U.S. patent number 3,760,732 [Application Number 05/104,896] was granted by the patent office on 1973-09-25 for weapon system for a set in-flight digital time fuze with muzzle action.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Edmund L. Bisson, William A. Schuster.
United States Patent |
3,760,732 |
Schuster , et al. |
September 25, 1973 |
WEAPON SYSTEM FOR A SET IN-FLIGHT DIGITAL TIME FUZE WITH MUZZLE
ACTION
Abstract
An improved rapid fire weapons system that permits a projectile
while in ght to be safely and accurately set and armed for either
muzzle action or long distance detonation of the projectile against
either moving or stationary targets by a coded high frequency
transmitted pulse or in the event of an electrical failure by a
hand settable switch to muzzle action. The invention described
herein may be manufactured, used, and licensed by or for the
Government for governmental purposes without the payment to us of
any royalty thereon.
Inventors: |
Schuster; William A.
(Hopatcong, NJ), Bisson; Edmund L. (Hackettstown, NJ) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
22303015 |
Appl.
No.: |
05/104,896 |
Filed: |
January 8, 1971 |
Current U.S.
Class: |
102/215; 89/6;
244/3.19 |
Current CPC
Class: |
F42C
17/04 (20130101); F42C 13/047 (20130101) |
Current International
Class: |
F42C
13/00 (20060101); F42C 17/00 (20060101); F42C
13/04 (20060101); F42C 17/04 (20060101); F42c
011/06 (); F42c 011/00 (); F42c 009/00 () |
Field of
Search: |
;102/7.2R ;244/3.19 |
References Cited
[Referenced By]
U.S. Patent Documents
|
|
|
3419861 |
December 1968 |
Resnik et al. |
3531691 |
September 1970 |
Sitler et al. |
|
Primary Examiner: Borchelt; Benjamin A.
Assistant Examiner: Webb; Thomas H.
Claims
What is claimed is:
1. An improved rapid fire weapon system of the type wherein a
moving target is tracked by a range finder having an output
electrically connected to a computer that assimilates the range
finder output producing a computer output which relates the
distance from a fired projectile, as it exits from a muzzle of a
gun to the target, said computer output being electrically
connected to a pulse transmitter to cause said pulse transmitter to
radiate a coded high frequency electromagnetic pulse as a function
of the range finder sensed distance between said projectile while
in flight and the target, wherein the improvement comprises:
a receiving antenna located in said projectile for picking up said
transmitted signal;
a detector/discriminator, electrically connected to said antenna,
detects said coded pulses transmitted and delivers at least one or
more output pulses to an electrically connected amplifier and to an
electrically connected muzzle burst level discriminator and
amplifier when the detector/discriminator detects a high voltage
long duration signal from the pulse transmitter calling for muzzle
burst action, said muzzle burst level discriminator and amplifier
being nonresponsive to the normal range setting pulses generating a
first activation signal which can initiate a detonator;
means for counting, electrically connected to said amplifier and
responsive to said range setting pulses, generates a second
activation signal after a predetermined maximum number of
counts;
means for gating the input to said means for counting responsive to
said range setting pulses to prevent said counting means from
receiving additional pulses from spurious signals which may be
received by said antenna after the range setting pulses have been
detected and amplified;
means for generating additional pulses within said projectile are
electrically coupled to said gating means, filling said means for
counting with the additional pulses necessary to reach the
predetermined maximum number of counts, said additional pulses
being a function of the distance from the projectile as it leaves
the muzzle of the gun and the target;
a first means for supplying energy to operate circuitry of said
detector/discriminator, amplifier, means for gating, and means for
generating additional pulses after the projectile is launched;
a second means for supplying energy to initiate said detonator upon
receipt of an activation signal from either the means for counting
and the muzzle burst level discriminator and amplifier;
a hand settable switch is electrically connected intermediate to
said second energy source and said detonator providing for
initiating said detonator in the event of electrical circuits
failure in the pulse transmitter;
means for safely arming said projectile is electrically connected
intermediate to said counting means and said detonator, between
said muzzle burst level discriminator and amplifier and said
detonator, and between said hand settable switch and said
detonator; and
an electronic gate responsive to either said first or second
activation signal and electrically coupled intermediate to said
second energy source and said detonator, discharges energy from
said second energy source into said detonator through said arming
means.
2. An improved rapid fire weapon system as recited in claim 1
wherein the means for counting comprises:
a three decade counter coupled to said means for gating, first
sequentially counts the number of coded pulses generated by said
pulse transmitter and passed by said detector/discriminator and
amplifier circuits, secondly, said counter is responsive to the
output of the means for generating additional pulse, said means for
generating additional pulses supplies the additional counts
necessary to fill the counter to the predetermined maximum number
and is directly related to the distance from the projectile to the
target, the further the distance the greater number of additional
counts necessary to fill the three decade counter; and
an automatic initial clear circuit, electrically coupled to said
three decade counter, generates a signal, after the projectile has
left the muzzle of the gun, which sets the decades of said three
decade counter to zero thus assuring a setting responsive only to
the pulse transmitter.
3. An improved rapid fire system as recited in claim 1, wherein the
means for gating comprises:
a first "And" gate, having a first input electrically coupled to
the output of said amplifier, allows pulses generated by the pulse
transmitter to pass, having a second input;
an "Or" gate, electrically coupled intermediate to said first "And"
gate and said three decade counter permits the pulses generated by
said amplifier to pass to said three decade counter;
means for delaying said first "And" gate electrically connected
intermediate to said amplifier and said second input of said first
"And" gate inhibiting said first "And" gate from passing any
subsequent spurious signals; and
a second "And" gate having first input and a second input
electrically connected to said means for generating additional
pulses coupled to said delaying means and intermediate to said "Or"
gate prevents passage of pulses generated by said means for
generating additional pulses from reaching the three decade counter
until a signal is received from said delay means making said second
"And" gate responsive.
4. An improved rapid fire system as recited in claim 3 wherein the
delaying means comprises:
a delay circuit having its input electrically coupled to the output
of said amplifier for generating after a fixed predetermined period
of time a signal;
an inverter having its input electrically connected intermediate
the output of said delay and said second "And" gate second input
and its output electrically coupled to said first "And" gate second
input for inhibiting said first "And" gate from passing subsequent
signals received from said amplifier, when said delay delivers said
signal simultaneously to said electrically coupled second "And"
gate making it responsive to pass additional pulses from said means
for generating additional pulses.
5. An improved rapid fire system as recited in claim 4 wherein the
means for generating additional pulses is a clock oscillator having
an output pulse frequency of 100 herz.
6. An improved weapon system as recited in claim 1 wherein the
first means for supplying energy is a reserve battery activated by
the set back forces created when projectile is launched, said
battery activates said automatic initial clear circuit when 90
percent of the battery output voltage has been reached, and
supplies energy to operate said clock oscillator,
detector/discriminator, means for gating, means for delay,
amplifier and three decade counter.
7. An improved weapon system as recited in claim 1 wherein the
second means for supplying energy is a piezoid generator, said
piezoid generator supplies energy to operate electrically coupled
said muzzle burst level discriminator and amplifier and initiates
said coupled detonator when said electronic gate is triggered
either by said muzzle burst level discriminator and amplifier or
said activation signal of said three decade counter, said piezoid
generator provides the energy to fire said detonator by the
intermediate electrically connected said hand settable switch.
8. An improved weapon system as recited in claim 1 wherein the
means for safely arming said projectile comprises:
a first pair of delay spin switches intermediate to said
electrically coupled three decade counter and a coupled isolation
circuit, said isolation circuit matches the impedance of said three
decade counter to the impedance of said coupled electronic gate;
and
a second pair of spin switches electrically connect both the hand
settable switch and the output of said electronic gate through an
in series setback switch to said detonator preventing said
detonator from receiving a malfunctioning timing signal from said
muzzle burst level discriminator and amplifier, said three decade
counter or said electronic gate prior to the projectile being
launched from said gun.
9. An improved weapons system as recited in claim 1 wherein said
electronic gate is a silicon controlled rectifier.
Description
BACKGROUND OF THE INVENTION
This invention relates to a weapons system for setting a fuze and
has particular reference where the projectile is alternatively
either set-in flight by a transmitted coded high frequency
electromagnetic signal or by manually setting the fuze in emergency
situations such as where the transmitting equipment becomes
inoperative.
Prior art fuzes have had the capability of being set mechanically
by hand, electrically, chemically, and/or combinations of these
methods. In all of these instances the fuze was set prior to the
firing of the projectile from the launching weapon. The development
of automatic loaders and rammers for rapid fire weapons has made
access to the fuze which requires mechanical manual setting by hand
impractical. A mechanical fuze setter for available mechanical time
fuzes is too large and heavy to be adaptable for mobile automatic
high rate of fire equipment.
For fuzes which are set before they are loaded into the gun an
error is introduced, in the fuze setting, by the varying time
parameters required to load and fire the gun, thus making it very
difficult, if not impossible to hit fast moving targets. Using our
set in-flight digital time fuze invention minimizes these timing
errors and makes it feasible to shoot at fast moving targets with a
rapid fire rate with greater accuracy.
Those fuzes which are electronically set prior to firing of the
projectile, while still in the launching weapon, are encumbered
with electrical connections which must make contact with an
electrical umbilical cable which is usually connected to the fire
control equipment. In our invention there is no necessity for an
umbilical connection between the fuze and the ground equipment
because the fuze is set while in flight. In prior art fuze systems
described aforesaid malfunctions can occur because of faulty
contact between the connectors from the projectile and the
umbilical cord which transmits the electrical signals for setting
the fuze.
Another problem with prior art fuze systems, which are set prior to
launch, is the danger that a malfunction which occurs in the time
fuze, while the projectile is in the weapon, will endanger the
launch crew. For systems which use an actuated in-flight counter
concept, the system has been found unsatisfactory to meet the need
for rapid rate of fire since the tracking radar must illuminate the
projectile in-flight until functioning occurs at the desired range.
Where the range is approximately 5000 meters the flight time is
generally 10 to 15 second, thus the tracking time required has a
limiting effect on the resultant rate of fire. In the present
invention the digital time fuze is set subsequent to weapon firing
and very shortly after the projectile leaves the muzzle of the gun
by means of "high frequency" pulses sent from a pulse transmitter
at the weapon site to a receiver in the fuze. These high frequency
pulses contain coded information received from collaterally coupled
ranging and computing equipment which arm and detonate the
projectile a given distance from the oncoming target. As used
throughout the specification and claims, the term "high frequency"
refers to a range of frequencies between 20 megaherz and 10
gigaherz.
SUMMARY OF THE INVENTION
The present invention relates to a set in-flight digital time fuze
which can be armed and detonated by either coded high frequency
pulses received from a pulse transmitter activated by collaterally
coupled ranging and computing equipment, or manually set by
hand.
The projectile after exiting from the gun, and having traveled a
predetermined distance generally ranging from 175 feet to 300 feet,
receives a series of high frequency pulses of approximately 0.5
microseconds duration. These pulses are propagated from a
transmitter in the fire control equipment and received by the
receiving antenna in the fuze. The number of pulses transmitted
being a function of time to be set in the fuze. These pulses after
being received by the receiving antenna are detected by a
detector/discriminator circuit which will only favorably receive
signals from the fire control pulse transmitter. The output of the
detector/discriminator is coupled to an amplifier where the signal
is amplified and fed to a three decade counter through an
intermediate first "And" and an "Or" gate, and to a delay circuit
which inhibits a second "And" gate which prevents a clock
oscillator output signal from reaching the three decade counter,
until the amplified pulse settings from the fire control signal are
entered into the counter. After a delay of approximately 0.015
seconds the output of the delay circuit not only initiates the
internal fuze counting, but is also used to inhibit the first "And"
gate so that no additional pulses from the amplifier can reach the
three decade counter. At this point the fuze oscillator continues
to fill the counter until the maximum count is reached which
switches a silicon controlled rectifier, or other suitable
electronic gate causing the detonator to function.
Electrical energy is provided for the aforementioned circuitry by a
suitable reserve battery which is activated on setback. Electrical
energy for initiation of the detonator is provided by a
piezoelectric generator whose energy is also derived from the
setback force.
In order to insure that the counting circuits are in the "O" set
state, at the time that the high frequency pulses are inserted into
the three decade counter, an automatic initial clear circuit
operates as soon as the battery voltage achieves approximately 90
percent of its full output voltage.
Where activation of the projectile is desired at or near the muzzle
a high amplitude long duration pulse is sent to the fuze as soon as
the projectile emerges from the weapon. This special high amplitude
long duration signal by-passes the amplifier and is coupled
directly into the muzzle burst level discriminator and amplifier
circuit. The muzzle burst level discriminator-amplifier circuitry
is powered by the piezoelectric generator. The output of the muzzle
burst level discriminator-amplifier is coupled to the silicon
controlled rectifier whose activation causes the initiation of the
detonator. During the muzzle burst operation the fuze oscillator,
three decade counter, delay, and gating circuits, amplifier, and
detector/discriminator circuitry are not operative since the
battery voltage is relatively low. Safety due to electrical
malfunction, in the fuze during muzzle burst operation, is provided
by a pair of normally open spin switches and setback switch which
isolate the electrical circuits between the detonator and the
piezoelectric generator.
In case of power failure or damage to the range finding, computing
and transmitting equipment, which is usually located in or on the
launch vehicle or weapon carrier, muzzle action can be obtained by
manually setting the fuze by a hand settable switch to a muzzle
action mode.
One of the objects of this invention is to provide a set in-flight
digital time fuze which can arm and detonate a projectile fired by
a rapid fire weapon.
Another object of this invention is to improve the setting of fuzes
in rapid fire weapons without any loss of accuracy.
Another object of this invention is to insure that a set in-flight
fuze will not endanger the launch crew because of malfunction.
A further object of this invention is to enable a projectile fuze
to be electronically set for rapid fire weapons or, in case of an
emergency, to be manually set.
Another object of this invention is to provide an improved set-in
flight fuze which can set the time for arming and detonating a
projectile after launch without the disadvantage and limitation of
prior art arrangements which utilize umbilical electrical
connections to the fuze from a fire control system.
For a better understanding of the present invention, together with
other and further objects thereof, reference is made to the
following description taken in connection with the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a diagram of a set-in flight time fuze and fire control
equipment for a weapon system.
FIG. 2 is a chart showing the time sequence for the fuze components
as a function of the distance of travel of a projectile having a
muzzle velocity of 2,330 ft/sec.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1 is a block diagram of a set in-flight digital time fuze with
muzzle action. The components of the fuze 19 located in the
projectile are shown below the dashed line 18, the components above
the dashed line are those used in the weapon for electronic fire
control. Ranging equipment 10 is coupled to a computer 12 through
conductor 11; computer 12 evaluates the distance between the
projectile launch vehicle (not shown) and the target (not shown)
and feeds an output through conductor 13 to pulse generator and
transmitter 14; pulse generator and transmitter 14 generates coded
pulses of high frequency energy which is transmitted by a
transmitting antenna 16. The coded high frequency burst of pulses
is received by the fuze receiving antenna 20; these pulses are of a
specific pulse duration, amplitude, and frequency. The number of
pulses transmitted are a function of the time it takes for the
projectile to reach the target area. The further the target, the
smaller the number of pulses transmitted.
The coded pulse signal is received by the fuze antenna 20 and
detected by the detector/discriminator 22 which selectively
discriminates between these coded pulses and spurious signals and
favorably receives the transmitted coded pulse signals. The
detector/discriminator 22 is similar to diode detectors described
in "Electronic Designers Handbook," Pages 703-707, McGraw Hill by
R. W. Landee, D. C. Davis, A. P. Albrecht. The output of the
detector/descriminator 22 is coupled to an amplifier 25 by a
conductor 23, and to a muzzle burst level discriminator and
amplifier circuit 26 by conductor 24. The amplifier 25 is similar
to, and may be obtained, from Motorola Semi-conductor Prod. Inc.,
5005 E. McDowell Rd., Phoenix, Ariz. 85008, Model MC 1510 Wideband
Integrated Circuit Amplifier. The muzzle burst level discriminator
and amplifier 26 consists of a Schmitt Trigger and Wideband
Amplifier. The Schmitt Trigger is similar to Schmitt Triggers
described in "Transistor Circuits and Applications" pp 136-137,
Prentice-Hall Inc., Englewood Cliffs, N. J. (1968) by Laurence G.
Cowles. The widebank amplifier is available from the Motorola
Semiconductor Products Inc., 5005 E. McDowell Rd., Phoenix, Ariz.
85008, Model MC 1510.
The amplifier output is coupled by conductor 27 to a first "And"
gate 28 which permits the coded signal to pass thru. The first
"And" gate 28 is coupled to an "Or" gate 30 by conductor 29. The
output of "Or" gate 30 actuates the three decade counter 32, by
conductor 31, for the specific number of pulses transmitted. The
decade counter 32 is available from Fairchild Semiconductors, 313
Fairchild Dr., Mt. View, Calif. 94040, Model DTUL 945 Flip-Flop. At
the same time that the amplifier 25 sends a signal to the first
"And" gate 28, a pulse is fed to delay 34 through conductor 33. The
output from delay 34 actuates the inverter 36 by conductor 35. The
delay 34 is similar to a delay which may be obtained from Fairchild
Semiconductor Model DTL 951. The output of inverter 36 is coupled
to the first "And" gate 28 by conductor 37 and inhibits the further
transmission of pulses through the first "And" gate 28. The purpose
of the circuit consisting of delay 34, inverter 36, and first "And"
gate 28 is to inhibit spurious transmitted pulses from entering the
three decade counter 32 after the required information is received.
This circuit insures that the first fuze time set by the initially
received pulses from the fire control transmitter is not disturbed
by subsequent pulse trains. This is advantageous because it
prevents the fuze that is once set from being accidentally or
purposely disturbed.
After a fixed period of time, predetermined by the characteristics
of delay circuit 34, a signal is transmitted from delay 34 by
conductor 39 to a second "And" gate 40 making it receptive to pass
pulses received from clock oscillator 42 by means of conductor 41.
The clock oscillator 42 is similar to the clock oscillator
described in "Transistor Circuits and Applications," pp 191-192,
Prentice-Hall, Inc., Englewood Cliffs, N. J. (1968) by Laurence G.
Cowles. "And" gate 40 output is coupled by conductor 43 to "Or"
gate 30 which transmits the clock oscillator 42 pulses which supply
to the three decade counter 32 the remaining additional pulses
necessary to fill the counter and cause an activation signal. The
"Or" gate 30, "And" gates 28 and 40, and inverter 36 are available
from Fairchild Semiconductors, 313 Fairchild Dr., Mountain View,
Calif. 94040, Model DTL 946 Quad Two-Input Gate Element, Fairchild
Diode-Transistor Micrologic.
The clock oscillator 42, detector/discriminator 22, amplifier 25,
delay 34, inverter 36, gates 28, 30, and 40, and an auto initial
clear circuit receive their energy from a battery 44 which is
activated by setback forces upon launch of the projectile through
conductor 45.
In order to insure that the three decade counter 32 is in the
"zero" count position before it receives any initial signal
detected from the pulse transmitter 14, an auto initial clear
circuit 46 transmits by conductor 47 a signal to the three decade
counter 32 when approximately 90 percent of the battery 44 maximum
output voltage is reached. The auto initial clear circuit 46 is
similar to the circuit described in "Electronic Digital
Techniques," pp 150-151, McGraw Hill (1960) by Paul M. Kintner. The
signal generated by the auto initial clear circuit 46 will initiate
a pulse establishing a "zero" setting for each decade of the three
decade counter 32. At least one pulse is necessary to be received
by the fuze receiving antenna 20 and passed through to "And" gate
40 before the clock oscillator 42 pulses will pass "And" gate 40
and be counted by the three decade counter 32. The three decade
counter 32 will deliver an actuation signal after it has received a
predetermined number of counts; this actuation signal is
electrically connected by conductor 49 to a first pair of delay
spin switches 48. The first pair of delay spin switches 48 are
normally open mechanical switches whose function is to protect
against a premature firing signal from the decade counter 32. After
the projectile has reached a given angular velocity the delay spin
switches 48 will permit the decade counter 32 actuation signal to
be electrically coupled by conductor 51 to a matching isolation
circuit 50 and to the trigger terminal of a silicon controlled
rectifier 52, or any other equivalent electronic gate, by conductor
53. The isolation circuit 50 is similar to the isolation circuit
described in "Transistor Circuits and Applications," pp 29-31
Prentice-Hall Inc., Englewood Cliffs, N. J. (1968) by Laurence G.
Cowles. Silicon controlled rectifiers similar to silicon controlled
rectifier 52 are available from the Semiconductor Products
Department, General Electric Co., Syracuse, N. Y. 13201; Model
Number: C 20B. The output of a piezoelectric generator 54 which is
activated by the pressure forces of setback provides the energy
necessary to initiate a detonator 60. The output of the
piezoelectric generator 54 is coupled to the silicon rectifier 52
by a conductor 55. When the silicon controlled rectifier 52
receives an actuation signal generated by the three decade counter
32, the energy of piezoelectric generator 54 will be conducted
through the SCR 52 by conductor 57 through a second pair of spin
switches 56 and through conductor 67 to a series coupled setback
switch 58 through a conductor 59 to said detonator 60. The
piezoelectric generator rectifier 54 is similar to rectifiers
described in "Electronic Designers Handbook", pp 15-2 to 15-17,
McGraw Hill, by Landee, Davis and Albrecht.
The energy from the piezoelectric generator 54 can be supplied
either through the SCR 52, or where mechanical hand setting is
desirable, by a normally open hand settable switch 62 via
conductors 63 and 64, through spin switches 56 and setback switch
58 to the detonator 60. This alternate path of conduction permits
the projectile to be safely armed and detonated even though there
is a failure in the fire control circuitry or pulse generating
circuitry.
The additional pair of spin switches 56 and a setback switch 58 are
located intermediate to SCR 52 and the detonator 60 by conductor
57, and intermediate to the normally open hand settable switch 62,
in order to prevent the projectile from firing in the barrel of the
gun in the event that there is premature discharge of SCR 52, or a
spurious output from the piezoid generator 54.
The energy from the piezoid generator 54 also supplies energy to
operate the muzzle burst level discriminator and amplifier circuit
26 by a conductor 65. The muzzle burst level discriminator and
amplifier 26 is activated when the ranging equipment 10 determines
that a target is very close to the launching weapon, and transmits
a special high voltage long duration signal to which the muzzle
burst level discriminator and amplifier 26 is receptive. The muzzle
burst level discriminator 26 is insensitive to the normal range
setting pulses. Upon receiving the special muzzle action signal the
muzzle burst level discriminator 26 transmits a pulse to the
silicon rectifier 52 through conductor 66, isolation circuit 50 and
conductor 53, enabling the energy from the piezoid generator 54 to
initiate the detonator a short distance from the muzzle of the gun.
Thus, muzzle action can be accomplished either by mechanically
operating the hand settable switch 62, or electronically by having
the muzzle burst level discriminator and amplifier 26 be responsive
to a special signal generated by the fire control circuitry as
shown above the dashed line 18.
FIG. 2 is a chart which shows a plot of the time sequence for
setting an in-flight digital time fuze as a function of the
distance from the breach of the gun or launch vehicle whose
projectile muzzle velocity is approximately 2,330 feet per second.
At time t.sub.o the projectile 74 is shown in the breach end of the
gun 70. At time t.sub.1 the projectile 74 has just received its
initial propelling thrust which causes a sufficient acceleration to
activate battery 44 and close setback switch 58. After
approximately 8 milliseconds, at time t.sub.2, while the projectile
74 is still in the weapon, the accelerating forces within the
projectile 74 generate sufficient pressure for the piezoid
generator 54 to develop an output voltage. When the projectile
approaches the muzzle end 71 of the gun 70, after 9 milliseconds,
as shown at t.sub.3. the normally open spin switches 48 and 56
close, electrically connecting the detonator 60 in the circuit. At
t.sub.4 the projectile 74 has, after 60 milliseconds, reached a
point in time where the battery 44 has developed approximately 90
percent of its maximum output voltage which is sufficient to
initiate the auto initial clear circuit 46 to deliver a pulse to
the three decade counter 32 so that each of its decades are "0"
set. At time t.sub.5, 70 milliseconds after firing of the
projectile propellant, the auto initial clear circuitry 46
completes its function. After the projectile travels between 75-125
milliseconds as shown by time t.sub.6 and t.sub.9 a distance of 177
feet and 300 feet respectively, the projectile 74 is ready to
receive a coded pulse which sets detonation time of the projectile
in response to the pulse transmitted from the fire control
circuitry as shown above dashed line 18 in FIG. 1. The increment of
time between t.sub.7 and t.sub.8 represents the duration of time
required for setting the fuze electronically for the maximum time
setting and using the parameters of the system described.
From the above description it will be evident that the invention
provides a means for accurately setting a time fuze in a projectile
while it is in flight. The in-flight setting is accomplished
without the use of encumbering electrical cables. The fuze can, in
the event of electrical failure, remain operative by being
mechanically hand set. In addition the invention has electrical
circuitry and mechanical components which protect the launch crew
in the event of a malfunction in the circuitry or the receipt of
unwanted spurious signals.
We wish it to be understood that we do not desire to be limited to
the exact detail of construction shown and described for obvious
modification will occur to a person skilled in the art.
* * * * *