U.S. patent number 3,744,418 [Application Number 05/149,489] was granted by the patent office on 1973-07-10 for flares.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Jesse F. Tyroler.
United States Patent |
3,744,418 |
Tyroler |
July 10, 1973 |
FLARES
Abstract
A flare is produced which by incremental configuration provides
a more or less constant level of illumination on the ground.
Inventors: |
Tyroler; Jesse F. (Dover,
NJ) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
22530517 |
Appl.
No.: |
05/149,489 |
Filed: |
June 3, 1971 |
Current U.S.
Class: |
102/338;
102/360 |
Current CPC
Class: |
F42B
4/26 (20130101) |
Current International
Class: |
F42B
4/00 (20060101); F42B 4/26 (20060101); F42b
013/38 () |
Field of
Search: |
;102/35,35.2,35.4,35.6,37.6,37.7,37.8 |
References Cited
[Referenced By]
U.S. Patent Documents
Other References
Military Pyrotechnics Series; Part Three; AMC Pamphlet; AMCP
706-187; Oct. 963; (pp. 157, 158, 272, 273).
|
Primary Examiner: Stahl; Robert F.
Claims
I claim:
1. A flare adapted to provide a substantially constant ground
illumination during descent comprising:
A. a flare container
B. a plurality of light illuminating pyrotechnic compositions of
differing illumination levels arranged in three transverse zones in
said container so that the composition providing the highest light
illumination is placed at a terminal end and successive zones of
illuminant compositions are disposed thereafter in decreasing order
of light illumination
C. igniting means located adjacent to the composition having the
highest light illumination, and
D. gravitational retarding means attached to the flare container,
wherein the first zone adjacent to the igniting means is a
pyrotechnic composition of 65 percent Mg (125 .+-. 25 microns), 35
percent NaNO.sub.3 and 6 percent laminac 4116; the second zone is a
pyrotechnic composition of 70 percent Mg (200 .+-. 25 microns), 30
percent NaNO.sub.3 and 6 percent laminac 4116; and the third zone
is a pyrotechnic composition of 60 percent Mg (350 .+-. 50 microns)
40 percent NaNO.sub.3 and 6 percent laminac 4116.
Description
The invention described herein may be manufactured, used and
licensed by or for the Government for governmental purposes without
the payment to me of any royalties thereon.
Standard airdropped flares in the past have consisted of a
cylindrical flare pellet enclosed by a metallic or non-metallic
jacket with an igniter. This flare assembly was placed into
position over the target to be illuminated by artillery, mortar or
aircraft and employed some gravitational retarding means, such as a
parachute, wings or vanes, to elongate its suspension over the
target area. These flares were designed to burn with a constant
candle-power output and, since, even with retarding means, the
flare descended a considerable distance, the illumination on the
ground, which is proportional to the inverse square of the distance
of the flare to the ground, continually increased. As a result if
the target area below the flare was adequately illuminated at the
initiation of burning, upon descent of the flare the target was
illuminated far in excess of what was required. More commonly
however, the illumination at initiation was inadequate and only
after descent of the flare did the illumination become
adequate.
It is therefore an object of this invention to provide a flare
which will provide a nearly constant illumination on the ground
while in descent.
Yet another object is to provide an equally effective flare which
is lighter in weight than standard flares in present use.
A still further object of this invention is to provide an
incremental flare which is more efficient and economical than
standard flares in present use.
Other objects and many of the attendant advantages of this
invention will be readily appreciated as the same become better
understood by reference to the following description.
This invention relates to the design of a flare such that the flare
provides constant, adequate illumination on the ground throughout
its descent.
A preferred method of effecting the above consists of a standard
flare system wherein the flare pellet is made up of increments of a
standard flare composition, e.g. Mg/NaNO.sub.3 /laminac, and each
increment is varied by Mg particle size.
An illustrated example of a flare system utilizing an incremental
flare pellet can be seen in FIG. 1. In this Figure a flare
container 1 with standard igniting means 2 is incorporated with an
incremental flare pellet. A three increment type of pellet was
chosen as an example in this case. The first increment 3 may
contain as a fuel Mg with a particle size of 125 .+-. 25 microns,
the second increment 4, Mg of 200 .+-. 25 micron size and the third
increment 5, Mg of 350 .+-. 25 micron size.
By varying the particle size of the metallic fuel, the ratio of
fuel to oxidizer, the types of fuels and oxidizers, the burning
rate and candlepower may also be changed as the flare burns through
each increment while still maintaining its approximate luminous
efficiency in terms of candle-seconds per unit weight or volume.
Since the flare will be designed to ignite at a particular altitude
and descend at a known rate, the candlepower may be varied such
that the product of the candlepower divided by the square of the
distance of the flare from the ground is a constant. This constant
represents the illumination level on the ground.
Lastly, as a gravitational retarding means, a parachute 6 is shown
in FIG. 1.
Further, it has been found that when successive layers or zones of
illuminant composition are placed in the flare container in
parallel zones slanted to the vertical axis, a smoother change in
light intensity occurs as the flare burns from one increment to
another. Examples of a flare pellet embodying such slanted
increment design can be seen in FIGS. II and III. This type of
slanted loading is accomplished by means of punches whose faces are
slanted with reference to the vertical axis, i.e., a conical or
somewhat canted cylindrical punch.
Although it is not intended that the invention be limited thereto,
there is set forth herein below for the purposes of illustration
examples of how an incremental flare may be produced.
EXAMPLE I
THREE INCREMENT FLARE SYSTEM
Percent Metallic Fuel Nominal MATERIALS by weight particle size
Candlepower 100/200 mesh 1st Inc. Mg/NaNo.sub.3 / Laminac 4116*
65/35/6 125 .+-. 25 microns 500,000 50/100 mesh 2nd Inc.
Mg/NaNO.sub.3 / Laminac 4116 70/30/6 200 .+-. 25 microns 275,000
30/50 mesh 3rd Inc. Mg/NaNo.sub.3 / Laminac 4116 60/40/6 350.+-. 50
microns 100,000 *Polyester-Styrene resin (30% solution in styrene)
98.0% Methyl Ethyl Ketone in Dimethyl Phthalate 1.5% cobalt
Naphthenate 0.5%
The burn times chosen were based upon a 60 second total burn time
and a relatively constant descent velocity of the flare system. The
first increment has a nominal burn time of 16 seconds, the second
increment 19 seconds and the third increment 25 seconds. The
illumination on the ground produced by the above example may be
found by dividing the nominal candlepower of the particular
increment by the square of the height of the burning flare from the
ground.
EXAMPLE II
TWO INCREMENT FLARE SYSTEM
Percent Metallic Fuel Nominal MATERIALS by weight particle size
Candlepower 100/200 mesh 1st Inc. MgNaNO.sub.3 / Laminac 4116
65/35/6 125 .+-. 25 microns 500,000 20 parts 50/100 mesh 2nd Inc.
MgNaNO.sub.3 / Laminac 4116 60/40/6 200 .+-. 25 microns 165,000 20
parts 30/50 mesh 350 .+-. 25 microns
The burn times chosen were based upon a 60 second total burn time
and a relatively constant descent velocity. The first increment has
a nominal burn time of 25 seconds and the second increment, a
nominal burn time of 35 seconds.
A similar calculation to find the ground illumination may be made
as recited in Example I.
Various fuels, oxidizing agents, and binding agents known to the
art may be substituted for their analogues in Examples I and
II.
Fuels which may be used to advantage in place of the magnesium are
aluminum (and alloys thereof), titanium, charcoal, sulfur, silicon,
zirconium, calcium silicide, and metallic hydrides.
Oxidizing agents which may be selected include the nitrates of
barium, strontium, sodium and potassium, the perchlorates of
ammonium and potassium and the peroxides of barium, strontium and
lead.
Binding agents which may be substituted include polyvinyl chloride,
ethyl cellulose, metallic resinates, oils, waxes and asphaltum.
Found to be particularly effective were binding agents of polyester
and sulfur plastics which are polymerized in the pressed flare
candle and vinyl alcohol acetate resin.
The aforelisted illuminate type compositions are placed in any well
known type of flare container in order of highest light intensity
to lowest light intensity. The composition layer of highest
intensity is placed in the flare case such that it is in contact
with igniting means and will therefore burn first.
The successive layers or zones of illuminant composition are then
placed in the flare container in parallel zones slanted to the
vertical axis. This slanting effectuates a smoother change in light
intensity as the flare burns from one illuminant composition to
another. An example of this type of loading would be the use of a
cylindrical punch with a conical point to obtain conical mating
surfaces of the zones of various illuminant compositions
incrementally loaded into a cylindrical flare container.
The proportion of the volumes and compositions of the incremental
layers is selected in accordance with the burning time,
illumination level (ground), initial height and rate of descent
desired for the flare system.
Both igniting means and gravitational retarding means known to the
art may be used in the present invention.
I wish it to be understood that I do not desire to be limited to
the exact details and compositions described in this specification
for obvious modification will occur to a person skilled in the
art.
* * * * *