Information
-
Patent Grant
-
6534987
-
Patent Number
6,534,987
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Date Filed
Thursday, March 1, 200123 years ago
-
Date Issued
Tuesday, March 18, 200321 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 324 389
- 324 380
- 324 378
- 324 381
- 324 385
- 324 388
- 324 398
- 123 599
- 123 651
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International Classifications
-
Abstract
A magneto-system firing apparatus which is capable of rapidly detecting an abnormal state in the case where abnormality occurs in the make/break operation of a contact point due to damage of a breaker or the like. A magneto-system firing apparatus includes a magnet fixed to a rotary shaft that interlocks with a crank shaft of an engine; a primary coil to which a low-voltage current that is generated due to the rotation of the magnet is supplied; a breaker which is connected to the primary coil and interrupts the low-voltage current supplied to the primary coil by its break operation; a secondary coil in which a predetermined voltage is induced due to the current interruption caused by the break operation of the breaker to actuate the firing apparatus by application of the voltage generated in the secondary coil; a crank angle detecting portion for detecting the rotating angle of the crank shaft; a breaker make/break state detecting portion for detecting the make/break state of the breaker; and a breaker failure detecting device having a breaker make/break abnormality detecting portion which is capable of detecting the abnormal state of the breaker make/break operation on the basis of information from the crank angle detecting portion and the breaker make/break state detecting portion.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a magneto-system firing apparatus, and more particularly to a magneto-system firing apparatus mounted on an aircraft and having a breaker failure detecting portion which is capable of detecting an abnormal state of the make/break operation of the breaker.
2. Description of the Related Art
In general, a battery type firing apparatus is applied to an engine for an automobile, but a self-generatable magneto-system firing apparatus is used in the aircraft from the viewpoint of safety.
As shown in
FIG. 8
, the magneto-system firing apparatus of this type includes a permanent magnet
11
disposed on a rotary shaft
10
that interlocks with a crank shaft of an engine, a primary coil
13
that forms an ignition coil wound around an iron core
12
which is so disposed as to surround the permanent magnet
11
, a secondary coil
14
larger in turn ratio than the primary coil
13
, a cam mechanism
15
connected to the primary coil
13
and disposed on the rotary shaft
10
, and a mechanical breaker
18
which is driven by the cam mechanism
15
, and makes intermittent a current generated in the primary coil
13
due to the make/break operation of a contact point
17
which is abutted against the surface of the cam
16
or spaced apart from the cam
16
.
In the magneto-system firing apparatus
19
of this type, in the case where a low-voltage current is generated as an inductance current in the primary coil
13
due to the rotation of the permanent magnet
11
interlocked with the rotation of the crank shaft, the breaker
18
is driven by the cam mechanism
15
so as to be actuated so that the contact point
17
is opened, and the low-voltage current in the primary coil
13
is broken, as a result of which a high-voltage current is induced in the secondary coil
14
, and the high voltage is applied to spark plugs (not shown) disposed in the respective cylinders through a distributor
20
to cause spark discharge at spark gaps and fire an air-fuel mixture in the cylinders, thereby driving pistons. In the figure, reference numeral
21
denotes a capacitor and
22
is a spark plug.
In the breaker
18
thus structured, since the above contact point
17
is repeatedly physically abutted against and spaced apart from the surface of the cam
16
to make and break the current that flows in the primary coil
13
, there is a possibility that the contact point
17
is burned and damaged while it is used. In the case where the contact point
17
is thus burned and damaged, even if the crank reaches a predetermined rotating angle at a spark timing, the breaker
18
does not appropriately conduct the make/break operation, so that the current in the primary coil
13
is not broken, with the results that because the high-voltage current is not induced in the secondary coil
14
, there is a case in which the spark discharge does not occur in the spark plug, and the air-fuel mixture within the cylinder is not fired.
In order to prevent the above situation, in an engine for an aircraft, there is formed a so-called dual ignition system having two magneto-system firing apparatuses
19
for each of the piston cylinders from the viewpoint of safety. A pilot is under an obligation to conduct the stop operation with respect to the two magneto-system firing apparatuses
19
mounted on the respective cylinders, to confirm that the number of revolutions of an engine is lowered a certain degree, and to confirm whether or not the respective magneto-system firing apparatuses
19
are normally actuated, before every time the aircraft takes off. The above confirming operation must be conducted every time before flying which is troublesome.
Also, at the time of inspections on the ground, the operation of inspecting the breakers is periodically conducted every several tens hours, and in the case where the contact point
17
is burned and damaged, it is necessary to replace the breaker
18
with a new one. Thus, the inspecting and maintaining operation is also complicated. Under the above circumstances, up to now, it is desirable to provide a means for detecting the burning damage and deterioration of the breaker
18
of the magneto-system firing apparatus
19
at a real time.
However, it is difficult to provide the means for detecting the abnormal operation of the breaker
18
for the following reasons.
In order to judge whether or not the contact point
17
of the breaker
18
is normally actuated, there is proposed, for example, a manner in which a circuit that can detect the resistance value of the breaker
18
is disposed in the breaker
18
, and the respective resistance values at the make/break time of the contact point
17
are measured, and whether or not the contact point
17
is appropriately made and broken, is judged on the basis of a change in the resistance value.
In this case, the primary coil
13
of the ignition coil is connected in parallel with the breaker
18
, and the impedance of the primary coil
13
is about 0.65 to 0.7 Ω. Since the breaker
18
is influenced by the impedance when the breaker
18
is made, the resistance value detected on the breaker
18
when the breaker
18
is broken becomes about 0.65 to 0.7 Ω, likewise.
On the other hand, when the breaker
18
is made, the resistance value of the breaker
18
is 0 Ω, but since a difference in the resistance between the make and break states is slight, it is difficult to distinguish the make state from the break state, and to judge whether or not the make/break operation is appropriately conducted.
Also, as described above, when the breaker
18
is broken, the low-voltage current in the primary coil
13
is interrupted with the result that a large serge voltage is generated in the secondary coil
14
. Therefore, in the case where a detecting circuit and an electronic parts for detection are connected to the breaker
18
, since the detecting circuit and the electronic parts cannot withstand the serve voltage, it is difficult to connect the detecting circuit and the electronic parts for detection to the breaker
18
.
SUMMARY OF THE INVENTION
An object of the present invention is to provide a magneto-system firing apparatus which is capable of detecting an abnormal state rapidly in the case where the breaker is damaged or the like, and there occurs abnormality in the make/break operation of the contact point.
Also, another object of the present invention is to provide a magneto-system firing apparatus that detects the abnormality of the make/break operation on the basis of information related to an angle of a crank shaft of an engine and information related to the make/break operation of the breaker.
In order to achieve the above objects, there is provided a magneto-system firing apparatus, comprising: a magnet fixed to a rotary shaft that interlocks with a crank shaft of an engine; a primary coil to which a low-voltage current that is generated due to the rotation of the magnet is supplied; a breaker which is connected to the primary coil and interrupts the low-voltage current supplied to the primary coil by its break operation; a secondary coil in which a predetermined voltage is induced due to the current interruption caused by the break operation of the breaker to actuate the firing apparatus by application of the voltage generated in the secondary coil; a crank angle detecting portion for detecting the rotating angle of the crank shaft; a breaker make/break state detecting portion for detecting the make/break state of the breaker; and a breaker failure detecting device having a breaker make/break abnormality detecting portion which is capable of detecting the abnormal state of the breaker make/break operation on the basis of information from the crank angle detecting portion and the breaker make/break state detecting portion.
Accordingly, in the present invention, the breaker make/break abnormality detecting portion conducts judgment on the basis of information related to the crank angle outputted from the crank angle detecting portion and information related to the breaker make/break state outputted from the breaker make/break state detecting portion and detects the abnormal state in a case the breaker make/break state is abnormal. As a result, if abnormality occurs in the make/break state of the breaker, the abnormality can be rapidly recognized.
Accordingly, in the case where the magneto-system firing apparatus according to the present invention is employed in an aircraft, if abnormality occurs in the make/break state of the breaker, a pilot can recognize the abnormal state. As a result, since the pilot can recognize the abnormal state of the breaker at a real time, although it is necessary to periodically conduct the inspecting operation of the breaker every 20 hours at the time of inspection on the ground up to now, it is unnecessary to always periodically conduct the inspecting operation in a short period, and the period of the inspecting operation can be lengthened, and the number of times of complicated inspecting operation can be lessened.
Also, according to a second aspect of the present invention, abridge circuit is connected between the primary coil and the breaker, and the breaker is connected with the breaker failure detecting device through a serge voltage preventing means for preventing a serge voltage generated in the primary coil. Also, the crank angle detecting portion includes a magnetic portion disposed on the rotary shaft, a sensor that detects the magnetic portion, and a crank angle detecting means for outputting an electric signal resulting from detecting the magnetic portion by the sensor as an electric signal that represents the rotating angle of the crank. The breaker make/break state detecting portion is so structured as to output the make/break state of the breaker as an electric signal, and the breaker make/break abnormality detecting portion is so structured as to output a predetermined electric signal on the basis of the electric signals outputted from the crank angle detecting portion and the breaker make/break state detecting portion if the make/break operation of the breaker is abnormal.
Accordingly, in the second aspect of the present invention, since the bridge circuit is connected between the primary coil and the breaker, an influence of the impedance of the primary coil to the beaker can be removed. Therefore, since the resistance of the breaker becomes 0 Ω when the breaker is made and infinite when the breaker is broken, the make/break state of the breaker can be readily detected.
Also, since the breaker is connected with the breaker failure detecting device through the serge voltage preventing means for preventing the serge voltage generated in the secondary coil, the influence on the breaker failure detecting device can be prevented, and the abnormal state of the make/break operation of the breaker can be detected without damaging the break failure detecting device.
Also, according to a third aspect of the present invention, the crank angle detecting portion is so structured as to output an electric signal of a high level while the crank moves from a predetermined angular position before a compression top dead center to the top dead center and output an electric signal of a low level while the crank moves from the top dead center to the predetermined angular position before the top dead center, and there is further provided a waveform shaping means for waveform-shaping the electric signal of the high level into a waveform shaping signal representing the predetermined angular position before the top dead center and a waveform shaping signal representing the top dead center.
The spark plug disposed in the piston cylinder is so structured as to fire the air-fuel mixture within the piston cylinder by conducting spark discharge at the predetermined angular position of the crank before the piston reaches the top dead center. Accordingly, in the third aspect of the present invention, in order to judge whether or not the breaker is normally actuated, the electric signal of the high level corresponding to a position of the predetermined angular position before the top dead center of the crank to the top dead center is waveform-shaped and used as information of detecting the breaker make/break abnormality detection.
Further, according to a fourth aspect of the present invention, the breaker make/break abnormality detecting portion compares the waveform shaping signal outputted from the crank angle detecting portion and representing the predetermined angular position before the top dead center with a terminal portion of the electric signal outputted from the breaker make/break state detecting portion and representing the make state, and compares the electric signal outputted from the crank angle detecting portion and representing the top dead center, with the signal outputted from the breaker make/break state detecting portion and representing the break state.
Since the firing apparatus is so structured as to conduct the firing at the predetermined angular position of the top dead center (BTDC) of the crank shaft of the engine, it is necessary that the breaker is appropriately broken when the crank shaft reaches the angular position.
Accordingly, in the second, third and fourth aspects of the present invention, a slight error in the timing of the actual make/break operation of the breaker is estimated, the information of from an angular position slightly lower than the angular position of the crank shaft when firing to the top dead center (TDC) which is predetermined to the engine is grasped by the electric signal of a high level, and similarly information as to the make/break operation of the breaker is grasped by the electric signals of the high level and the low level, and those electric signals are compared with each other to detect the breaker make/break abnormality.
Accordingly, the breaker make/break abnormality detecting portion compares the electric signal representing the predetermined angular position before the top dead center outputted from the crank angle detecting portion, with the terminal portion of the electric signal outputted from the breaker make/break state detecting portion and representing the make state, and judges that the make operation of the breaker is appropriately conducted if the electric signal representing the make state of the breaker is inputted when the electric signal representing the predetermined angular position before the top dead center is inputted. Also, the breaker make/break abnormality detecting portion compares the electric signal outputted from the crank angle detecting portion and representing the top dead center, with the electric signal outputted from the breaker make/break state detecting portion and representing the break state, and judges that the break operation of the breaker is appropriately conducted if the electric signal representing the break state of the breaker is inputted when the electric signal representing the top dead center is inputted.
According to a fifth aspect of the present invention, the bridge circuit comprises a diode bridge circuit, and the serge voltage preventing means comprises a diode. Also, according to a sixth aspect of the present invention, the predetermined angle before the top dead center is 40 degrees. Since the engine for the aircraft is generally so structured as to fire at an angular position of 20 to 26 degrees before the top dead center, when it is judged whether or not the breaker is normally actuated, a reference position for detecting the breaker make state is provided at the angular position near 40 degrees before the top dead center which is before 20 degrees before the top dead center.
In addition, according to a seventh aspect of the present invention, the breaker make/break abnormality detecting portion comprises a flip-flop circuit.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a conceptual diagram showing a magneto-system firing apparatus in accordance with the present invention, and a diagram showing a state in which a bridge circuit is connected and disposed between an ignition coil and a breaker, and the breaker is connected with a breaker failure detecting device through a serge voltage preventing means.
FIGS. 2 and 3
are diagrams showing directions of a current that flows in a circuit in a state where the bridge circuit is disposed between the ignition coil and the breaker, in which
FIG. 2
shows a flow of the current in a plus direction and
FIG. 3
shows a flow of the current in a minus direction;
FIG. 4
is a diagram showing a breaker failure detecting device in a magneto-system firing apparatus in accordance with an embodiment of the present invention;
FIG. 5
is a diagram showing a crank angle signal detected by a crank angle detecting portion and a breaker make/break state signal detected by a breaker make/break state detecting portion corresponding to the crank angle signal, in which the crank angle signal outputs a signal of high level while a crank shaft reaches from 40 degrees before a top dead center (BTDC) to the top dead center (TDC), and the breaker make/break state signal outputs a signal of high level in a make state;
FIG. 6
is a diagram showing the structure of a breaker make/break state detecting means in accordance with an embodiment of the present invention;
FIG. 7
is a diagram showing a crank angle signal detected by a crank angle detecting portion and a breaker make/break state signal detected by a breaker make/break state detecting portion corresponding to the crank angle signal, and also a diagram showing a crank angle signal waveform shaped by a waveform shaping means and representing a crank angle signal outputting a signal of high level at 40 degrees before the top dead center (BTDC) and the top dead center (TDC), a breaker make/break state signal outputted from the breaker make/break state detecting portion and a signal resulting from inverting the breaker make/break state signal; and
FIG. 8
is a conceptual diagram showing the general structure of a magneto.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Hereinafter, a description will be predetermined in more detail of a magneto-system firing apparatus in accordance with an embodiment of the present invention with reference to the accompanying drawings.
As shown in
FIG. 1
, in a magneto-system firing apparatus
30
according to this embodiment, a magneto-system firing apparatus main body
31
is connected with a breaker failure detecting device
40
.
In this embodiment, a diode bridge circuit
35
is connected between a primary coil C
1
that constitutes an ignition coil
37
and a breaker
34
. Also, the breaker
34
is connected with a breaker failure detecting device
40
through a serge voltage preventing means
39
formed of a diode D
5
that can prevent a serge voltage generated in the primary coil C
1
. In the figure, reference numeral
38
denotes a spark plug.
The diode bridge circuit
35
is made up of diodes D
1
to D
4
which are arranged as shown in FIG.
1
. In general, since an electric power is generated by a magneto and an a.c. flows in the ignition coil
37
, in the conventional magneto, an a.c. that flows in bi-directions of the coil flows, and the a.c. flows in the breaker
34
as the bi-directional current, likewise.
However, in this embodiment, since the diode bridge circuit
35
is provided, the a.c. that flows in the ignition coil
37
is rectified and converted into a one-way current. As a result, in this embodiment, a direction of the current that flows in the breaker
34
is always kept constant.
That is, as shown in
FIGS. 2 and 3
, assuming that a direction of the current that flows upstream is a plus side and a direction of the current that flows downstream is a minus side with respect to the ignition coil
37
,
FIG. 2
shows a case where a current of the plus direction flows in the ignition coil
37
as shown in the figure, and after a current flow passes through the diode D
1
and the breaker
34
, the current flow passes through the diode D
4
and returns to the ignition coil
37
.
Also, as shown in
FIG. 3
, a current flow in the case where the current of the minus direction flows in the coil, after the current flow passes through the diode D
2
and the breaker
34
, the current flow passes through the diode D
3
and returns to the ignition coil
37
. The diodes D
1
to D
4
to be used in the diode bridge circuit
35
can withstand the serge voltage generated in the ignition coil
37
when the current that flows in the ignition coil
37
is broken by the breaker
34
.
Accordingly, in this embodiment, in detecting the failure of the breaker
34
, in the case where a resistance when the breaker
34
is made and broken is measured to detect the make/break state of the breaker
34
, because an influence of the impedance of the primary coil C
1
connected in parallel with the breaker
34
is intercepted by the diode bridge circuit
35
, the resistance is 0 Ω when the breaker is made and infinite when the breaker is broken, thereby being capable of clearly judging the make and break states of the breaker
34
.
Up to now, since the bi-directional current flows in the breaker
34
as an a.c., both contact portions at the contact point are burned and damaged. However, in this embodiment, since the diode bridge circuit
35
is provided to rectify the current into a d.c., only one contact portion is burned and damaged. Therefore, a material of the contact portion at the contact point is easily selected.
Also, as shown in
FIG. 1
, since the breaker failure detecting device
40
is connected to the breaker
34
through the serge voltage preventing means
39
, an influence of the serge voltage generated in the secondary coil C
2
on the breaker failure detecting device
40
when the breaker
34
is broken can be removed, and the breaker failure detecting device
40
is not damaged by the serge voltage or the like. As a result, the magneto-system firing apparatus
30
according to this embodiment can be connected with an electronic parts or a circuit or the like for detecting the resistance value of the breaker.
Then, as shown in
FIG. 4
, the breaker failure detecting device
40
used in the magneto-system firing apparatus
30
according to this embodiment includes a crank angle detecting portion
50
for detecting the rotating angle of the crank shaft, a breaker make/break state detecting portion
60
for detecting the make/break state of the breaker, a breaker make/break abnormality detecting portion
70
for detecting the abnormal state of the breaker make/break operation on the basis of information from the crank angle detecting portion
50
and the breaker make/break state detecting portion
60
, and a display portion
80
for displaying the abnormal state detected by the breaker make/break abnormality detecting portion
70
.
In this embodiment, the breaker failure detecting device
40
is structured by an electric circuit, but may be structured by a digital circuit using a microcomputer without any problem.
The crank angle detecting portion
50
includes a magnetic portion
51
disposed within the magneto and disposed on a rotary shaft
10
that interlocks with the crank shaft of the engine, a sensor
52
for detecting the magnetic portion
51
, a crank angle detecting means
53
that outputs an electric signal resulting from detecting the magnetic portion
51
by the sensor
52
as an electric signal representing a crank angle, and waveform shaping means
54
and
55
that shape the waveform of an electric signal outputted from the crank angle detecting means
53
.
The spark plug disposed in a cylinder conducts spark discharge at a predetermined angular position of the crank before a piston reaches a top dead center, to thereby fire an air-fuel mixture within the cylinder. Therefore, in the present invention, in order to judge whether or not the breaker
34
is normally actuated, an electric signal of high level corresponding to a position between a position of the predetermined angle before the top dead center of the crank and the top dead center is waveform-shaped and used as a basic information of detection of the breaker make/break abnormality.
As described above, in an engine for an aircraft, the spark plug is structured so as to be fired when the crank reaches a position of 20 degrees before the top dead center (TDC). Therefore, in order to decide that the firing system is appropriately actuated in the engine for the aircraft, it is necessary that in the case where the crank reaches the crank angle of 20 degrees of the top dead center (TDC), the breaker
34
is normally broken, and a high-voltage current is induced in the secondary coil. Therefore, in this embodiment, in detecting whether or not the breaker
34
is normally actuated, it is judged whether or not the breaker
34
is made at the angular position of 40 degrees of the top dead center (TDC) before 20 degrees before the top dead center, and when the crank reaches the top dead center (TDC), it is judged whether or not the breaker
34
is broken, to thereby judge the presence/absence of the make/break abnormality of the breaker
34
.
The magnetic portion
51
is formed of a pair of magnetic blades
56
,
56
on the peripheral edge portion of a rotor
55
disposed on the rotary shaft
10
, and a sensor
52
for detecting the magnetic blades
56
is disposed in the vicinity of the rotary shaft
10
. The sensor
52
may be used a general electromagnetic pickup, a magnetic resistant element, or the like.
Therefore, the rotary shaft
10
disposed within the magneto rotates in accordance with the rotation of the crank shaft, and when the sensor
52
detects the passing of the magnetic blades
56
,
56
, the sensor
52
outputs a predetermined electric signal to the crank angle detecting means
53
. The crank angle detecting means
53
has information related to a relationship between the crank angle and the number of revolutions of the rotary shaft
10
in advance, and outputs the crank angle at that time as an electric signal at a timing for each of cylinders with reference to the above information.
The rotary shaft
10
of the magneto is driven by the engine through a drive gear. For example, in case of a four-cylinder engine, the drive gear of 1:1 is used so that the number of revolutions of the engine and the number of revolutions the rotary shaft
10
of the magneto become identical with each other. As usual, the four-cylinder engine conducts firing twice when the crank shaft rotates one revolution. Accordingly, the make/break operation of the breaker is also conducted twice.
FIG. 5
shows the crank angle signal and the breaker make/break timing corresponding to the crank angle signal while the crank of the four-cylinder engine rotates one revolution in a magneto-system firing apparatus of this embodiment. As shown in
FIG. 5
, the crank angle detecting means
53
is structured so as to output the electric signal of high level while the crank moves from a position of 40 degrees before the top dead center (BTDC) to the top dead center (TDC), and output the electric signal of low level while the crank moves from the top dead center (TDC) to the position of 40 degrees before the top dead center (BTDC).
Also, after the crank angle signal representing the crank angle is outputted from the crank angle detecting portion
50
, is inputted to said waveform shaping means
54
and
55
, and waveform-shaped.
That is, as shown in
FIG. 4
, the crank angle detecting means
53
are connected to the two waveform shaping means
54
and
55
. The waveform shaping means
54
waveform-shapes the electric signal of high level representing that the crank is positioned in while the crank reaches the top dead center (TDC) from the position of 40 degrees before the top dead center (BTDC) into the electric signal representative of the position of 40 degrees before the top dead center, and the waveform shaping means
55
waveform-shapes the electric signal representing the top dead center. As a result, the waveform shaping means
54
outputs a waveform shaping signal (1) as the crank angle signal of high level corresponding to the position of the crank shaft that is 40 degrees before the top dead center (BTDC), and the waveform shaping means
55
outputs a waveform shaping signal (2) as the crank angle signal of high level corresponding to the position of the crank shaft that is the top dead center (TDC). Those waveform shaping signals (1) and (2) are inputted to the breaker make/break abnormality detecting means
71
and
72
that constitute a breaker make/break abnormality detecting portion
70
which will be described later, respectively.
As shown in
FIG. 4
, the breaker
34
is connected with a breaker state detecting means
62
that constitutes the breaker make/break state detecting portion
60
through the diode D
5
as the serge voltage preventing means. As shown in
FIG. 5
, the breaker state detecting means
62
outputs an electric signal representing the make/break state of the breaker.
FIG. 5
shows the make/break timing of the breaker
34
with reference to the crank angle, and the signal of high level is outputted in case of the make state and the signal of low level is outputted in case of the break state, responding to the breaker make/break timing respectively. In this embodiment, an example where the breaker
34
comes to the break state from the make state at 20 degrees before the top dead center (BTDC) is explained.
Subsequently, the detection of the breaker make/break state will be described in the structure where the diode bridge circuit
35
is disposed between the breaker
34
and the ignition coil
37
.
In this embodiment, the breaker make/break state detecting portion
60
has a breaker state detecting means
62
formed of a circuit, and
FIG. 6
shows an embodiment of the detecting circuit.
As shown in
FIG. 6
, the breaker state detecting means
62
is connected to the breaker
34
through the diode D
5
, and the diode D
5
is provided so as to prevent a reverse voltage for preventing the influence of the serge voltage generated in the secondary coil C
2
on the detecting circuit side when the breaker
34
conducts the make/break operation.
In addition, a control power supply VDD of the detecting circuit is connected to an anode side of the diode D
5
through a resistor R
1
, and further a cathode side of the diode D
5
is connected to one end of the breaker. Also, the other end of the breaker
34
is connected to the GND side of the control power supply within the detecting circuit.
On the other hand, the anode side of the diode D
5
is further connected to the minus side input terminal of an IC
1
which is a voltage comparator through a resistor R
2
. Also, the plus side input terminal of the IC
1
is connected to a neutral point of the variable resistor VR
1
. One end of the fixed resistor portion of the variable resistor VR
1
is connected to the control power supply VDD of the detecting circuit, and the other end of the fixed resistor portion is connected to GND of the control power supply. A capacitor C
1
is further connected to the neutral point portion of the variable resistor VR
1
so as to stabilize the set voltage at the variable resistor VR
1
portion.
The breaker make/break state detecting portion
60
thus structured operates as follows:
First, a case in which the breaker
34
is in the break state will be described. In the case where the breaker
34
is in the break state, since the detecting circuit is disconnected from the breaker
34
, no current flows into the breaker
34
from the detecting circuit, and a potential at the anode side of the diode D
5
becomes equal to the control supply voltage VDD, and a value resulting from dividing the control power supply voltage is applied to the plus side input terminal of the voltage comparator IC
1
by the variable resistor VR
1
. The voltage at the plus side input terminal becomes about ½ of the control power supply voltage. The voltage comparator IC
1
compares the potential at the plus side input terminal with the potential at the minus side input terminal, and outputs a voltage corresponding to mark [(+) or (−)] which is larger in potential. Therefore, in the case where the breaker is in the break state, because the potential at the minus side input terminal becomes VDD that is larger than VDD/
2
which is the potential at the plus side input terminal, the voltage comparator outputs the voltage of the control power supply voltage GND level. Also, in the case where the breaker
34
is in the make state, the diode D
5
is short-circuited to GND which is the control power supply voltage of the detecting circuit. As a result, the potential at the anode side of the diode D
5
becomes GND level of the control power supply voltage. In this case, strictly speaking, the potential at the anode side of the diode D
5
is higher than the GND level by the forward direction voltage drop of the diode, about 0.7 V. In
FIG. 6
, the resistor R
1
is so designed as to limit a current that flows from the control power supply when the breaker
34
becomes in the make state and is determined in accordance with a current value that breaks an oxide film on the breaker
34
.
Accordingly, in the case where the breaker
34
is in the make state, a voltage of about 0.7 V is applied to the minus side input terminal of the voltage comparator IC
1
. On the other hand, a voltage of about ½ of the control power supply voltage is applied to the plus side input terminal of the voltage comparator IC
1
. However, since a power supply of 15 V is normally used for the control power supply voltage, that value becomes about 7.5 V. Therefore, in the case where the breaker is in the make state, since the plus side input terminal side is larger in the voltage at the input terminal of the voltage comparator IC
1
than the minus side, the voltage comparator IC
1
outputs the control power supply voltage VDD.
As a result, as shown in
FIG. 5
, the breaker make/break state detecting portion
60
outputs the breaker make/break state signal of high level in the case where the breaker is in the make state by the make/break timing of the breaker
34
, and outputs the breaker make/break state signal of low level in the case where the breaker
34
is in the break state. Those breaker make/break state signals are inputted to a breaker make/break abnormality detecting means
71
and
72
which will be described later.
Subsequently, the breaker make/break abnormality detecting portion
70
will be described. The breaker make/break abnormality detecting portion
70
comprises two breaker make/break abnormality detecting means
71
and
72
, OR circuits
73
and
74
connected to the respective breaker make/break abnormality detecting means
71
and
72
, and an inverter circuit
75
for inverting the breaker make/break state detecting signal outputted from the breaker make/break state detecting portion
60
.
In this embodiment, the above two breaker make/break abnormality detecting means
71
and
72
are made up of a flip-flop circuit, respectively. The breaker make/break abnormality detecting means
71
detects the abnormality of the breaker
34
in the make state, and the breaker make/break abnormality detecting means
72
detects the abnormality of the breaker
34
in the break state.
As shown in
FIG. 4
, the SET terminal of the breaker make/break abnormality detecting means
71
that detects the abnormality when the breaker is in the make state is connected to one waveform shaping means
54
that constitutes the crank angle detecting portion
50
, and the RESET terminal of the breaker make/break abnormality detecting means
71
is connected to one OR circuit
73
.
On the other hand, the SET terminal of the breaker make/break abnormality detecting means
72
that detects the abnormality when the breaker is in the break state is connected to the other waveform shaping means
55
that constitutes the crank angle detecting portion
50
, and the RESET terminal of the breaker make/break abnormality detecting means
72
is connected to the other OR circuit
74
.
The above OR circuits
73
and
74
are connected to the breaker make/break state detecting means
62
that constitutes the breaker make/break state detecting portion
60
. In this case, one input terminal of the other OR circuit
74
is connected with an inverter circuit
75
. As shown in
FIG. 7
, the inverter circuit
75
is used to partially invert a breaker make/break state detection signal outputted from the breaker make/break state detecting portion
60
.
That is, in order that the electric signal corresponding to before the top dead center (BTDC) outputted from the waveform shaping means
55
of the crank angle detecting portion
50
and the breaker make/break state detection signal are compared with each other using the flip-flop circuit to detect the make/break abnormality, the breaker make/break state signal outputted from the breaker make/break state detecting means
62
maybe used as it is. However, in order that the electric signal corresponding to the top dead center (TDC) and the breaker make/break state detection signal are compared with each other using the flip-flop circuit to detect the make/break abnormality, the breaker make/break state signal needs to be inverted.
Also, one input terminals of each of the OR circuits
73
and
74
are connected with a reset circuit
76
respectively. The reset circuit
76
is provided so as to accurately detect the state of the breaker
34
. The reset circuit
76
has a function of suspending the operation of the detecting circuit so that the detecting circuit does not malfunction in the case where the number of revolutions of the engine is equal to or smaller than a predetermined number of revolutions, and outputs a signal of high level at the time where the detecting circuit is operative and outputs a signal of low level at the time where the detecting circuit is inoperative.
Hereinafter, the operation of the breaker make/break abnormality detecting means
71
and
72
will be described.
As described above, the crank angle signal representative of 40 degrees before the top dead center (BTDC) detected by the crank angle detecting means
53
that constitutes the crank angle detecting portion
50
and is waveform-shaped by the waveform shaping means
54
is inputted to the SET terminal of the breaker make/break abnormality detecting means
71
which is a flip-flop circuit. On the other hand, the breaker make/break state signal outputted from the breaker make/break state detecting means
62
is inputted to the RESET terminal of the breaker make/break abnormality detecting means
71
through the OR circuit
73
.
The flip-flop circuit operates so as to give priority to the high level signal when a signal of high level is inputted to the RESET terminal and even if any signal is inputted to the SET terminal of the flip-flop circuit, the flip-flop circuit forcedly makes its output as low level. Also, when a signal of high level is inputted to the SET terminal after the reset terminal of the flip-flop circuit becomes low level, the flip-flop circuit retains the high level output until a signal of high level is inputted to the RESET terminal again.
In the magneto-system firing apparatus
30
according to this embodiment, as described above, the breaker
34
is structured so as to shift from the make state to the break state at 20 degrees before the top dead center (BTDC), and as shown in
FIG. 7
, in the case where the breaker
34
conducts normally the make/break operation, it is necessary that the breaker
34
becomes in the make state when the crank angle is 40 degrees before the top dead center (BTDC).
Accordingly, in the case where the breaker make state signal is inputted to the RESET side terminal of the breaker make/break abnormality detecting means
71
formed of a flip-flop circuit, and the crank angle signal is inputted to the SET terminal, the breaker make/break detecting means
71
gives priority to the input at the RESET terminal side regardless of an input to the SET terminal because the breaker make state signal which is an input of the RESET side terminal is high level, and the breaker make/break abnormality detecting means
71
outputs a signal of low level.
As a result, the breaker make/break abnormality detecting means
71
that detects the abnormality when the breaker is in the make state, outputs a signal of low level in the case where the (breaker
34
normally conducts the make operation.
On the other hand, in the case where the breaker
34
normally conducts the make/break operation, when the crank angle becomes the top dead center (TDC), firing in the plug has been already made as a result of which it is necessary that the breaker
34
becomes in the break state, and the break state of the breaker
34
is detected by the breaker make/break abnormality detecting means
72
.
In this case, since the breaker make/break state detecting means signal outputted from the breaker make/break state detecting means
62
is inputted to the breaker make/break abnormality detecting means
72
through the inverter circuit
75
as shown in
FIG. 7
, the inverted breaker make/break state signal is inverted in level as compared with the breaker make/break state signal which is not yet inverted. In the case where the breaker
34
is in the make state, the breaker make/break state signal is inputted as the low level to the breaker make/break abnormality detecting means
72
whereas in the case where the breaker
34
is in the break state, the breaker make/break state signal is inputted as the high level to the breaker make/break abnormality detecting means
72
.
Accordingly, in the case where the breaker make/break state signal is inputted to the RESET side terminal of the breaker make/break abnormality detecting means
72
formed of a flip-flop circuit, and the crank angle signal is inputted to the SET terminal, the breaker make/break detecting means
72
gives priority to the input at the RESET terminal side regardless of an input to the SET terminal when the breaker break state signal which is an input of the RESET side terminal is high level, and the breaker make/break abnormality detecting means
72
outputs a signal of low level.
As a result, the breaker make/break abnormality detecting means
72
that detects the abnormality when the breaker is in the break state, outputs a signal of low level as in the case of the detection of the make state from the breaker make/break abnormality detecting means
72
in the case where the breaker
34
normally conducts the break operation.
Subsequently, in the breaker make/break abnormality detecting means
71
and
72
, a state where the breaker
34
does not normally conducts the make/break operation will be described.
As a case where the operation of the breaker
34
is abnormal, for example, there are assumed a case where the breaker
34
is in the break state at the time the crank angle is of 40 degrees before the top dead center (BTDC), and a case where the breaker
34
is in the make state when the crank angle is positioned at the top dead center (TDC).
For example, in the case where the breaker
34
is in the break state at the time of 40 degrees before the top dead center (BTDC), the crank angle signal of low level which is in the break state is inputted to the RESET terminal of the breaker make/break abnormality detecting means
71
. A signal of high level which is a crank angle signal is inputted to the SET terminal, and since the flip-flop circuit retains the high level output until the signal of high level is inputted to the RESET terminal again, the breaker make/break abnormality detecting means
71
outputs the signal of high level.
Also, similarly, in the case where the breaker
34
is in the make state when the crank angle is positioned at the top dead center (TDC), a signal representative of the breaker make/break state which is inputted to the RESET side terminal of the breaker make/break abnormality detecting means
72
becomes a signal of low level representative of the make state which is inverted by the inverter circuit
75
. Therefore, a signal of high level is outputted from the breaker make/break abnormality detecting means
72
as in the above.
Accordingly, in the case where the abnormality of the make/break operation of the breaker is detected, the signal of high level is outputted from the breaker make/break abnormality detecting means
71
and
72
.
Then, in this embodiment, there is provided an abnormality display portion
80
that displays the abnormal state detected by the breaker make/break abnormality detecting portion
70
.
The abnormality display portion
80
comprises an OR circuit
81
connected to the breaker make/break abnormality detecting means
71
and
72
, a driver circuit
82
connected to the OR circuit
81
and a display means
83
connected to the driver circuit
82
.
Accordingly, in the case where abnormality occurs in the make/break operation of the breaker
34
, and a signal of high level is outputted from any one of the breaker make/break abnormality detecting means
71
and
72
, the signal of high level is current-amplified in the driver circuit
82
through the OR circuit
81
, and thereafter the display means
83
displays “breaker operation abnormality”. The display means
83
is appropriately disposed in a cockpit of an aircraft, as a result of which a pilot or the like can recognize the abnormality of the make/break operation of the breaker
34
of the magneto-system firing apparatus
30
in a state where he sits on a seat.
In this embodiment, the description was predetermined of an example in which the magneto-system firing apparatus of the present invention is applied to the aircraft. However, the present invention is not limited to the above embodiment, but can be applied to an engine having a magneto-system firing apparatus mounted on a machine other than the aircraft. Also, the contents disclosed in the above specification is not limited to the above embodiment as long as they are not out of the subject matter recited in the following claims.
The foregoing description of the preferred embodiments of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and modifications and variations are possible in light of the above teachings or may be acquired from practice of the invention. The embodiments were chosen and described in order to explain the principles of the invention and its practical application to enable one skilled in the art to utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto, and their equivalents.
Claims
- 1. A magneto-system firing apparatus, comprising:a magnet fixed to a rotary shaft that interlocks with a crank shaft of an engine; a primary coil to which a low-voltage current that is generated due to the rotation of said magnet is supplied; a breaker which is connected to said primary coil and interrupts the low-voltage current supplied to said primary coil by its break operation; a secondary coil in which a predetermined voltage is induced due to the current interruption caused by the break operation of said breaker to actuate the firing apparatus by application of the voltage generated in said secondary coil; a crank angle detecting portion for detecting the rotating angle of said crank shaft; a breaker make/break state detecting portion for detecting the make/break state of said breaker; and a breaker failure detecting device having a breaker make/break abnormality detecting portion which is capable of detecting the abnormal state of the breaker make/break operation on the basis of information from said crank angle detecting portion and said breaker make/break state detecting portion.
- 2. A magneto-system firing apparatus as claimed in claim 1, wherein a bridge circuit is connected and arranged between said primary coil and said breaker, and said breaker is connected with said breaker failure detecting device through a serge voltage preventing means for preventing a serge voltage generated in said primary coil;wherein said crank angle detecting portion comprises a magnetic portion disposed on said rotary shaft, a sensor that detects the magnetic portion, and a crank angle detecting means for outputting an electric signal resulting from detecting said magnetic portion by said sensor as an electric signal that represents the rotating angle of said crank; and wherein said breaker make/break state detecting portion is structured so as to output the make/break state of the breaker as an electric signal, and said breaker make/break abnormality detecting portion is structured so as to output a predetermined electric signal on the basis of the electric signals outputted from said crank angle detecting portion and said breaker make/break state detecting portion if an abnormality occurs in the make/break operation of the breaker.
- 3. A magneto-system firing apparatus as claimed in claim 2, wherein said crank angle detecting portion is structured so as to output an electric signal of a high level while said crank moves from a predetermined angular position before a compression top dead center to the top dead center and output an electric signal of a low level while said crank moves from the top dead center to the predetermined angular position before the top dead center, and there is further provided a waveform shaping means for waveform-shaping the electric signal of the high level into a waveform shaping signal representing the predetermined angular position before the top dead center and a waveform shaping signal representing the top dead center.
- 4. A magneto-system firing apparatus as claimed in claim 3, wherein the predetermined angle before the top dead center is 40 degrees.
- 5. A magneto-system firing apparatus as claimed in claim 2, wherein said breaker make/break abnormality detecting portion compares the waveform shaping signal outputted from said crank angle detecting portion and representing the predetermined angular position before the top dead center with a terminal portion of the electric signal outputted from said breaker make/break state detecting portion and representing the make state, and compares the electric signal outputted from said crank angle detecting portion and representing the top dead center with the signal outputted from said breaker make/break state detecting portion and representing the break state.
- 6. A magneto-system firing apparatus as claimed in claim 5, wherein the predetermined angle before the top dead center is 40 degrees.
- 7. A magneto-system firing apparatus as claimed in claim 5, wherein said breaker make/break abnormality detecting portion comprises a flip-flop circuit.
- 8. A magneto-system firing apparatus as claimed in claim 2, wherein said bridge circuit comprises a diode bridge circuit, and said serge voltage preventing means comprises a diode.
- 9. A magneto-system firing apparatus as claimed in claim 2, wherein said breaker make/break abnormality detecting portion comprises a flip-flop circuit.
- 10. A magneto-system firing apparatus as claimed in claim 1, wherein said breaker make/break abnormality detecting portion comprises a flip-flop circuit.
US Referenced Citations (1)
Number |
Name |
Date |
Kind |
6279558 |
Fukuda |
Aug 2001 |
B1 |
Foreign Referenced Citations (3)
Number |
Date |
Country |
A 6-307318 |
Nov 1994 |
JP |
A 10-184510 |
Jul 1998 |
JP |
A 2000-213443 |
Aug 2000 |
JP |