U.S. patent number 3,876,942 [Application Number 05/399,317] was granted by the patent office on 1975-04-08 for emergency airplane locating transmitter.
This patent grant is currently assigned to Aero Electronics Development Co., Inc.. Invention is credited to Charles A. Koster, Wayne E. Perry.
United States Patent |
3,876,942 |
Koster , et al. |
April 8, 1975 |
Emergency airplane locating transmitter
Abstract
A bracket mounted, portable airplane emergency locating
transmitter manually or automatically actuated for transmitting
radio distress signals with voice capabilities which is
automatically actuated by a predetermined gravitational force along
the flight axis of the aircraft.
Inventors: |
Koster; Charles A. (Phoenix,
AZ), Perry; Wayne E. (Tempe, AZ) |
Assignee: |
Aero Electronics Development Co.,
Inc. (Tempe, AZ)
|
Family
ID: |
23579072 |
Appl.
No.: |
05/399,317 |
Filed: |
September 21, 1973 |
Current U.S.
Class: |
455/92; 455/98;
455/97 |
Current CPC
Class: |
H04B
1/02 (20130101); H04B 1/034 (20130101) |
Current International
Class: |
H04B
1/02 (20060101); H04B 1/034 (20060101); H04b
001/02 () |
Field of
Search: |
;325/111-115,119,105
;343/702,705 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Griffin; Robert L.
Assistant Examiner: Ng; Jin F.
Attorney, Agent or Firm: Lindsley; Warren F. B.
Claims
What is claimed is:
1. An airplane locating device comprising:
a hand-carried portable housing,
said housing comprising a rectangular configuration having a
battery compartment at one end, a transmitter compartment between
its ends and a handle at the other end,
said housing defining a display plane on its front surface adjacent
said transmitter compartment for mounting and exposing to an
operator a selector switch and a microphone jack,
a bracket for detachably fitting one face of said housing,
said bracket being fixedly attached to the airplane for holding
firmly said device,
switching means mounted in said housing for selectively connecting
a battery placed in said battery compartment with a transmitter
placed in said transmitter compartment,
said switching means comprising a selector switch and an impact
switch,
said selector switch in one position directly connecting the
battery in said battery compartment to the transmitter in said
transmitter compartment and when in another position connecting the
battery through said impact switch to the transmitter,
said impact switch upon closure under given impact forces
energizing the transmitter,
a transmitter mounted in said transmitter compartment transmitting
periodically changing audio distress signals on civilian and
military international distress frequencies,
a microphone jack mounted on said housing for transmitting by said
transmitter a voice modulated output signal,
a connector in electrical contact with the output signal of said
transmitter for attaching a radiation antenna to said housing,
and
means mounted on said housing for resetting said impact switch to
its contact open position.
2. The airplane locating device set forth in claim 1 in further
combination with:
connector means mounted on said housing for remotely controlling
the energization of said transmitter for test purposes.
3. The airplane locating device set forth in claim 1 in further
combination with:
a radiation antenna for connection to said connector for
broadcasting distress signals generated by said transmitter.
Description
BACKGROUND OF THE INVENTION
This invention pertains to apparatus manually or automatically
actuated to transmit on civilian and military international
distress frequencies of 121.5 MHZ and 243.0 MHZ distress
signals.
Heretofore, devices of the above type have failed to serve the dual
plane mounted and portable uses so that distress signals could not
be properly transmitted and clearly picked up by search parties.
The former devices also lacked durability on impact to prevent
damage to the transmitter and were complex and costly to produce,
thereby placing them outside of small plane owners' use.
SUMMARY OF THE INVENTION
In accordance with the invention claimed, an improved portable or
bracket-mounted airplane locating device is provided which has both
automatic distress tone and voice modulation capabilities and is
automatically or manually operable, depending on how the selector
switch is set.
It is, therefore, one object of this invention to provide an
improved device for locating a downed aircraft.
Another object of this invention is to provide apparatus for
identifying a plane crash site and thereby reduce the rescue
time.
A further object of this invention is to provide an immediate radio
signal on a given frequency at the moment of impact.
A still further object of this invention is to provide a downed
plane transmitter that is self-contained and may be bracket-mounted
and operated with a fixed external antennae or portably used with a
telescoping antenna, and which requires little maintenance for long
periods of time.
Further objects and advantages of the invention will become
apparent as the following description proceeds and the features of
novelty which characterize this invention will be pointed out with
particularity in the claims annexed to and forming part of this
specification.
BRIEF DESCRIPTION OF THE DRAWING
The present invention may be more readily described by reference to
the accompanying drawings, in which:
FIG. 1 is an exploded, partially broken-away perspective view of a
portable or bracket-mounted airplane locating device incorporating
the features of this invention;
FIG. 2 is a perspective view of the portable device shown in FIG. 1
with the portable telescopic antenna mounted in position;
FIG. 3 is a schematic illustration of the circuitry embodied in the
airplane locating device shown in FIG. 1;
FIG. 4 is a wiring diagram of the transmitter; and
FIG. 5 is a modification of the remote control feature shown in
FIGS. 1-4.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring more particularly to the drawings by characters of
reference, FIG. 1 discloses a downed or crashed airplane locating
device 10 comprising a housing 11 having a detachably mounted back
12 which is formed for fitting into an airplane-mounted bracket 13.
An antenna 14 is shown for being received and retained by a
connector 15 mounted on the face or front 16 of housing 11.
The housing 11, as viewed in FIG. 1, comprises a compartment 17
containing four batteries 18A-18D, a compartment 19 containing a
printed wiring board (PWB) 22 and an auxiliary compartment 23 in
which is mounted an impact switch 24. A partition 25A in back 12
and a similar partition 25B in housing 11 separates the battery
compartment 17 from compartment 19 and auxiliary compartment
23.
On the front 16 of housing 11 are mounted in addition to antenna
connector 15 a master switch 26, a microphone jack 27, a remote
control jack 28, a "power on" indicator 29, and an impact switch
reset button 30. Detachably mounted back 12 and associated neoprene
gasket 90 are normally held in position against the rear side of
housing 11 by six screws, two of which, namely screws 32 and 33,
are shown. The screws pass through clearance holes 34, 35 and 36 in
back 12 and turn into threaded holes (not shown) in the rear of
housing 11. An integral carrying handle 37 is provided at the top
of housing 11.
Airplane-mounted bracket 13 is normally secured to the frame of the
airplane and is employed to hold the airplane locating device 10 in
place. For proper operation of impact switch 24, the mounting
position for bracket 13 should be such that arrow 38 shown on face
16 of housing 11 is pointed in the direction of flight. Bracket 13
is made from a flat piece of sheet metal formed into a flat
rectangular pocket-like center section 39 for receiving and
supporting housing 11 and more particularly the rear surface of
cover 12. Its wrap-around top flange 40 formed by two right angle
bends 42 and 43 passing under handle 37 causes the tab formed by
bend 43 to fit over the top edge 45 of surface 16 of housing 11.
Side flanges 46 and 47 of mounting bracket 13 are bent to secure
the sides of housing 11 and prevent its lateral motion. A lower
flange 48 comprising a first flat surface 49 extending at a right
angle to center section 39 and a second flat surface 50 extending
laterally thereto in a plane parallel to center section 39 bears
against a lower edge 53 of back 12 and serves in cooperation with
top section 40 to prevent longitudinal motion of housing 11.
Surface 50 is a mounting surface for retainer clip 54, and when
clip 54 is placed over surface 50 of section 48, fastener 56 by
engaging with mating part 57 of fastener 56 grips lower extension
58 of housing 11 to firmly capture and retain housing 11 within
bracket 13. A plastic ring 59 loosely secures clip 54 to bracket 13
when clip 54 is not secured by fastener 56. Clip 54 is thus
prevented from being lost or misplaced when not in use.
Antenna 14, which may be of a telescopic configuration, is equipped
with a twist-lock connector 62 that mates with antenna connector 15
on housing 11. Two snap clips 63A and 63B are provided on the side
of housing 11 to hold antenna 14 when it is not in use. The clips
expand to snap over the outer cylindrical surface of the antenna to
hold it in place.
FIG. 2 shows antenna 14 mounted by means of connector 62 to housing
11 and detachably mounted back 12 in position on housing 11.
The simplified schematic of FIG. 3 shows the electrical
relationships between physical parts illustrated in FIG. 1. A
transmitter 64 is assembled on printed wiring board 22 of FIG. 1.
Other parts shown in FIG. 3 which are identified by the same
numerals in FIG. 1 are antenna connector 15, impact switch 24,
microphone jack 27, remote control jack 28, light-emitting diode
(LED) power-on indicator 29 and batteries 18A-18D. A resistor 60
connected in series with LED power-on indicator 29 limits current
through the diode when voltage is applied thereacross. Transmitter
64 delivers modulated radio-frequency signals to antenna 14 via
antenna terminal 69 when negative input terminal 65 and positive
input terminal 70 are connected to the negative and positive
terminals 71 and 72, respectively, of series-connected batteries
18A-18D. Positive terminal 72 of batteries 18A-18D is permanently
wired to transmitter terminal 70. When master switch 26 is in the
ON position, negative battery terminal 71 is connected directly
through switch 26 to transmitter terminal 65. When master switch 26
is in the OFF position, battery terminal 71 is not connected to
transmitter 65 and the transmitter does not operate. When master
switch 26 is in the AUTO position, connection between battery
terminal 71 and transmitter terminal 65 can only be made through
switch 26, and thence through impact switch 24 or remote cabin
control switch 28 to terminal 65. If either of these switches (24
or 28) is closed, the transmitter will operate. When battery
voltage is applied across terminals 65 and 70 by any of the means
described above, current will flow through resistor 70 and light
emitting diode 29, and diode 29 will emit light, indicating the
transmitter 65 is energized and should be delivering modulated
radio frequency signals to antenna 14 via terminal 69 and antenna
connector 15. For operation in the automatic mode, switch 206 is
moved to the AUTO position. Impact switch 24 will normally be open,
but the impact of a crash by the airplane will close impact switch
24 to complete the circuit between battery terminal 71 and
transmitter terminal 65, thereby initiating operation of the
transmitter. Following closure of impact switch 24, the impact
switch may be reset to the open condition by depressing reset
button 30. Impact switch 24 is of the well known type offered to
the market by Technar, Inc., and sold by them as an acceleration
sending switch. Details of this switch are shown in a copending
application filed by the same applicants as this application and
entitled "Airplane Crash Locating Device", Ser. No. 389,967 filed
Aug. 20, 1973.
When master switch 26 is in the automatic mode, the pilot of the
airplane may wish to operate the transmitter even though no crash
has occurred. He may be out of fuel and contemplating an emergency
landing in a remote area or he may wish to test the operation of
the device. A remote switch accessible from the pilot's position in
the aircraft and connected by means of an electrical cable to
remote control jack 28 may be closed by the pilot to accomplish
this purpose.
The signal delivered by transmitter 64 is automatically modulated
by a sweep frequency multivibrator. Alternatively, voice modulation
may be employed by means of a microphone connected at jack 27.
The circuit diagram for transmitter 64 as shown in FIG. 4 includes
a crystal oscillator 73, a modulator 74, an output amplifier 75, a
relaxation oscillator 76 and a stable multivibrator 77. The
transmitter is powered from batteries 18A-18D, which are connected
to positive input terminal 70 and negative terminal 65.
Crystal oscillator 73 is a transistorized version of the well known
plate tuned plate vacuum tube oscillator in which a piezoelectric
crystal serves as the series tuned circuit for the grid. In
oscillator 73, piezoelectric crystal 78 acts as a series tuned LC
circuit in the emitter base circuit of oscillator transistor
79.
Piezoelectric crystals are commonly used in oscillator circuits of
this type because of their ability to control with a great deal of
accuracy the frequency of the oscillator. When excited
electrically, the crystal tends to vibrate at its resonant
frequency, which is determined by its dimensions and other
mechanical properties. In the presence of such mechanical
vibrations, electrical signals are produced across the opposite
faces of the crystal. The equivalent electrical circuit drawn
between these two opposite crystal faces comprises a first
capacitor connected directly from one face to the other and in
parallel with the first capacitor, a series network including a
second capacitor, an inductor and a resistor. The first capacitor
represents the shunt capacitance between the two faces and its
capacitance is much greater than that of the second capacitor so
that the resonant frequency is determined almost entirely by the
second capacitor and the inductor.
In the case of the preferred embodiment of this invention, the
resonant frequency of the crystal is 121.5 Mhz. A first terminal 82
of crystal 78 is connected in parallel with resistor 95 to emitter
83 of transistor 79. Resistor 93 is the collector resistor for
transistor 79 providing a stabilized operating impedance for the
tuned collector circuit comprised of inductor 88 and capacitors 87
and 89.
Capacitors 87 and 89 and inductor 88 comprise a tuned circuit in
the collector circuit of transistor 79. This tuned circuit is
adjusted by adjusting the value of inductor 88 to set its resonant
frequency near the crystal frequency. Resistors 85 and 92 and
bypass capacitor 91 establish the operating point voltage for the
amplifier portion of the oscillator and RF ground of the base
circuit necessary for a common base configuration. The network
comprising resistors 95 and 96 and capacitor 97 sets the desired DC
and AC emitter impedance to ground. The combined resistances of
both resistors 95 and 96 constitute the DC resistance, while only
resistor 95 is effective as an Ac resistance because of the
shunting of resistor 96 by capacitor 97. Resistor 98 acts as a
power divider to adjust the R-F signal level to modulator 74 and
feed back through crystal 78 to transistor 79. Resistors 99 and 144
act as a DC divider network to appropriately adjust the DC bias of
transistor 142.
Relaxation oscillator 76 comprises an oscillator stage including
unijunction transistor 101, resistors 102, 103 and 104 and
capacitor 105, and an amplifier stage including transistor 106 and
resistors 107, 108, 109 and 110.
Unijunction transistor 101 in the oscillator stage has an emitter
111, a first base 112 and a second base 113. The impedance between
emitter 111 and base 112 is high until emitter voltage exceeds a
given fraction, typically five-tenths to seven-tenths of the
voltage impressed from base 113 to base 112. When this fraction of
the base-to-base voltage is exceeded, the impedance from emitter
111 to base 112 drops abruptly to a very low value. The term
commonly employed to identify the fraction of base-to-base voltage
at which the drop in emitter-to-base impedance occurs is "the
intrinsic standoff ratio." The very low emitter-to-base impedance
is sustained only so long as the emitter-to-base current is
sustained above the critical "valley current" (typically 1 to 10
milliamperes) for the device.
In the relaxation oscillator 76 of FIG. 4, the initial base-to-base
(113 to 112) voltage is essentially equal to the battery voltage
present at positive input terminal 70 relative to negative input
terminal 65, the latter being at ground potential. Battery voltage
in the preferred embodiment is approximately 7.2 volts. Assuming an
intrinsic standoff ratio of 0.6, capacitor 105 will be charged
exponentially by a current flowing through resistor 104 to a
voltage equal to (7.2 .times. 0.6) 4.32 volts, whereupon the
emitter-to-base impedance of unijunction transistor 101 will drop
abruptly to a very low value, allowing capacitor 105 to discharge
quite rapidly, the discharge current flowing from the upper plate
110 of capacitor 105 to emitter 111, to base 112 through resistor
103 to ground. Resistor 103 limits the discharge current. When the
discharge current falls below the valley point current of
unijunction transistor 101, the emitter-base impedance returns to
its very high level and capacitor 105 again begins to charge
exponentially as before. The discharge time interval is typically
very short compared with the charging interval and the resultant
voltage waveform across capacitor 105 is thus a sawtooth waveform
with a relatively slow and nearly linear rising portion and a
relatively steep and abrupt falling portion. The period of the
sawtooth waveform across capacitor 105 is approximately equal to
the product of the value of the resistance of resistor 104 times
the value of the capacitance of capacitor 105.
The sawtooth waveform just described is applied by means of
resistors 107 and 108 acting as a voltage divider to the base 114
of transistor 106. Transistor 106, having resistor 110 connected
between its emitter 115 and ground, reacts in the manner of a high
input impedance DC coupled amplifier in which the voltage gain is a
function of the current gain of transistor 106 and the ratio of
collector resistor 109 and emitter resistor 110. A sawtooth current
waveform thus flows in collector resistor 109 and voltage waveform
at collector 116 of transistor 106 is thus an inverted sawtooth
waveform with the characteristics of the waveform produced at the
emitter of transistor 101 and previously described.
Stable multivibrator 77 is commonly employed to produce a
rectangular wave voltage at its output terminal 117. The two
transistors alternately switch ON and OFF, the first turning ON as
the second turns OFF and then at the next switching time, the first
turning off as the second turns on. In the switching operation, the
transistor turning off is aided by the transistor turning on and
the transistor turning on is aided by the transistor turning off.
Assume, for example, that transistor 118 is initially off and
transistor 119 is initially on. The right hand terminal 121 of
capacitor 120 is held essentially at ground potential by virtue of
its connection through diode 122 and thence through saturated
transistor 119 to ground. The left hand terminal 123 of capacitor
120, by virtue of the charge remaining on capacitor 12, is still
negative with respect to ground, and is thereby sustaining
transistor 118 in its off condition by holding its base 124 at a
negative potential relative to ground. This charge on capacitor 120
and the negative potential at base 124 are steadily being reduced,
however, by a charging current flowing from collector 116 of
transistor 106 through resistor 130 into terminal 123 of capacitor
120. At this same time, capacitor 126 is being charged toward
battery voltage applied at terminal 70 of transmitter 64, the
charging current flowing through resistor 127, capacitor 126 into
base 128 of transistor 119 and from emitter 129 to ground, thereby
aiding in sustaining the on condition of transistor 119. At some
point in time, the charging current to capacitor 120 will raise the
base 124 of transistor 118 to a sufficiently positive potential
(approximately 0.6 volts) to supply a base drive current into base
124 and thereby switch transistor 118 to the on condition. As
transistor 118 turns on, its collector 131 moves quickly to a very
low potential barely above ground, and by virtue of its connection
through diode 132 it also drives the left-hand terminal 133 of
capacitor 126 to a voltage only slightly more positive than ground.
Because the right-hand terminal 134 is at this time substantially
negative with respect to the left-hand terminal 133 as the result
of the charging current that had been flowing through capacitor 126
during the previous interval, right-hand terminal 34 and hence base
128 of transistor 119 are now substantially negative with respect
to ground and transistor 119 is thereby switched to and sustained
in the off condition.
The conditions of the previous interval are not reversed such that
a charging current through resistor 135 and capacitor 120 into base
124 now holds transistor 118 in the on condition while a current
flowing from collector 116 of transistor 106 through resistor 136
into right-hand terminal 134 of capacitor 126 reduces the charge on
capacitor 126 and gradually raises the voltage at base 128 of
transistor 119 from an initially negative value toward the slightly
positive value necessary to switch transistor 119 on and thereby
initiate the succeeding interval.
It has been noted that each interval is terminated when the
charging current through resistor 130 or 136 has raised base
voltage of the off transistor 118 or 119 to a sufficiently positive
level to switch the off transistor to an on condition. This
condition will be produced relatively sooner or later, depending
upon the voltage present at collector 116 of transistor 106.
It has been shown previously that the voltage present at collector
106 is of an inverted sawtooth form beginning at an initially high
value and falling slowly toward a minimum value. During the
initially high value, the charging of capacitor 123 or 126 through
resistor 130 or 136, respectively, will occur rather rapidly and
the intervals described above relating to "on" and "off" periods of
transistors 118 and 119 will be relatively short, i.e., the
switching frequency will be relatively high. As the initially high
value of the sawtooth wave decays, the switching frequency also
decays until the sawtooth wave switches abruptly from its minimum
value and the switching frequency of the astable multivibrator
simultaneously jumps abruptly to its highest rate.
As transistors 118 and 119 of the multivibrator 77 alternately
switch from off to on in a periodic manner, the voltage present on
collector 131 of transistor 118 as well as the voltage at collector
117 of transistor 119 is a rectangular wave. During the "on"
condition of transistor 118, for example, collector 131 of
transistor 118 is essentially at ground potential, while during its
"off" condition its collector 131 is pulled up to battery voltage
by pull-up resistor 137, which is connected between collector 131
and positive battery terminal 70. Similarly, collector 117 of
transistor 119 is essentially at ground potential while transistor
119 is on and it is essentially at battery voltage during the off
period of transistor 119 by virtue of the connection of pull-up
resistor 138 between collector 117 and positive battery terminal
70. Note that diode 132 is reverse-biased when transistor 118 is
off so that collector 131 of transistor 118 is isolated from the
voltage drop appearing across resistor 127 as a result of charging
current to capacitor 126. Collector 117 of transistor 119 is
similarly isolated during the off period of transistor 119 by the
then reverse-biased diode 122.
Modulator 74 has a first input terminal 100 which receives the
121.5 Mhz output of oscillator 73, and a second input terminal 139
which receives the rectangular wave output of the multivibrator 77
as taken from collector 117 of transistor 119. Modulator 74
includes two transistors 142 and 143, five resistors, 144, 145,
146, 147 and 148, a coupling transformer 149, three capacitors 152,
153, and 154, and an output terminal 155.
In the operation of modulator 74, the signal received from
oscillator 73 at modulator input terminal 100 is transmitted to
output terminal 155 when transistor 142 is biased in its active
region, but the signal from oscillator 73 is not transmitted to
output terminal 155 when transistor 142 is biased in its off
condition. The bias condition of transistor 142 is produced by the
action of transistor 143 in response to the signal it received from
input terminal 139.
Thus, for example, assume that the instantaneous voltage at input
terminal 139 is essentially zero volts. The base of transistor 143
is held substantially at ground potential by a base voltage applied
through resistor 148 to base 156 and transistor 143 is held
substantially at ground potential by a base voltage applied through
resistor 148 to base 156 and transistor 143 is thus held "off."
Resistors 145 and 146 act as a voltage divider network connected
between positive battery input terminal 70 and ground and the
divider terminal 157 is substantially more positive with transistor
143 off than the DC value of the signal present at modulator input
terminal 100. By virtue of the connection of divider terminal 157
to the emitter 158 of transistor 142 and the connection of base 159
of transistor 142 to input terminal 100, emitter 158 is accordingly
more positive than base 159 and transistor 142 is thus biased in
the off condition so that the signal from oscillator 73 is not
transmitted to output terminal 155. Assuming now that the signal at
input terminal 139 is positive, a base drive current flows through
resistor 148 into base 156, turning transistor 143 on. When
transistor 142 is turned on, the voltage at terminal 157 is
substantially more negative than when transistor 142 is off, and
emitter 158 of transistor 142 is no longer positive with respect to
base 159. The input signal from oscillator 73 is now transmitted
via transistor 142 and coupling transformer 149 to output terminal
155. The RF signal appearing at output terminal 155 has thus been
shown to be modulated on and off by means of the rectangular wave
signal appearing at input terminal 139 as received from
multivibrator 77.
Capacitor 152 is selected to be resonant with the inductance of
transformer 149, thereby becoming a parallel resonant circuit at
the RF frequency. Capacitor 153 is an RF bypass for emitter
158.
Transmitter 64 is also designed to permit voice modulation as an
alternate mode of operation. Microphone jack 27 provided for this
purpose has a signal terminal 162, a grounding terminal 163 and a
chassis ground terminal 164. When a microphone is plugged into jack
27 and pressing the "talk" button of the microphone connects
terminal 163 to ground, transistor 119, by virtue of the connection
of its base 128 to grounding terminal 163, is held in an off
condition so that the multivibrator 77 becomes inoperative. The
signal from the microphone installed in jack 27 is now transmitted
via coupling capacitor 154 to the base 156 of transistor 143 and
the microphone signal thus drives transistor 143 over a range
spanning the conductive to non-conducting states of transistor 143,
thereby controlling the bias condition of transistor 142 and
accordingly modulating the signal from oscillator 73 at the
audio-frequency rate produced by the microphone. Resistor 165 and
diode 166 supply voltage to the microphone through jack 27.
Output amplifier 75 includes a transistor 167, a coupling capacitor
168, a high frequency bypass capacitor 169, inductors 172 and 173,
biasing resistors 174 and 175, tank circuits 176 and 177, and
output terminal 178. The combination of inductors 172 and 173 in
conjunction with tank circuits 176 and 177 form a ladder network
filter for impedance matching of the transmitter to the antenna at
the desired frequencies. Bias resistors 174 and 175 establish the
desired DC bias condition at the base 183 of transistor 167 so that
the output signal from the modulator 74 coupled from terminal 155
through capacitor 168 to the base 183 of transistor 167 produces a
pulse of RF collector current in transistor 167 corresponding to
each cycle of oscillator voltage passed by modulator 74. The pulses
of collector current of transistor 167 flowing through inductor 172
excites tank circuit 176 at the crystal-controlled frequency of
121.5 Mhz produced by oscillator 73 and as modulated by modulator
74. Tank circuit 176 is thus caused to ring or oscillate in
synchronism with the oscillator signal at 121.5 Mhz. Inductor 172
provides a path by which synchronizing impulses are supplied to
tank circuit 176 and at the same time it provides adequate AC
isolation between tank circuit 176 and transistor 167 to permit the
substantially sinusoidal oscillation of tank circuit 176. High
frequency energy at 121.5 Mhz is coupled to output terminal 178
through inductor 173. The tank circuit 177 is tuned to a resonant
frequency of 243 Mhz and it receives current pulses via inductors
172 and 173 as transistor 167 responds to signals delivered by
modulator 74. For each impulse received by tank 176, two cycles of
oscillation occur therein at its resonant frequency of 243 Mhz.
Both the 121.5 Mhz oscillator signal and its 243 Mhz harmonic are
thus present at output terminal 178, which is connected to antenna
14.
An improved and exceptionally versatile emergency airplane locating
transmitter has thus been described which may be automatically
energized on impact or manually energized. The transmitted signal
is modulated by means of a specially controlled multivibrator which
produces a periodically changing audio distress signal. It is also
designed and equipped to permit voice modulated output signals by
connecting a microphone to jack 27 on the front of housing 11. The
device is equipped with a special mounting bracket so that it may
be secured to the aircraft and it is also fitted with a convenient
carrying handle for portable use.
A second embodiment of the remote control structure shown in FIGS.
1-4 is shown in FIG. 5, wherein a +12v DC source 190 energizes a
bus 191 of the aircraft through a circuit breaker 192, cabin switch
193, remote connector 194, remote disable module 195 and aircraft
grounding terminal 196. The disable module 195 and connector 194
are integral parts of the airplane locating device 10. Cabin switch
193 is remotely located in any suitable position for convenient
access by the pilot.
The remote control feature in this second embodiment has three
operating modes; i.e., AUTOMATIC, REMOTE ON and REMOTE OFF. These
three operating modes are determined by the position of the remote
cabin switch 193 which has a double pole, double throw, center off
configuration.
For automatic operation, cabin switch 193 is set in the "AUTO"
position for which no interconnections are made between any of its
six contacts, A, B, C, D, E and F. Activation of transmitter 64 of
device 100 is thus dependent in this mode upon the operation of
inertia switch 24 as in the case of the embodiment shown in FIGS.
1-4 wherein transmitter 64 is energized from the negative terminal
71 of battery 18A-18D through master switch 26 in its "AUTO"
position, inertia switch 24 in its closed condition to transmitter
terminal 65. The positive terminal 72 of battery 18A-18D is
directly connected to the positive transmitter terminal 70.
The "REMOTE ON" mode is employed when an emergency has occurred due
to a forced landing and the pilot of the aircraft wishes to
activate transmitter 64 manually from the cockpit. In this case,
remote cabin switch 193 is set to the "on" position, which closes
contacts D and E of this switch. Contacts D and E are connected in
parallel with inertia switch 24 through terminals G and H of
connector 194, and serve as a manual means of overriding the open
condition of switch 24 or as a means for insuring operation when
inertia switch 24 should have closed or might have closed due to
the impact of a crash landing. In either event, transmitter 64 is
energized as in the automatic mode except that the negative battery
connection may be made in this case through closed contacts D and E
of remote cabin switch 193 rather than through inertia switch
24.
The "REMOTE OFF" mode is employed only in the event that the
inertia switch 24 has been closed inadvertently and the unit has
been activated without need. In this situation, the pilot of the
aircraft sets the remote cabin switch 193 to the "off" position,
which connects the +12v bus 191 via main circuit breaker 192,
contacts B and C of cabin switch 193, and terminal J of remote
connector 194 to positive input terminal 197 of remote disable
module 195. The negative input terminal 198 of remote disable
module 195 is returned via terminal K of connector 194 to aircraft
ground terminal 196. A positive 12 volt source is thus contained to
positive terminal 197 relative to negative terminal 198 of module
195, and a resulting current flowing from terminal 197 through
resistor 199, 4.7 volt zener diode 200 and fuse 201 to negative
terminal 198 establishes a +4.7 volt potential at cathode 202 of
zener diode 200. The 4.7 volt potential is applied through diode
203 to the junction of resistors 95 and 96, which are serially
connected between emitter 83 of transistor 79 and ground in
oscillator circuit 73 of transmitter 64. The emitter base junction
of transistor 79 is thereby biased to an "off" condition and
oscillator 73 is thus disabled. In normal operation, when the
"remote off" condition is not set, diode 200 is reverse biased by
the positive operating voltage present at the junction of resistors
95 and 96 and the remote disable module 195 has no effect on the
normal operation of transmitter 64.
Fuse 201 is incorporated as a fail-safe mechanism which is operated
in the event the "remote off" mode has been set and a subsequent
crash occurs, in which case it is desirable that the transmitter 64
should be rendered operational. In the event of such a crash it is
likely that external fixed antenna 15 will come into contact with
the frame of the aircraft. Such a contact making an electrical
connection between antenna 15 and aircraft ground causes fuse 201
to open as a result of a fault current flowing from positive
battery terminal 72 to transmitter terminal 70 through inductor
181, antenna terminal 178, aircraft frame or ground to ground
terminal 196, terminal K of remote connector 194 and fuse 201 to
negative battery terminal 71. The resultant opening of fuse 201
effectively removes the +12 volt potential at terminal 197 and the
remote disable module 195 is itself disabled and prevented from
interfering with the operation of transmitter 64.
Severing or shorting of connections between remote connector 194
and remote cabin switch 193 during a crash also results in
fail-safe conditions in that transmitter operation is not thereby
prevented.
Loss of the +12 volt source or the opening of the main breaker 192
in the event of a crash will also cancel the effect of the "remote
off" condition to allow transmitter operation. Thus, a useful and
highly reliable remote control capability is provided.
Although but two embodiments of the present invention have been
illustrated and described, it will be apparent to those skilled in
the art that various changes and modifications of the invention may
be made therein without departing from the spirit of the invention
or from the scope of the appended claims.
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