U.S. patent number 3,612,857 [Application Number 05/019,896] was granted by the patent office on 1971-10-12 for location marker for producing luminous display.
This patent grant is currently assigned to N/A. Invention is credited to Dave P. Beatty, James O. Reinhart.
United States Patent |
3,612,857 |
Beatty , et al. |
October 12, 1971 |
LOCATION MARKER FOR PRODUCING LUMINOUS DISPLAY
Abstract
A location marker having a first compartment containing at least
one cloth streamer saturated with a chemiluminescent material and
having a second compartment containing an activator composition for
activating the chemiluminescent material, said first and second
compartments being separated by a frangible barrier. A fuze section
is provided having first and second triggering means whereby said
first triggering means activates a gas-generating component to
cause said activator composition to rupture said frangible barrier
and saturate said at least one cloth streamer, and whereby said
second triggering means actuates a pyrotechnic delay train which,
in turn, ignites an explosive composition to eject said at least
one cloth streamer from its compartment.
Inventors: |
Beatty; Dave P. (Worthington,
IN), Reinhart; James O. (Bloomfield, IN) |
Assignee: |
N/A (N/A)
|
Family
ID: |
21795619 |
Appl.
No.: |
05/019,896 |
Filed: |
March 16, 1970 |
Current U.S.
Class: |
362/34; 116/209;
362/458; 102/342; 252/700 |
Current CPC
Class: |
F42B
12/40 (20130101); F21K 5/00 (20130101) |
Current International
Class: |
F21K
5/00 (20060101); F42B 12/02 (20060101); F42B
12/40 (20060101); F21v 009/16 () |
Field of
Search: |
;102/37.8,37.6,60,87
;240/2.25 ;116/124B |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Stahl; Robert F.
Claims
We claim:
1. A location marker comprising,
a tubular container,
at least one strip of cloth saturated with chemiluminescent
material in one end of said container,
a piston housing slidably mounted in said tubular container having
a fluid compartment and a piston slidably mounted in said fluid
compartment,
a quantity of activator fluid in said fluid compartment,
a frangible barrier closing one end of said fluid compartment,
means for slidably moving said piston in said piston housing
whereby movement of said piston causes said frangible barrier to
break and saturate said at least one strip of cloth with activator
fluid, and
means for slidably moving said piston housing whereby movement of
said piston housing ejects said at least one strip of cloth.
2. A location marker as set forth in claim 1, wherein said at least
one strip of cloth is saturated with chemiluminescent material
comprised of 0.2 molar bis (2, 4, 5-trichloro-6-carbobutoxyhyenyl)
oxalate, 0.003 molar 9, 10-bis (phenylethynyl) anthracene, 1
percent cyanacryl terpolymer, and 2 percent bis-(2-ethylhexyl)
phthalate in benzene and wherein said activator fluid is comprised
of 1.5 molar hydrogen peroxide in dimethyl phthalate.
3. A location marker as set forth in claim 1, wherein said means
for slidably moving said piston includes a first firing pin, a
primer, and a gas-generating pellet whereby triggering of said
firing pin detonates said primer and ignites said gas-generating
pellet and gas from same pellet moves said piston to rupture said
frangible barrier whereby said at least one strip of cloth
saturated with chemiluminescent material is activated by said
activator fluid.
4. A location marker as set forth in claim 3, wherein said means
for slidably moving said piston housing comprises a second firing
pin, a primer, a pyrotechnic delay train, and an explosive pellet
whereby detonation of said explosive pellet after said
gas-generating pellet is ignited ejects said at least one strip of
cloth.
5. A location marker as set forth in claim 4, wherein said first
and second firing pins are maintained in a cocked position by a
bore rider pin having means for preventing triggering of said
firing pins while said location marker is within a launching tube.
Description
STATEMENT OF GOVERNMENT INTEREST
The invention described herein may be manufactured and used by or
for the Government of the United States of America for governmental
purposes without the payment of any royalties thereon or
therefor.
BACKGROUND OF THE INVENTION
The present invention relates to a location marker and more
particularly to a location marker which can be launched from an
aircraft and, when deployed on the ground, will emit a luminous
display which can be seen at night by aircraft personnel.
Various devices are presently being employed to mark ground or sea
locations by dropping, or launching, markers from aircraft. In
general, these devices serve either to locate friendly personnel
who might be in need of rescue or to locate enemy troop or supply
location for future destruction. Frequently, a spot in the ocean is
to be marked, such as for spotting submarines, and many of these
locating device utilize the water environment to activate a smoke-
or flame-producing composition. For example, one marine location
marker employed during night operation by the U.S. Navy consists of
a steel can containing a main charge of calcium carbide in its
bottom inner section and a centrally located tube containing a
smaller charge of calcium phosphide. The reaction of these
chemicals with sea water produces acetylene and phosphine.
Phosphine ignites spontaneously within 70 seconds after water
enters the marker. The burning phosphine ignites the acetylene as
it escapes from the can and a flame about 9 inches high is
produced.
Another marine location marker which is used to produce both flame
and smoke contains red phosphorous. Ignition is accomplished by
electrical current supplied by a sea-water-activated battery. When
sea water enters the battery cavity in the base assembly, the sea
water acts as a electrolyte in the battery causing sufficient
electrical current to be produced to initiate an electric squib
which, in turn, ignites a starter mix and red phosphorus. Gases of
combustion force a valve body out of the nose of the location
marker thereby allowing yellow flame and white smoke to be emitted.
A marker containing 784 grams of red phosphorus will burn between
13 and 19 minutes.
Still another type of location marker employed in a water
environment is one containing a fluorescein dye which is expelled
by an explosive charge to spread dye on the water. This marker is
designed to be launched either from surface craft or aircraft to
produce a daylight reference on the ocean's surface in the form of
a dye slick which is used in antisubmarine warfare or as a distress
signal in search and rescue operations. Unless the sea is extremely
rough, these dye slick markers normally provide a marker which
lasts substantially longer than the burning-type markers.
Smoke and flame producing markers are also employed by the military
for locating and marking ground areas. Instead, of sea water being
used as an initiating agent, however, various mechanical and
chemical means are utilized to ignite a pyrotechnic composition
which burns to produce a signal.
SUMMARY OF THE INVENTION
The present invention relates to a location marker having a first
compartment for holding one or more cloth streamers which are
saturated with a chemiluminescent material. A second compartment is
provided for holding a liquid activator composition and the first
and second compartments are separated by a frangible barrier, such
as a glass disk. A fuze section is provided adjacent the second
compartment and contains first and second firing pins. These firing
pins are maintained in a cocked position by a bore rider pin which
prevents actuation of the firing pins until the location marker has
cleared its launching tube. A gas generator pellet is provided in
the fuze section and, upon actuation of the firing pins, the gas
generator pellet is ignited and gas therefrom moves a piston which
injects the liquid activator composition into the first compartment
containing one or more cloth streamers. An ejection pellet is also
provided in the fuze section and, upon ignition of the ejection
pellet, the cloth streamers are ejected from their compartment. The
cloth streamers fall to the ground and provide a highly effective
location marker which is visible from 5 miles for about 15
minutes.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a longitudinal sectional view of a preferred embodiment
of the present invention;
FIG. 2 is a partial sectional view showing a location marker in a
launching tube;
FIG. 3 is a partial sectional view showing a location marker
leaving a launching tube;
FIG. 4 is a sectional view showing the preferred embodiment in a
fired condition;
FIG. 5 is a sectional view showing cloth streamers being ejected
from a compartment;
FIG. 6 is an enlarged view of a firing pin; and
FIG. 7 is a diagrammatic view showing cloth streamers after landing
in a target area.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring first to FIG. 1 of the drawing, there is shown a
cylindrical container 11 that has one end crimped to a fuze section
12 and the other end crimped to an end cap 13. End cap 13 is
provided with an opening 14 through which fluid can pass, and
opening 14 is closed by a threaded plug 15 which attaches to end
cap 13. A piston housing 16 is slidably positioned inside container
11 and has a cavity for holding fluid. A distribution pipe 17,
having a plurality of holes 18 therein, is attached to one end of
piston housing 16 and a frangible barrier 19, such as a glass disk,
is provided to retain fluid within the cavity of piston housing 16.
A piston 21 is slidably positioned in the cavity of piston housing
16. An ejection cylinder 22, which is split into two halves, is
positioned inside container 11 between one end of piston housing 16
and the inner end of end cap 13, and movement of piston housing 16
causes end cap 13 to be separated from container 11.
One or more cloth streamers 23 are placed within container 11 and
streamers 23 are saturated with a chemiluminescent fluid which can
be introduced into container 11 through opening 14 in end cap 13.
By way of example, chemiluminescent fluid might be comprised of 0.2
molar bis (2, 4, 5-trichloro-6-carbobutoxyheyenyl) oxalate, 0.003
molar 9, 10-bis (phenylethynyl) anthracene, 1 percent cyanacryl
terpolymer, and 2 percent bis-(2-ethylhexyl) phthalate in benzene.
A suitable activator fluid 24, which is retained in the cavity of
piston housing 16, might be 1.5 molar hydrogen peroxide in dimethyl
phthalate.
Firing pins 25 and 26 are slidably positioned in fuze section 12
and are maintained in a cocked positioned by a bore rider pin 27.
The driving force for each firing pin is supplied by a separate
firing pin spring 30. As best shown in FIG. 6 of the drawings, each
firing pin is provided with a tang 28, a bore 29 and a slot 31.
Bore rider pin 27 is provided with three enlarged diameter sections
32, 33, and 34 and a head 35. Enlarged diameter section 32 is
slidably engageable in bore 29 of firing pin 25 and enlarged
diameter section 33 is slidably engageable in bore 29 of firing pin
26 and, when so engaged, firing pins 25 and 26 are held in a cocked
position. Spring 36 is provided as a driving force to move bore
rider pin 27 out of fuze section 12, however, during a cocked
condition, pneumatic button 37 engages the end of enlarged diameter
section 34 to prevent movement of bore rider pin 27 and release of
firing pins 25 and 26. Spring 38 is provided to maintain pneumatic
button 37 in engagement with enlarged diameter section 34.
Primers 41 and 42 are provided in fuze section 12 and are in line
to be struck by firing pins 25 and 26, respectively. A
gas-generating pellet 43, which is to be ignited by primer 42, is
provided to produce gas for driving piston 21 and an ejection
pellet 44 is provided to produce an explosive force for driving
piston housing 16 and ejecting streamers 23. By way of example,
gas-generating pellet 43 might be comprised by a mixture of
magnesium and Teflon that is pressed into a pellet, and ejection
pellet 44 might be black powder. Delay pellets 45 are positioned
between primer 41 and ejection pellet 44 to delay ejection of
streamers 23 for sufficient time to permit activator component to
pass through holes 18 in distribution pipe 17.
As one method of launching the marker of the present invention is
by compressed air, a sealing ring 46 of resilient material is
provided around the outer periphery of fuze section 12 to prevent
excessive leakage of air between the outer perimeter of the marker
and the inner surface of a launching tube 47. As dropping the
marker could cause movement of pneumatic button 37 and accidental
release of bore rider pin 27, a safety cap 48 is provided around
the end of fuze section 12 and locked thereto by retaining ring
49.
OPERATION
After the location marker of the present invention is assembled as
shown in FIG. 1 of the drawings with streamers 23 therein,
chemiluminescent fluid is added through orifice 14 of end cap 13 to
saturate cloth streamers 23. Immediately prior to launching,
retaining ring 49 and safety cap 48 are removed.
Upon launching in launching tube 47, the propelling force, such as
that of an explosion, or compressed air, causes pneumatic button 37
to move inwardly thereby compressing spring 38 and freeing, or
releasing, bore pin 27. Spring 36 moves bore rider pin 27 against
the inner bore of launcher 47, but as shown in FIG. 2 of the
drawing, the movement of pin 27 is insufficient to release firing
pins 25 and 26. Upon location marker clearing launching tube 47,
spring 36 moves pin 27 outwardly and releases firing pins 25 and 26
and their respective firing pin springs 30 drive firing pins 25 and
26 forwardly and detonate primers 41 and 42, respectively.
As best shown in FIG. 4 of the drawings, primer 41 ignites gas
generating pellet 43 and the gas pressure therefrom drives piston
21 forwardly causing fluid 24 to break frangible barrier 19. As
piston 21 continues to move forwardly, fluid 24 is forced through
distribution pipe 17 and holes 18 to saturate streamers 23 and
activate the chemiluminescent fluid which has been absorbed by
streamers 23. Primer 41 is detonated simultaneously with primer 42,
and primer 41 ignites delay elements 45 which, in turn, detonate
ejection pellet 44. By way of example, delay elements 45 might be
designed to ignite ejection pellet 44 about 8 seconds after
gas-generating pellet 43. This delay allows fluid 24 to pass
through holes 18 and saturate streamers 23 and also allows a free
fall of the location marker before expellent charge 44 ejects
streamers 23.
Referring now to FIG. 5 of the drawings, explosive charge 44 is
shown being detonated and piston housing 16 is moving outwardly
from fuze section 12. Piston housing 16 moves ejection cylinder 22
against end cap 13 and end cap 13 is separated from container 11.
As piston housing 16 continues to move forwardly, ejection cylinder
22 continues to separate from container 11. When the rearward end
of ejection cylinder 22 clears the end of container 11, the two
halves of ejection cylinder 22 separate and fall away. To
facilitate separation of streamers 23, a small drogue parachute 51
may be provided to one end of each streamer 23. Also, if desired,
the other end of each streamer 23 may be fastened to either
container 11 or piston housing 16 to provide a weight so that
streamers 23 may be more accurately deployed. Without such a
weight, streamers 23 would be highly susceptible to wind and their
location could not be accurately placed by dropping from an
aircraft. FIG. 7 of the drawings shows a pair of streamers 23 lying
on the ground and emitting a colored glow that can be seen at night
from searching aircraft.
* * * * *