U.S. patent number 3,613,583 [Application Number 04/821,596] was granted by the patent office on 1971-10-19 for altitude-compensated hybrid infrared flares.
Invention is credited to William Lai, John C. Trowbridge.
United States Patent |
3,613,583 |
Lai , et al. |
October 19, 1971 |
ALTITUDE-COMPENSATED HYBRID INFRARED FLARES
Abstract
A hybrid infrared flare is ignited by first igniting a
methane-oxidizer mixture with a spark which in turn ignites the
fuel grain. Burning is sustained by a continuous flow of oxidizer
through the upstream oxidizer injector. Oxidizer is also supplied
at the downstream end of the flare to provide an oxidizer sheath
around the exhaust flame so that the oxidizer mixes with the
fuel-rich exhaust products of the flare to enhance the infrared
output regardless of the altitude at which the flare is located.
Nitrogen is supplied at the upstream end of the flare to quence
combustion between burns when the flares are used in multistart
operation.
Inventors: |
Lai; William (Los Altos,
CA), Trowbridge; John C. (Saratoga, CA) |
Assignee: |
|
Family
ID: |
25233791 |
Appl.
No.: |
04/821,596 |
Filed: |
May 5, 1969 |
Current U.S.
Class: |
102/336; 60/264;
102/356; 60/251 |
Current CPC
Class: |
F42B
4/26 (20130101) |
Current International
Class: |
F42B
4/00 (20060101); F42B 4/26 (20060101); C06d
001/10 () |
Field of
Search: |
;60/220,264,251,261,35.6RS ;102/37.8,35 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Stahl; Robert F.
Claims
We claim:
1. A hybrid infrared flare comprising a fuel grain having a hollow
central port, a first oxidizer injector at one end of said fuel
grain; means for supplying an oxidizer to said first oxidizer
injector; means for supplying a small amount of fuel to said first
injector; means for igniting the fuel and oxidizer within said
first injector to thereby ignite the fuel grain which burns with
the oxidizer to form an exhaust flame at the end of said port
remote from the first injector; means, at the other end of said
fuel grain, for providing an oxidizer sheath around the exhaust
flame of said flare and means for supplying nitrogen to said first
injector for quenching the combustion a predetermined time after
combustion is initiated.
Description
BACKGROUND OF THE INVENTION
Hybrid flares depend upon afterburning of the fuel-rich exhaust for
enhancement of infrared output. Fuel-rich exhaust operation makes
the hybrid flares altitude sensitive since afterburning in the
atmosphere is altitude dependent because of rarefied conditions at
higher altitudes.
SUMMARY OF THE INVENTION
According to the invention, an oxidizer is injected downstream of
the flares to provide an oxidizer sheath around the flare exhaust
flame so that the oxidizer mixes with the fuel-rich exhaust
products to provide the afterburn, thus compensating for altitude
sensitivity induced by rarefied ambient conditions at higher
altitudes. Nitrogen may be supplied at the forward end of the flare
to quench the combustion at the end of a burn, when the flares are
used in multistart operation.
IN THE DRAWING
FIG. 1 is a schematic diagram of a hybrid flare according to the
invention;
FIG. 2 shows one possible operating sequence for the flare of FIG.
1; and
FIG. 3 is a schematic of a programmer which may be used with the
device of FIG. 1.
DETAILED DESCRIPTION OF THE INVENTION
Reference is now made to FIG. 1 of the drawing wherein reference
number 10 shows an infrared flare having a fuel grain 12 with a
central port 13 which is located within a support housing 14 made
of a material such as aluminum. The fuel grain may be made of a
material such as carboxy-terminated polybutadiene.
An oxidizer such as oxygen or hydrogen peroxide from supply 16 and
a fuel such as methane from fuel supply 18 are supplied to the
upstream injector 19 under the control of solenoid valves 20 and 21
in lines 22 and 23, respectively. A spark igniter 24 ignites the
fuel and oxidizer which, in turn, ignites the fuel grain 12. To
make the flare substantially altitude insensitive, oxidizer is also
supplied to downstream injector 26. The injector 26 is an annular
manifold with an annular nozzle in the form of a slit or holes to
provide a sheath of oxidizer 27 around the exhaust flame 28. The
manifold 26 is supplied with oxidizer from supply 16 through
solenoid valve 30 and conduits 32. A separate oxidizer supply may
be provided for supplying a different oxidizer such as dinitrogen
tetroxide to the manifold 26 if desired. Mass flow control of the
fuel and oxidizer is provided by means of conventional sonic chokes
33. The sequence of operation is controlled by sequence programmer
34. One type of programmer which may be used is shown in FIG. 3,
wherein cam-operated switches S.sub.1, S.sub.2, S.sub.3, and
S.sub.4 act to control the operation of solenoid valves 37, 21, 20,
and 30, respectively. When the motor 35 starts, switches S.sub.2,
S.sub.3, S.sub.4, and S.sub.5 are closed to energize solenoids 20,
21, and 30 and to energize the spark igniter 24 from the ignition
circuit 38. The motor may be started either by a ground signal to
the motor control 39, or the motor control 39 may include a timer
to start the motor a predetermined time after the flare is
launched. The flare launching system forms no part of this
invention and therefore is not shown. The motor control could also
include a timer to restart the motor 35 at predetermined intervals.
Switch S.sub.6 may be used to stop the motor after one sequence of
operation or the stop signal could come from a ground control
signal or from the timer within motor control 39. The sequence
programmer shown is only for illustration purposes and it is to be
understood that any programmer may be used that provides the
desired operation, for example, the series 60 solid-state
sequential programmer, by Tempo Instruments, Inc. may be used.
Nitrogen from supply 36 may be supplied through the methane line 23
to the upstream injector 19 through solenoid valve 37 to quench the
combustion between burns for multistart operation.
In one possible sequence of operation as shown FIG. 2, the motor 35
is started in a manner indicated above. At time T.sub.0 the
solenoid valves 20 and 21 are energized to supply oxidizer and
methane to the upstream injector and at the same time the igniter
is energized to ignite the fuel which, in turn, ignites the fuel
grain. The oxidizer continues to flow, after the methane fuel stops
flowing, to support burning of the fuel grain. Also at T.sub.0,
oxidizer is supplied to the downstream injector 26 and continues
for the full period of the burn. The oxidizer from injector 26
provides an oxidizer sheath around the exhaust flame 28 to support
afterburning of the fuel-rich mixture at all altitudes. At the end
of the desired burn the oxidizer is shut off and nitrogen is
supplied to the upstream injector to quench combustion within the
fuel grain port.
The operating sequence given is merely illustrative as other
operating sequences may be used, for example, an altitude sensor
operating a second solenoid valve could be provided in series with
valve 30 to permit a flow of oxidizer from the downstream injectors
only above a certain predetermined altitude.
There is thus provided a hybrid infrared flare in which the
afterburn is substantially altitude insensitive.
* * * * *