[0001] This invention relates to an engine, in particular a two stroke motorcycle engine.
[0002] Such an engine comprises a normal cylinder, in the chamber of which the associated
piston moves; the fuel in the form of air plus mixture, this latter comprising gasoline
and oil, reaches said cylinder chamber through feed passages. These feed passages
are known as transfer passages or induction passages according to whether the fuel
reaches said chamber from the crankcase or directly from outside the engine.
[0003] In an engine of the described type there is a requirement for facilitating burnt
gas discharge from the cylinder without causing remixing of said gas with the fuel,
by suitably directing the fuel feed into the cylinder during the known scavenging
phase. In this respect, the more the burnt gas is discharged from the cylinder without
it mixing with the fuel, the better the engine performance.
[0004] In known engines the fuel feed is suitably directed into the cylinder or rather into
its chamber by giving the feed passages a suitable fixed geometry to attain the required
object.
[0005] This method involving a fixed geometry for said passages does not allow fuel feed
into the cylinder chamber to be optimized as a function of the engine operating conditions
(rotational speed and/or degree of accelerator opening). Consequently, good engine
performance is obtained only for example for a certain engine speed or, more generally,
for particular engine operating conditions.
[0006] An object of the present invention is therefore to provide an engine of improved
performance compared with engines of the state of the art, and in particular an engine
in which mixing between the fuel (or fresh gas) and the burnt gas present in the cylinder
chamber is reduced to a minimum under any engine operating condition, ie for any rotational
speed or for any degree of opening of the accelerator.
[0007] This and further objects which will be apparent to the expert of the art are attained
by an engine, in particular a two-stroke motorcycle engine of the stated type, characterised
by comprising in at least one of the feed passages movable deflector means arranged
to vary the geometry of said passage and to orientate the fuel jet within the cylinder
chamber in such a manner as to enable said jet to urge the burnt gas towards the usual
exhaust port provided in said cylinder, said deflector means being arranged on a wall
of said feed passage in proximity to its entry into said chamber, the movement of
said deflector means and thus the variation in the geometry of said passage being
obtained as a function of the engine rotational speed and/or the the position of the
piston within said chamber of engine cycle and/or the degree of opening of the accelerator.
[0008] The present invention will be more apparent from the accompanying drawing which is
provided by way of non-limiting example and in which:
Figure 1 is a longitudinal section through a cylinder of an engine constructed in
accordance with the invention;
Figure 2 is a section on the line II-II of Figure 1; and
Figure 3 is a section on the line III-III of Figure 1.
[0009] With reference to said figures a two-stroke engine comprises a cylinder 1 having
a barrel 2 defining a chamber 3 in which a piston 4 moves.
[0010] The cylinder 1 comprises a usual burnt gas exhaust port 5 and a known induction port
6 for the fuel or fresh gas.
[0011] Feed passages 7 connected to the induction port 6 open into the chamber 3 of the
cylinder 1, said feed passages 7 being formed in the barrel 2.
[0012] The feed passages 7 can derive either from the pump sump (not shown), in which case
they are known as transfer passages, or (as in the illustrated example) from the induction
port 6 connected to the environment external to the engine, in which case they are
known as induction passages.
[0013] According to the invention, in at least one of said feed passages 7 there are provided
movable deflector means 8 arranged to modify the geometry of said passage and consequently
to throttle it. In this manner a varying orientation of the fuel (or fresh gas) jet
leaving said passage is obtained based on the position of the deflector means in said
passage.
[0014] More specifically, the deflector means 8 are at least one flexible blade 8A fixed
at one end 9, mechanically or by adhesive, to the wall 10 of the feed passages (of
only two passages 7A and 7B in the example) in a position corresponding with a seat
11 formed for example by milling.
[0015] Said blades 8A can be located either on the convex walls 10 of the passages 7 (as
shown in the example) or on the concave walls 12 of these passages, or on the lateral
walls of the passages.
[0016] These blades are provided in each passage 7 such that when in the position which
gives maximum passage opening they rest against the walls 10 of said passages or as
close to them as they can reach. In this case the free end 13 of the blades 8A is
in line with the port 14 in the wall 15 of the chamber 3 into which the passage 7
opens, but without projecting from this latter. This prevents the moving piston 4
being able to touch said end 13, with obvious resultant problems.
[0017] It will now be assumed that an engine provided with a cylinder 1 constructed in accordance
with the invention is to be used.
[0018] With the engine in operation, during the scavenging phase the fresh gas reaches the
chamber 3 of the cylinder 1 by passing through the feed passages 7. In these passages
the said gas encounters the blades 8A and is directed by them into said chamber 3
in such a manner as to prevent its mixing with the burnt gas and facilitate discharge
of the burnt gas through the exhaust port 5.
[0019] The fresh gas is therefore fed into said chamber with a certain inclination which
is a function of the position of the blades 8A in the passages 7.
[0020] Depending on the effect of the pressure in the chamber 3 and in the passages 7, and
the thrust exerted on them by the fresh gas flowing through these passages, the blades
8A can automatically assume any position between the position corresponding to maximum
passage opening (as described) and that corresponding to minimum passage opening.
These positions (or inclinations) can also vary during the scavenging phase according
to the instantaneous fresh gas flow through the passages 7. It can be generally stated
that the higher the engine rotational speed the more the blades approach the position
corresponding to maximum opening of the relative passage.
[0021] The various said positions are attained (as stated, automatically) as a function
of the engine rotational speed and/or degree of opening of the accelerator, and of
the position of the piston 4 in the cylinder chamber 3, and enable the fuel to be
directed in the best possible manner into said chamber 3. In this manner the burnt
gas present in said chamber is discharged through the port 5 without mixing (or only
to a very small extent) with the fresh gas, so enabling the engine to give high performance.
[0022] In particular, to facilitate burnt gas discharge the blades 8A are arranged in the
feed passages in such a manner as to move (and consequently direct the fresh gas)
towards the upper end of the chamber 3 of the cylinder 1 or towards its wall 15. This
further improves burnt gas discharge and prevents the fresh gas mixing with the exhaust
during fresh gas feed into the chamber 3, so further increasing engine performance.
1. An engine, in particular a two-stroke motorcycle engine comprising a cylinder containing
a chamber in which a piston moves, a fuel or fresh gas composed of air and the usual
oil-gasoline mixture reaching said chamber via feed passages, characterised by comprising
in at least one of the feed passages (7) movable deflector means (8) arranged to vary
the geometry of said passage (7) and to orientate the fuel jet within the cylinder
chamber (3) in such a manner as to enable said jet to urge the burnt gas towards the
usual exhaust port (5) provided in said cylinder (1), said deflector means (8) being
arranged on a wall (10) of said feed passage (7) in proximity to its entry (14) into
said chamber (3), the movement of said deflector means (8) and thus the variation
in the geometry of said passage (7) being obtained as a function of the engine rotational
speed and/or the the position of the piston within said chamber or engine cycle and/or
the degree of opening of the accelerator.
2. An engine as claimed in claim 1, charactherised in that the movement of the deflector
means (8) occurs automatically, said movement being caused by the pressure difference
between the cylinder chamber (3) and the feed passage (7) and the thrust exerted by
the fuel flowing through said passage (7).
3. An engine as claimed in claim 1, characterised in that the deflector means (8)
comprise at least one blade element (8A) fixed at one end (9) to a wall (10) of the
feed passage.
4. An engine as claimed in claim 3, characterised in that the blade element (8A) is
fixed to the wall (10) of the feed passage (7) advantageously mechanically or by adhesive.
5. An engine as claimed in claim 3, characterised in that the end (9) of the blade
element (8A) is positioned in a seat (11) provided in the wall (10) of the feed passage
(7).
6. An engine as claimed in claim 1, characterised in that the blade element (8A) is
arranged in the relative feed passage (7) so as to move advantageously in a different
manner according to whether said blade element (8A) is disposed in a passage close
to the exhaust port (5) or distant from it, said movement and the consequent orientation
of the fuel jet being towards the upper end of the cylinder chamber (3) or towards
the wall (15) of said chamber respectively.