U.S. patent number 3,757,695 [Application Number 05/003,606] was granted by the patent office on 1973-09-11 for charging system for electric bomb fuzes (u).
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Evan D. Fisher.
United States Patent |
3,757,695 |
Fisher |
September 11, 1973 |
CHARGING SYSTEM FOR ELECTRIC BOMB FUZES (U)
Abstract
An electric bomb charging device self-contained within the bomb
requiring external charging gear. The device is placed within a
charging well located along the longitudinal surface of the bomb
and is adapted so as to receive the slipstream of air flowing along
the bomb's surface after it is released from the aircraft. The
charging device transforms the air slipstream into the electrical
energy necessary to operate a proximity sensor and electric fuze
located within the bomb. The device is provided with a protective
cover that is removed by a lanyard only upon the bomb's release,
and a minimum threshold velocity must be attained before the
charging device is actuated. In a first embodiment form, the device
is comprised of a modified fluidic generator, while in a second
embodiment it takes the form an anemometer-type vane coupled with
an electric alternator. Both embodiments employ electronic circuits
to regulate the output voltages derived therefrom.
Inventors: |
Fisher; Evan D. (Chevy Chase,
MD) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
21706667 |
Appl.
No.: |
05/003,606 |
Filed: |
December 19, 1969 |
Current U.S.
Class: |
102/207; 102/224;
102/208 |
Current CPC
Class: |
F42C
15/295 (20130101); F42C 11/04 (20130101); F42C
11/00 (20130101); F42C 19/04 (20130101) |
Current International
Class: |
F42C
15/295 (20060101); F42C 19/00 (20060101); F42C
15/00 (20060101); F42C 19/04 (20060101); F42C
11/00 (20060101); F42C 11/04 (20060101); F42b
005/08 () |
Field of
Search: |
;102/7.2G |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Feinberg; Samuel
Claims
I claim as my invention:
1. An environmental charging system for providing energy to
electric bomb fuzes without the use of external charging equipment,
comprising:
a. an electric fuze bomb having an existing charging well common to
electrically fuzed bombs and centrally located along the
longitudinal portion of the bomb;
b. a proximity sensor connected to said charging well by a
multiwire cable and centrally located at the forward portion of the
bomb for providing target signals;
c. an electric fuze connected to said charging well by an
additional multiwire cable and responsive to said target signals
for actuating an explosive mechanism;
d. slipstream actuated energizing means for providing electric
energy to said proximity sensor and to said electric fuze in
response to a predetermined threshold fluid flow, said slipstream
actuated energizer including a resonant cavity for producing fluid
oscillations of said input fluid, said energizer being located
within said charging well;
e. fluid input means within said energizing means for receiving
slipstream fluid flow along said bomb;
f. fluid output means for exhausting a portion of said slipstream
fluid;
g. mechanical means responsive to said slipstream fluid flow
comprising a diaphragm that vibrates in response to said fluid
oscillations and a rod connected to said diaphragm to transmit
vibrations to a metallic reed positioned within a magnetic
field;
h. a magnetic field coupled with said mechanical means for
producing electrical signals in response to said mechanical means;
and a magnetic lock means to prevent magnetic field actuation until
a preselected minimum air velocity is attained;
i. voltage regulating means for controlling said electrical signal
to provide a predetermined voltage output;
j. safety cover means being secured by an O-ring seal and retaining
nut to shield said input and output means; and
k. an arming lanyard to remove said safety cover means upon release
of said bomb from the aircraft.
Description
RIGHTS OF GOVERNMENT
The invention described herein may be manufactured, used, and
licensed by or for the United States Government for governmental
purposes without the payment to me of any royalty thereon.
BACKGROUND OF THE INVENTION
This invention relates generally to charging devices and, more
particularly, to environmental charging systems that provide energy
for electric bomb fuzes.
Many of the electrical bomb fuzes now in standard use require
complex external charging equipment for providing electrical energy
to the fuzing system. In addition to their unwieldy structure, such
equipment requires the use of special bomb mounting racks and
plug-in connectors not ordinarily found on aircraft. This type of
charging gear occupies a great deal of space, which frequency
precludes its use in special aircraft that use all existing space
to accommodate other vital control equipment as needed, for
example, in aircraft that carry atomic bombs. The special electric
charging gear in current use is installed and designed so that the
electric bomb fuzes are energized while falling from the aircraft
just after release. Upon release, the charging gear is disengaged
and the fuze becomes fully charged and ready for arming. The safety
of the bomb is dependent on the reliability of the various safety
devices in the fuze to prevent arming until the bomb has fallen a
safe distance from the aircraft. A malfunction of the charging or
releasing gear occurring, for example, while the plane is still on
the ground, would lead to a premature detonation of the bomb
causing serious injury to the aircraft and/or crew members.
Accordingly, a primary object of the present invention is to
provide a charging system for electric bomb fuzes that positively
will not energize the fuze until a prescribed minimum velocity is
attained.
Another object of the present invention is to provide a charging
system for electric bomb fuzes that is reliable, foolproof, easily
adaptable to existing bomb structures, and has a minimum of moving
parts.
A further object of the present invention is to provide a charging
system for electric bomb fuzes that requires no special mounting
racks or connectors for its utilization in existing bomb
structures.
A still further object of the present invention is to provide an
electric bomb charging device that is dependent for its actuation
upon the release of the bomb from the aircraft.
SUMMARY OF THE INVENTION
The aforementioned and other objects may be obtained by using a
charging device that is self-contained within the bomb and requires
no external connections or special mounting racks for its actuation
and support. The device of the present invention is placed within
an existing charging well of common electrically fuzed bombs and is
adapted to receive the slipstream of air flowing along the bomb's
surface subsequent to its release from the aircraft. The device
converts the energy of the slipstream into electrical energy that
powers the bomb fuze; no activation is possible in the absence of a
slipstream. The device is shielded from mud, air and condensation
prior to release by a lanyard-operated cover that is removed only
upon release. Further safety is assured in both embodiments by
requiring a minimum bomb velocity prior to their actuation.
BRIEF DESCRIPTION OF THE DRAWINGS
The specific nature of the invention, as well as other objects,
aspects, uses, and advantages thereof will clearly appear from the
following description and from the accompanying drawing, in
which:
FIG. 1 is a partially cut away illustration of a commonly used
electric-fuze bomb in combination with an environmental charging
device of the present invention;
FIG. 2 is a cut away view of a fluidic charging device of the
present invention; and
FIG. 3 is another embodiment of a charging device of the present
invention utilizing an electro-mechanical generator.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1 illustrates generally at 10 a very common configuration of a
high-explosive electrically fuzed bomb for which the device of the
present invention is intended. At 12 is depicted the environmental
charging device of the present invention located within and secured
by the center charging well 14 of bomb 10 located approximately at
the longitudinal midpoint of the bomb as shown in FIG. 1. A cover
16 shields the device 12 from the outside environment until ready
for use. Charging device 12 provides electrical power by means of a
multiwire cable 24 to a proximity sensor 22 located in the nose of
the bomb and by means of a multiwire cable 28 to an electric bomb
fuze 26 located aft.
Bomb 10 remains inactive until it is released. Upon release, cover
16 is removed automatically by an arming lanyard 18 attached to the
aircraft by means of a pin 20. The exposure of the charging device
12 to the air slipstream that flows past bomb 10 after release
actuates generators within the device 12 in a manner described more
fully below. The threshold level of proximity sensor 22 is
preselected such that when bomb 10 is at the optimum distance from
the target, sensor 22 emits a signal back through cable 24 and
through cable 28 to fuze 26 to detonate the bomb. In the event of
the failure of sensor 22 to emit said signal, fuze 26 is equipped
with point detonation capability in a manner well known in the
art.
FIG. 2 illustrates one preferred embodiment of environmental
charging device 12 of FIG. 1 in the form of a modified fluidic
generator. Cover 16 is shown in its pre-release position, sealing
the device so that mud, water or air cannot enter the device prior
to release. When arming lanyard 18 positively removes cover 16, the
slipstream of air along the surface of the bomb enters a resonant
cavity 32 and vibrates back and forth in the cavity at a
preselected frequency according to the dimensions of the cavity 32.
The vibrations of air in the cavity cause diaphragm 34 to
oscillate. Excess air is exhausted to the atmosphere through vent
33. The oscillations of diaphragm 34 are transmitted by means of a
rod 36 to a metallic reed 38 which in turn vibrates between the
poles of a permanent magnet 40. The motion of reed 38 tends to
switch the magnetic field set up by magnet 40 and thus induce an
emf in a coil 42 surrounding reed 38. This induced emf is
subsequently stepped up by transformer 44 and is rectified and
limited to the desired level by a rectifier and voltage limiting
circuit 45. The operating voltage needed for the proximity sensor
22 of FIG. 1 is coupled thereto by means of cable 46 which is
comprised of a three-wire line consisting of a ground wire, a hot
wire, and a wire to transmit said detonating signal from sensor 22
back to device 12 and through cable 48 to fuze 26 of FIG. 1. A
potting compound 50 protects the electronic components and cables
from shock and vibration. The safety features of the device 12 are
now apparent. The generator will operate only after the protective
cover 16 is removed and the bomb is moving above the preset minimum
velocity necessary to cause oscillation of the air in the resonant
cavity 32. This minimum velocity requirement means that the fuze
cannot energize until the aircraft is indeed in flight and is
exceeding the prescribed minimum velocity.
In FIG. 3 is shown another embodiment of the charging device 12 of
FIG. 1. This embodiment consists of a multipole alternator 52 which
is driven by an anemometer-type vane 54. Anemometer vane 54 is
locked in a fixed position by a cover 16 which is O-ring sealed to
the retaining nut 56. Tabs (not shown) are turned under the nut 56
flange which require a minimum pull force to remove cover 16. Cover
16 is fitted with arming lanyard 18 attached to the arming solenoid
(not shown) on the rack of the aircraft by means of ring 20. Cover
16 is removed from the device 12 by arming lanyard 18 upon release
of the bomb. The dsign of alternator 52 is such that the magnetic
lock of the rotor will prevent rotation of vane 54 up unless a
preselected minimum air velocity is attained with cover 16 removed.
Excess air is exhausted to the atmosphere through vent 53. A
transformer 60 steps up the AC voltage thus generated while a
voltage doubler and rectifier circuit 58 increases the rise rate of
the voltage and converts the generator output from AC to DC. Zener
diodes (not shown) can be used to regulate the output voltage to
the desired level to operate proximity sensor 22 and fuze 26 of
FIG. 1. The necessary signals are transmitted to the latter two
devices by means of cables 46 and 48, respectively.
The two embodiments shown in FIG. 2 and FIG. 3 are both
particularly designed to derive their power for operation from the
slipstream of air flowing along the longitudinal surface of the
bomb after it is released. In this manner, reliability of opeation
and pre-release safety is assured.
I with it to be understood that I do not desire to be limited to
the exact details of construction shown and described, for obvious
modifications will occur to a person skilled in the art.
* * * * *