subsequent to the vane in the direction of rotor movement, an
air-gas mixture being supplied to said intake port,
C. an exhaust port adjacent each separating vane at a position in
advance of said vane in the direction of rotor movement;
D. first and second combustion cavities disposed at
diametrically-opposed positions along a common axis at right angles
to the axis passing through said gas-separating vanes, said
combustion cavities including igniters to ignite the mixture
brought therein when the cavity of each lobe lies in registration
therewith;
E. a closure vane adjacent each combustion cavity at a position in
advance thereof in the direction of rotor movement, said closure
vane being adapted to continuously engage the surface of the rotor
in the course of rotor movement and
F. a sealing vane adjacent each combustion cavity at a position
subsequent thereto in the direction of rotor movement, said sealing
vanes being adapted to engage the surface of said rotor only when
the depth of the concave zones between lobes is relatively
shallow.
2. An engine as set forth in claim 1, wherein each lobe is provided
with a sealing vane at its crest which engages the wall of the
chamber, said sealing vane being subsequent to the lobe cavity in
the direction of movement.
3. An engine as set forth in claim 1, wherein said rotor is
provided with two pairs of lobes, the lobes being radially
displaced ninety degrees from each other.
4. An engine as set forth in claim 1, wherein said igniters are
spark plugs.
5. An engine as set forth in claim 1, wherein said vanes are
spring-biased.
6. An engine as set forth in claim 1, wherein said gas-separating
vanes are displaced ninety degrees and two-hundred seventy degrees
with respect to said circular chamber, and said combustion cavities
are disposed at zero degrees and one-hundred eighty degrees,
respectively.
7. An engine as set forth in claim 1, wherein said rotor is
centrally mounted on a shaft supported by bearings in the ends of
said stator.
8. An engine as set forth in claim 1, wherein said rotor has two
lobes diametrically-opposed to each other.
Description
BACKGROUND OF THE INVENTION
This invention relates generally to rotary internal combustion
engines, and more particularly to a statically and dynamically
balanced engine of this type which incorporates a multi-lobed rotor
concentrically mounted within the circular chamber of a stator.
The rotary internal combustion engine, often referred to as the
"Wankel" engine after the name of its inventor, is far simpler in
construction than the reciprocating piston engine, which currently
dominates the automotive field. In the Wankel engine, the
triangular rotor carries out essentially the same function as the
piston in a reciprocating internal combustion engine; that is to
say, the rotor acts to draw in a fresh air-gasoline mixture, to
compress the mixture, and after ignition thereof, to capture the
force of the expanding gases, the rotor finally serving to sweep
the exhausted gases out of the engine housing.
The rotor of a Wankel engine operates within a chamber that is the
functional equivalent of the cylinder in a reciprocating engine.
This chamber or housing has an epitrochoid shape dictated by the
motion of the rotor as it revolves about an eccentric on a rotating
main shaft. The eccentric movement is constituted by a gear
rotating about an off-center axis, causing the rotor to travel with
a non-uniform or wobbling motion. Equivalent motion in some engines
is obtained by a cam and roller or by a linkage mechanism.
In the Wankel engine, no valves exist to admit a mixture of
gasoline and air, or to discharge combustion products. To carry out
these functions, the engine is provided with two ports that open
directly into the stator chamber, the air-gas mixture entering the
chamber through one port and the exhaust gases leaving through the
other. These ports are effectively closed only when the moving
rotor passes over them to block the flow of the incoming mixture or
the outgoing spent gases. The three apexes of the triangular rotor
engage the internal wall of the stator chamber and thereby divide
the interior of the chamber into three distinct zones. As the rotor
revolves in an eccentric path within the stator, the respective
dimensions of the three zones undergo constant change.
In the course of an operating cycle of the Wankel engine, a fresh
air-gas charge is drawn in and compressed in the first zone, a
previous charge is ignited in the second zone and expanded therein
to provide thrust, and a still earlier charge--having previously
been ignited and expanded--is purged from the third zone.
As compared to a conventional reciprocating piston engine,
relatively little energy is wasted in a Wankel engine, for while
the piston must come to a complete halt every time it reverses
direction, the rotor of a Wankel engine is never arrested and
functions continuously to convert the force of the expanding gas
into a torque that is applied directly to the main shaft. The
reciprocating piston, on the other hand, requires a connecting rod
and a crank to transfer its motion into a rotational force.
Moreover, with a Wankel engine, one full turn of the triangular
rotor results in the application of three power impulses to the
main shaft, whereas in a reciprocating engine, one full operating
cycle of four strokes yields but a single power stroke.
Yet despite the generally recognized fact that the Wankel engine is
lighter and far more compact than a reciprocating engine of
equivalent horsepower and is mechanically much less complex and
less costly, it has heretofore failed to replace the reciprocating
engine to any significant degree. Though Wankel engines are now
used to a limited extent in some power tools, in lawn mowers and in
minor industrial applications, they have by no means supplanted the
reciprocating piston engine in vehicular applications, for in this
major commercial field the internal combustion piston engine is
still dominant throughout the world.
The main reason why the Wankel engine has not received widespread
acceptance despite its low cost and other significant advantages,
lies in its inherent lack of balance. Because of its eccentric
mounting, the wobbling motion of the rotor gives rise to
energy-dissipating forces which not only materially impair the
efficiency of the engine, but also produce objectionable vibration
and noise at levels that are unacceptable in a modern automobile or
other vehicle.
Moreover, because the asymmetrical Wankel engine is statically and
dynamically unbalanced, its life is relatively short, for the
wobbling action of the rotor quickly degrades and wears out the
engine parts particularly those made of standard materials.
It is for these reasons that expensive wearing surfaces using
exotic metals have, in recent years, been introduced in Wankel
engines, but these materials offer no solution to the deficiencies
inherent in the standard design of a Wankel-type engine.
SUMMARY OF THE INVENTION
In view of the foregoing, it is the main object of this invention
to provide a rotary internal combustion engine that obviates the
drawbacks of existing Wankel-type engines, and which operates with
an exceptionally high degree of efficiency.
More particularly, it is an object of this invention to provide a
rotary engine of the above-noted type, the engine being
characterized by a multi-lobed rotor concentrically mounted within
the circular chamber of a stator whereby the rotor and stator of
the motor and the forces generating internal combustion, are in
balanced relation, the motor being substantially free of vibration,
noise, and other objectionable factors.
Also an object of the invention is to provide a
concentrically-mounted rotor for a rotary combustion engine, the
rotor in one embodiment having two pairs of diametrically-opposed
lobes adapted to produce four opposed pairs of power pulses per
revolution, this being equivalent in power output to a
sixteen-cylinder, four-stroke conventional reciprocating piston
engine. In another embodiment of the invention, the rotor may
include but a single pair of lobes, in which event two opposed
pairs of power strokes are produced per revolution, equivalent to
that obtainable with a conventional eight-cylinder reciprocating
engine. In practice, more than two pairs of lobes may be included
in the engine for exceptionally high power outputs.
Another significant advantage of the invention is that it is even
simpler mechanically than a Wankel engine, for it dispenses with
the usual eccentric gearing. Not only is an engine according to the
invention less costly than a Wankel-type engine of equivalent
horsepower, but it also has a longer life, for with concentric
rotary motion and the attendant freedom from imbalance,
considerably less wear is experienced.
Briefly stated, these objects are attained in a rotary combustion
engine in which a rotor is concentrically mounted within a stator
having a perfectly circular chamber, the rotor being formed with at
least one pair of opposing lobes which engage the inner wall of the
chamber to define concave zones in the spacing between the lobes.
Formed in each lobe at the crest thereof, is a small cavity.
The stator is provided with two sets of intake and exhaust ports
associated with first and second gas-separating vanes which are
mounted at diametrically-opposed positions on the stator, and which
are spring-biased or otherwise controlled to continuously engage
the rotor surface. These vanes serve to separate the fresh air-gas
mixture fed into the intake port and the spent gases discharged
through the exhaust port in the port-set related thereto.
Formed on the inner wall of the stator are first and second
diametrically-opposed combustion cavities whose common axis is at
right angles to the axis passing through the gas separation vanes,
an igniter being placed in each cavity.
Mounted adjacent the incoming side of each combustion cavity (with
respect to the direction of rotor movement) is a spring-biased
closure vane which continuously engages the surface of the rotor.
Mounted adjacent the departing side of each combustion cavity is a
spring-biased sealing vane whose maximum extension is limited so
that it only engages the rotor surface when it lies in close
proximity to the stator wall, the sealing vane otherwise being
spaced from the rotor surface.
In the course of each revolution of the rotor, as each lobe
approaches the first gas-separation vane, the air-gas mixture from
the related intake port is admitted into the zone in front of the
lobe. As the lobe moves toward the first combustion cavity, it acts
to compress the gas in the front zone against the closure vane
related to the first combustion cavity, until a point is reached at
which the lobe cavity lies in registration with the first
combustion cavity. At this point, ignition of the compressed gas
mixture confined between the closure and sealing vanes in the lobe
and combustion cavities, takes place.
As lobe movement continues, the sealing vane associated with the
first combustion chamber loses contact with the rotor surface to
permit expansion of the exploded mixture, and as the lobe moves
toward the second gas-separation vane, the spent gases from the
previous ignition are forced out of the exhaust port associated
with the second vane. The lobe then occupies a position in line
with the second vane, at which point the above-described sequence
of actions is repeated with respect to the intake of the mixture,
the compression thereof, and ignition at the second combustion
cavity, followed by gas exhaust and the return of the lobe to its
initial position at the first gas-separation vane.
OUTLINE OF THE DRAWING
For a better understanding of the invention as well as other
objects and further features thereof, reference is made to the
following detailed description to be read in conjunction with the
accompanying drawings, wherein:
FIG. 1 is a longitudinal section taken through a preferred
embodiment of a four-lobe rotary combustion engine in accordance
with the invention;
FIG. 2 is a transverse section taken through line 2-2 in FIG.
1;
FIG. 3 is a separate view of the four-lobe rotor included in the
engine shown in FIG. 1;
FIG. 4 is a detail of one of the lobes of the rotor shown in FIG.
3;
FIG. 5 is a simplified showing of the engine to illustrate the
manner in which it operates in the course of an operating cycle,
the engine position being that occupied in Phase I;
FIG. 6 shows the same engine in Phase II;
FIG. 7 shows the same engine in Phase III;
FIG. 8 shows the same engine in Phase IV; and
FIG. 9 schematically illustrates two-lobe rotary combustion engine
according to the invention.
DESCRIPTION OF THE INVENTION
Referring now to FIGS. 1 to 4, there is shown a preferred
embodiment of a balanced rotary internal combustion engine in
accordance with the invention. The main components of the engine
are a rotor, generally designated by numeral 10, and a stator,
designated by numeral 11.
Rotor 10, also shown separately in FIG. 3, is constituted by a
cylinder whose outer surface is profiled to define four
symmetrically-arranged lobes 1, 2, 3 and 4, whose principal radial
axes are displaced ninety degrees from each other. At the crest of
each lobe is a small cavity C.sub.1, C.sub.2, C.sub.3 and C.sub.4,
respectively, as well as a spring-biased sealing vane V.sub.1,
V.sub.2, V.sub.3 and V.sub.4. The springs are adapted to urge these
vanes outwardly to continuously engage the circular inner wall of
the stator 11.
Inasmuch as the rotor, in the example shown is arranged to rotate
in the clockwise direction, the front of each lobe shall be
referred to as the "leading edge", and the rear thereof, as the
"trailing edge." The zone or recess in advance of a moving lobe
shall be referred to as the "front zone," and the zone behind a
moving lobe, as the "rear zone." Since the sealing vanes V.sub.1 to
V.sub.4 on the lobes are located adjacent the trailing edges
thereof, in the course of movement each lobe cavity (C.sub.1 to
C.sub.4) appears before its associated sealing vane, is seen from
any station along the stator.
Rotor 10 is concentrically mounted within stator 11, which is
formed to define a perfectly circular cylindrical main chamber
enclosed by end plates 12 and 13. The stator is provided with
bearings for supporting the main shaft 14 on which rotor 10 is
keyed. The stator, which also constitutes the housing of the
engine, includes annular side seals for the rotor, as well as a
mounting flange 15.
Stator 10 is effectively split into two like operating sections by
first and second gas-separating vanes B.sub.1 and B.sub.2. By means
of springs 16, or other means, which may be hydraulic or pneumatic
in nature, gas-separating vanes B.sub.1 and B.sub.2 are urged into
continuous engagement with the surface of rotor 10.
Gas-separating vanes B.sub.1 and B.sub.2 are installed at
diametrically-opposed positions 90.degree. and 270.degree. on the
stator), the vanes shifting in and out in the radial direction in
guide and support slots formed in the end housings of the stator to
accommodate the varying contours of the rotor surface. Thus at no
time do the gas-separating vanes permit fluids in one sections of
the main chamber of the stator to enter the other section
thereof.
Each gas-separating vane is associated with a set of ports. The
first set is constituted by a fresh air-gas mixture intake port
IP.sub.1 disposed below vane B.sub.1, and an exhaust port, EP.sub.1
disposed above the vane. The second set is reversely related to the
first set, and is provided with fresh air-gas mixture intake port
IP.sub.2, disposed above vane B.sub.2, and an exhaust port EP.sub.2
placed below the vane. Thus any lobe of the rotor traveling
clockwise first encounters exhaust port EP.sub.1, then vane
B.sub.1, followed by intake port IP.sub.1, after which it meets
exhaust port EP.sub.2, then vane B.sub.2, followed by intake port
IP.sub.2.
Formed in stator 10 are first and second combustion cavities
CC.sub.1 and CC.sub.2 disposed at diametrically-opposed positions
on a common axis lying at right angles to the axis common to
gas-separating vanes B.sub.1 and B.sub.2. Thus combustion cavity
CC.sub.1 is situated at 180.degree. and cavity CC.sub.2 at
0.degree. or 360.degree.. Placed within these cavities are spark
plugs 17 and 18, which, when energized, serve to explode the charge
therein.
Near the incoming side of combustion cavity CC.sub.1 (assuming
clockwise movement), is a closure vane A.sub.1, and similarly
placed with respect to combustion chamber CC.sub.2 is a closure
vane A.sub.2. Both closure vanes A.sub.1 and A.sub.2 are
spring-biased or otherwise operated to act in the same manner as
gas-separating vanes B.sub.1 and B.sub.2, so that the closure vanes
always remain in contact with the face of rotor 10 to continuously
seal the recesses or zones defined on either side thereof.
Near the departing sides of combustion cavities CC.sub.1 and
CC.sub.2 (again assuming clockwise movement), are special sealing
vanes S.sub.1 and S.sub.2 which, though also spring-biased, are
provided with end stops serving to limit the maximum extension of
the vanes. The stop positions are such as to cause special sealing
vanes S.sub.1 and S.sub.2 to close the recesses associated
therewith only during a short portion of the operating cycle,
rather than continuously, as in the case of vanes A.sub.1 and
A.sub.2.
In other words, special sealing vanes S.sub.1 and S.sub.2 are only
able to engage the rotor surface when the depth of the recesses
between successive lobes on the rotor is relatively shallow, these
vanes otherwise being unable to reach the rotor surface. This
part-time sealing action of vanes S.sub.1 and S.sub.2 is an
important aspect of the invention, and will be analyzed later in
greater detail.
We shall now consider the operation of the engine in the course of
a single rotor turn. Intake ports IP.sub.1 and IP.sub.2 are both
coupled to a suitable carburetor supplying a proper mixture of
gasoline and fresh air. (Alternatively, air alone may be supplied
to the intakes, in which event timed fuel injection takes place at
combustion cavities CC.sub.1 and CC.sub.2 through fuel injection
duct FI, as shown in FIG. 2.
PHASE I.
As shown in FIG. 5, in this phase, lobes 1 and 3 are aligned at
0.degree. and 180.degree. with combustion cavities CC.sub.2 and
CC.sub.1, the lobe cavities C.sub.1 and C.sub.3 lying in
registration with the combustion cavities. Lobes 2 and 4 are in
line at 90.degree. and 270.degree. respectively with gas-separating
vanes B.sub.1 and B.sub.2.
In phase I, the charge confined within the combustion cavities by
vanes A.sub.1 - S.sub.1 and A.sub.2 - S.sub.2, has just been
ignited, and lobes 1 and 3 are moving clockwise to begin exhausting
through exhaust ports EP.sub.1 and EP.sub.2, respectively.
Lobes 2 and 4 in phase I, as shown in FIG. 5, are at the end of
induction, in line with vanes B.sub.1 and B.sub.2, and now, as the
lobes move clockwise, proceed to compress the fresh fuel mixture
introduced through intake ports IP.sub.1 and IP.sub.2, in
preparation for ignition.
Let us consider what happens in the clockwise direction, just
before lobes 2 and 4 reach vanes B.sub.1 and B.sub.2. For this
purpose, let us position lobes 2 and 4 so that they block exhaust
ports EP.sub.1 and EP.sub.2, in which position EP.sub.1 and
EP.sub.2 are both open to supply the gas-air mixture into the space
between the leading edge of lobe 2 and the trailing edge of lobe 3,
and into the space between the leading edge of lobe 4 and the
trailing edge of lobe 1. The volume of these spaces increases as
lobes 2 and 4 advance toward intake ports IP.sub.1 and IP.sub.2,
respectively. This increasing volume creates induction of the
mixture, the end of the induction period being shown in FIG. 5.
PHASE II.
As shown in FIG. 6, lobes 1 and 3, which are positioned at about
10.degree. and 190.degree., are at the beginning of power expansion
at their trailing edges, and at the start of their exhaust at their
leading edges. Lobes 2 and 4, which have just passed vanes B.sub.1
and Bhd 2, are proceeding to block intake ports IP.sub.1 and
IP.sub.2, just prior to compression.
It will be seen in this Figure that gas-separating vane B.sub.1
provides a barrier between the spent gases beginning to exhaust
from the zone behind lobe 2 engaged by vane B.sub.1, and the zone
in front thereof, which is being supplied by a fresh charge through
IP.sub.1. Similarly, vane B.sub.2 is carrying out the same function
with regard to the zone behind lobe 4, which is discharging into
port EP.sub.2, and the zone in front of lobe 4, which is being
supplied by a fresh charge through IP.sub.2.
PHASE III.
As shown in FIG. 7, in phase III, lobes 1 and 3 continue their
power expansion at their trailing edges. In this phase, lobes 1 and
3 are about 30.degree. beyond 0.degree. and 180.degree. (dead
center of the ignition points), hence sealing vanes S.sub.2 and
S.sub.1 fall short of the receding surface of the rotor, so that
expansion of the power stroke can continue with increasing volume
of the space between closure vanes A.sub.2 and A.sub.1, and the
trailing edges of lobes 1 and 2. As lobes 1 and 3 move toward
exhaust ports EP.sub.1 and EP.sub.2, their leading edges force the
spent combustion products toward these ports.
Lobes 2 and 4 in phase III, having moved beyond intake ports
IP.sub.1 and IP.sub.2, proceed to compress the fresh air-gas
mixture in the zone in advance of their leading edges against
closure vanes A.sub.1 and A.sub.2, while a new charge is being
drawn from the intake ports in the zone behind the trailing
edges.
PHASE IV.
As shown in FIG. 8, lobes 1 and 3 are coming to the end of power
expansion at their trailing edges before exhaust takes place
through exhaust ports EP.sub.1 and EP.sub.2. The leading edges of
lobes 1 and 3 are finishing their exhaust of the previously
exploded charge through exhaust ports EP.sub.1 and EP.sub.2.
At the same time, the trailing edges of lobes 2 and 4 are
completing their fresh charge intake through intake ports IP.sub.1
and IP.sub.2, while their leading edges are carrying the compressed
mixture contained in lobe cavities C.sub.2 and C.sub.4 into
combustion cavities CC.sub.1 and CC.sub.2, where it is held for
ignition between sealing and closure vanes S.sub.1 - A.sub.1, and
S.sub.2 - A.sub.2, at which point we are back at phase I to repeat
the operating cycle.
Thus, in the course of each revolution of the rotor lobe 1, it
encounters two ignition stations to produce two power impulses.
Lobe 3, which is diametrically opposed to lobe 1, concurrently goes
through the same operating sequence, for when lobe 1 is in line
with combustion cavity CC.sub.1, lobe 3 is in line with combustion
cavity CC.sub.2, whereby the forces produced by simultaneous
ignition in these cavities are equal and opposite. A similar
relationship exists as between lobes 2 and 4, and the combustion
cavities.
Power is therefore applied simultaneously to the rotor at two
exactly opposed points, effectively providing inherent dynamic
balance. Similarly, induction pressures as well as exhaust and
compression pressures are always equal and opposite in the course
of rotor movement, resulting in a balanced performance.
Since the simultaneous action of lobe twins 1 and 3 is followed by
the simultaneous action of lobe twins 2 and 4, a pair of drive
impulses is generated every 90.degree. per revolution, or four
double impulses per revolution. This rotary-engine arrangement is
equivalent in power output to a sixteen-cylinder, four-stroke
conventional reciprocating-piston internal combustion engine. In
practice, the rotary engines of the type disclosed herein may be
arranged in tandem relationship to produce exceptionally high
horsepower ratings in a relatively confined space. The cooling
systems may be of the type presently used with Wankel engines.
The cooperative actions of closure valves A.sub.1 and A.sub.2 with
gas-separating vanes B.sub.1 and B.sub.2, give rise to induction,
compression and exhaust. The action of sealing vanes S.sub.1 and
S.sub.2 in first sealing the combustion zone and then allowing
expansion of power against the trailing edges of the lobes, in
effect transfers the compressed charge from the leading edge to the
trailing edge of the lobe during the combustion period.
Referring now to FIG. 9, there is shown a rotary engine in
accordance with the invention, which employs a rotor 20 having only
one pair of opposed lobes 1 and 3, the rotor profile otherwise
being circular. Rotor 20 cooperates with a stator 21 which is
essentially the same as stator 11, and includes opposed
gas-separating vanes B.sub.1 and B.sub.2, associated with two sets
of reversely related intake and exhaust ports IP.sub.1 - EP.sub.1,
and IP.sub.2 - EP.sub.2, as well as closure and sealing vanes
A.sub.1 - S.sub.1, A.sub.2 - S.sub.2.
For very small engines having a two-lobed rotor, all that is
necessary is one set of ports, one separating vane and one set of
compression and combustion vanes which provide maximum power at
slow speeds.
The operation of the two-lobe engine is such as to produce
simultaneous power pulses in combustion cavities CC.sub.1 and
CC.sub.2, which are diametrically opposed. Two double power pulses
are produced per revolution, this being equivalent to a
four-stroke, eight-cylinder reciprocating-piston engine.
One may also provide a rotor with three lobes, which are displaced
120.degree. from each other, in combination with only one pair of
compression-ignition and intake-exhaust closure vanes. This may be
arranged to fire alternately, top and bottom, every 60.degree., or
six alternate power pulses per revolution, this being equivalent to
a twelve-cylinder, four-stroke engine.
While there have been shown and described preferred embodiments of
balanced rotary combustion engine in accordance with the invention,
it will be appreciated that many changes and modifications may be
made therein without, however, departing from the essential spirit
of the invention.
* * * * *