US3771731A - Mechanically modulated combustion heated infrared radiation source - Google Patents

Mechanically modulated combustion heated infrared radiation source Download PDF

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US3771731A
US3771731A US00282523A US3771731DA US3771731A US 3771731 A US3771731 A US 3771731A US 00282523 A US00282523 A US 00282523A US 3771731D A US3771731D A US 3771731DA US 3771731 A US3771731 A US 3771731A
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recited
combustion chamber
window
blades
combustion
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H Dyner
J Hill
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Lockheed Corp
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Sanders Associates Inc
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J61/00Gas-discharge or vapour-discharge lamps
    • H01J61/84Lamps with discharge constricted by high pressure
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J61/00Gas-discharge or vapour-discharge lamps
    • H01J61/92Lamps with more than one main discharge path
    • H01J61/94Paths producing light of different wavelengths, e.g. for simulating daylight

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  • the present invention relates generally to the field of infrared radiation sources and more particularly to a new and novel combustion heated infrared radiation source having a mechanical modulation means.
  • FIG. 1 is a schematic cross-sectional view of a com-
  • FIG. 2 is a schematic elevation view of a rotating shutter modulator suitable for use with the radiation source of FIG. 1.
  • FIG. 3 is a schematic cross-sectional view of a mechanically modulated combustion heated infrared radiation source particularly adapted for use in a mobile application.
  • FIG. 4 is a schematic block diagram of a complete amplitude modulated infrared transmitter incorporating the apparatus of the present invention.
  • FIG. 1 there is schematically illustrated in cross section simplified combustion heated infrared radiation source in accordance with the present invention.
  • the source comprises a high temperature combustion chamber 10 formed of a high emissivity material and closed at one end by a window 12 which is transparent to radiation over a preselected spectral range.
  • Fuel is introduced into the combustion chamber 10 via a burner orifice 14 preferably in a direction relative to the combustion chamber 10 such that rapid mixing and'combustion are achieved.
  • the window 12 is in direct contact with the hot combustion gases it is preferred that the oxygen or air necessary to support combustion of the fuel be introduced at a low tempera v ture through a thin cylindrical slit 16 in the source facefrom the hot combustion gases is maximized and the practice of the present-invention.
  • combustion chamber walls thus comprise the infrared radiating surface.
  • exhaust cooling air is introduced through ducts 26 to an exhaust gas mixing chamber 28.
  • the exhaust products are thus cooled to a desired temperature determined by the mixture ratio of air to combustion products.
  • zirconium oxide are. particularly useful in the fabrication of the combustion chamberalthough any material capable of withstanding the high combustion temperatures is acceptable in the practice of the invention. It is preferred that the combustion chamber be laid up on a mandrel with zirconium oxide yarn and impregnated with a zirconium oxide cast in a similar manner to that employed with glass-reinforced resin plastics. In this way complex shapes optimized to withstand thermal shock may be easily fabricated.
  • a fuel providing as high a flame temperature as possible be employed, however, considerations such as fuel availability and toxicity are factors bearing on practical choices.
  • the temperature of an oxy-acetylene flame is 3,360 K and thus acetylene would be a desirable fuel.
  • This fuel is, however, explosive and in some applications, particularly those which are mobile, it is necessary to dissolve the acetylene in acetone which increases the storage weight per pound of usefuel fuel.
  • a relatively new fuel is the so called MAPP gas, a mixture of Methyl acetylene, Allene, Propane and Propylene. This is more stable than acetylene and thus may be stored as a liquid under its own vapor pressure without danger of explosion.
  • Another readily available fuel is liquid propane.
  • an operating temperature for the radiation source of FIG. 1 may be made based upon minimum specific fuel consumption consistent with minimum source size and optical aperture.
  • an operating temperature of 2,400" K for a propane fired device requires a combustion chamber diameter of 1.0 inch.
  • Propane consumption was found to be 0.58 pounds/hour and oxygen consumption 2.1 l pounds/hour.
  • the device thus fabricated produced a total radiation output of 325 watts.
  • FIG. 2 schematically illustrates a rotatingshutter mechanical modulator which is useful in combination with the radiation source of FIG. 1 in the practice of the present invention.
  • This modulator comprises at least one bank of continuously rotatable blades 30 each mounted between mounting brackets 32 in bearing assemblies 34.
  • the blades 30 are driven in rotation by a motor 36 through an output gear 38 and reduction gear 40.
  • Adjacent blades are driven in opposite directions by the train of substantially identical gears 42.
  • the motor 36 also drives gear 44 which is coupled by shaft 46 to a gear train substantially identical to that illustrated at 42 and 44 but disposed on the outside of the opposite mounting bracket 32.
  • the bearing assemblies 34 may be slightly preloaded thus placing the-blades 30 under some tension. It has been found by the Applicants that a typical size motor developing 0.5 in-oz of torque at 24,000 rpm and 0.8 in-oz of stall torque is adequate to drive a bank of nine blades 0.315 inch wide disposed on 0.300 inch centers.
  • the bearing assemblies 34 are of standard commercially available type and the gears may be for example standard pressure angle gears. It will be readily apparent that any of a wide variety of bearing assemblies and gears suitable to meet a given modulation frequency requirement could be used.
  • FIG. 2 Also illustrated in FIG. 2 is a second drive motor 46 and an associated gear train 48 identical, to that associated with blades 30 and discussed above.
  • This second motor 46 and gear train 48 are operative to drive a second bank of rotatable blades (obscured by blades 30 and thus not shown).
  • drive motor 36 may be operated at a constant speed and thus blades 30 modulate the output radiation at some preselected fixed frequency.
  • the second drive motor 46 may be variable in speed and operate to drive the second bank of shutter blades such as to amplitude modulate the fixed frequency radiation.
  • To achieve the radiating cavity 60 is a circular.
  • the inner wall 62 includes a plurality of flow passages 66 for the hot combustion gases to pass from the combustion chamber into the space 68 between the walls 62 and 64 and through a sonic exhaust nozzle 70 at the base of the radiation source.
  • a third or outer layer 76 of very high insulating efficiency but low temperature capacity insulation such as MIN-K a very low conductivity insulating material of utility at temperatures less than l,200 'K and commercially available from the Johns-Man'ville Co. may be used if necessary ordesired.
  • the insulated radiating cavity is disposed in a case structure 78 which is provided with a plurality of longitudinal heat exchange fins 80.
  • the radiating cavity 60 is closed at its output end by a window 82 which is transparent over the output wavelength range of interest.
  • a quartz window would be a logical choice based upon low cost and optimum resistance to thermal shock. Obviously, other window materials would be preferred for other regions of the spectrum.
  • the oxygen or air necessary to support combustion withinthe cavity 60 is introduced via an oxygen supply line 84 into a cylindrical slit 86 at the periphery of the window 82. The cold oxygen thus passes over the window 82 and serves to keep the window temperature within acceptable limits.
  • the fuel is introduced through fuel supply line 88 to a small orifice 90 disposed tangentially to the inner wall 62 of the radiating cavity 60.
  • propane is a desirable fuel in accordance with the fuel selection criteria discussed above with reference to FIG. 1.
  • the simplest ignition system of utility in the practice of the present invention is an electrical spark generated by discharging a condenser across a spark gap.
  • copper electrodes 92 and 94 are inserted into the radiation cavity 60 through a high temperature gasket 96 such as a replaceable zirconium oxide insert.
  • the electrodes 92 and 9,4 are coupled at their opposite ends through the housing structure 78 to an electrical connector block 98 of the type known in the art andthe interm] details-of which are thus notspecifically illustrated.
  • Radiation from the heated cavity wall 62 is passed by window 82 and mechanically modulated by a rotating shutter modulator 100 as described with reference to FIG. 2.
  • the electrical coupling to the modulator drive motor(s) is illustrated schematically at 102.
  • a reflective light funnel 104 of any preselected geometry may be used at the output side of the modulator 100 to provide a particular spatial distribution of the modulated output energy.
  • a plurality of heat exchanging fins 106 may also be disposed about the circumference of the light funnel 104. Additionally if required in a given application a suitable filter 108 may be disposed over the light funnel 104 output aperture.
  • Cooling of the radiation source in the mobile environment is provided by ducted air.
  • the exhaust gases issue from the-exhaust nozzle 70 into a mixing chamber 110 formed as a part' of the housing structure 78.
  • a layer 112 of high temperature resistance material may be placed opposite the nozzle 70. Cooling air is admitted via opening 114 in the mixing chamber 110, mixed with the hot exhaust gases and vented to the environment by means of coupling 116. It has been found that the exhaust gases from a propane fired radiation source may be reduced to a temperature of lessthan 250 F by mixing with ram'air at a mass ratio of about 35.
  • Cooling air is also admitted via airscoops 118 which are formed as a part of an outer shroud 120-. This air passes over the heat exchange fins 106 on light funnel '104, pastthe drive motors of modulator 100 and over the longitudinal heat exchange fins 80 on the housing structure 78. This air may be vented to the environment either directly or via the vent coupling 116.
  • a thermal switch 121 may be disposed in the exhaust mixing chamber 110 to continuously monitor the exhaust gas temperature. If, for example, the exhaust gas temperature has not risen to a preselected level within a given period of time after an ignition spark across the electrodes 92 and 94 a reignition sequence may be initiated in the manner'to be described hereinbelow.
  • a second thermal switch 122 may be diposed at any convenient positionnear the output window 82. In the event that the window were to break combustion gases would'quickly enter the optical cavity with an attendant temperature rise. Thus the rise in temperature may be used to initiate a shut-off sequence to be prescombustion heated infrared radiation transmitter in accordance with the principles of the present invention.
  • the radiating cavity combustion chamber 124 is coupled by supply lines 126 and 128 to an oxygen and fuel supplies 130 and 132 respectively; each supply line Combustion of the fuel heats the combustion chamber 124 which radiates the infrared. This radiation passes through the combustion chamber window 138 and is modulated by the above-described mechanical modulator 140.
  • the modulator drive motors 142 are driven by any suitable power source 144'.
  • the combustion products are coupled from the combustion chamber 124 to the exhaust mixing chamber 146 where they are mixed with cooling air which is provided via air intake 148.
  • the cooled gases are vented to the environment via exhaust coupling 150.
  • the ignition spark gap 152 is coupled via control logic 154 to the power source 144.
  • the control logic .154 also receives an inputs the electrical signals from the exhaust gas temperature sensor 156, optics temperature sensor 158, and starting means 160.
  • an initial starting signal applied from the starting means 160 to the control logic 154 serves to apply power from source 144 to the modulator drive motors and to initiate the ignition sequence.
  • This sequence includes charging of the ignition capacitor 162 and opening the solenoid valves 134 and 136 in the oxygen and fuel supply lines 126 and 128 respectively. Once the ignition capacitor 162 is fully charged it is discharged across the spark gap 142 in the combustion chamber 124. Assuming proper ignition the temperature of the exhaust gases in the exhaust mixing chamber will rise quickly to an operating level.
  • the exhaust gas temperature'sensor 156 will so indicate and the ignition sequence may be repeated. In such cases the oxygen and fuel solenoid valves 134 and 136 are closed for a period sufficient to vent any combustible gases from the combustion chamber 124, and the above-described ignition sequence repeated. If desired a predetermined number of unsuccessful ignition attempts may serve as the criterion for inactivating the entire system. An automatic inactivation sequence may also be initiated if the optics temperaturesensor 158 detects the conditions indicative of a broken window 138. In such event I the oxygen and fuel solenoid valves 134 and 136 would being provided with a solenoid valve 134 and 136.
  • supply 130 may be a tank of liquid oxygen or could be a chemicaloxygen generator whereby oxygen ,is generated chemically from sodium chlorate. Such be closed andpower removed from themodulator drive motors 142.
  • a combustion heated source of modulated radiant energy comprising a combustion chamber formed of awhen heated emit radiant energy, a window substantially transparent to said radiant energy closing or end of said combustion chamber, means for introducing a combustible mixture into said combustion chamber, j means for igniting said mixture such that said fuel is burned whereby said combustion chamber is heated and radiant energy is emitted through said window, i
  • m aterial which i means for exhausting the combustion products from said combustion chamber
  • Apparatus as recited in claim 1 further including means for cooling said window.
  • Apparatus as recited in claim 2 wherein said means for introducing a combustible mixture into said combustion chamber includes means for introducing an oxidizing agent into said combustion chamber and means for introducing a combustible fuel into said combustion chamber such that said oxidizing agent and fuel are mixed together.
  • said mechanical radiant energy modulator includes a first-plurality of blades mounted for rotation about a like first plurality of parallel axes disposed in substantially a single first plane adjacent the exterior surface of said window each axis separated from adjacent axes by a distance comparable to the width of said blades, and
  • combustion chamber is a crucible having an inner and outer wall.
  • combustion chamber is a'double-wa'll circular cone having an exhaust passage between said walls and the inner wall having a plurality of apertures therethrough, said exhaust passage terminating in an exhaust nozzle at the end of said combustion chamber opposite said window.
  • Apparatus as recited in claim 1 further including means for cooling said combustion products as they are exhausted from said combustion chamber.
  • combustion products cooling means comprises an exhaust mixing chamber into which said combustion products are introduced, and means'for introducing cooling air into said exhaust mixing chamber at a selected mass ratio to saidcombustion products.
  • said window is formed of quartz.
  • said fuel introducing means comprises a pressurized container of combustible gas, and a fuel supply line in communication at one end with said container and at the other end with said combustion chamber.
  • oxidizing agent introducing means comprises a supply of pressurized oxygen, and an oxygen supply line in communication at one end with said oxygen supply and at the other end with said combustion chamber.
  • Apparatus as recited in claim 18 wherein said supply of pressurized oxygen comprises a chemical oxygen generator.
  • Apparatus as recited in claim 17 furtherincluding a cylindrical slit disposed in said combustion chamber circumferentially abutting said window at the periphery of theinterior surface thereof, said slit being in circumferential communication with said combustion chamber, and said oxidizing agent being introduced into said slit such that said window is cooled thereby and maintained within a preselected temperature limit.
  • igniting means comprises a pair of electrodes inserted into said combustion chamber at the end thereof opposite said window, and means for generating an electrical spark across said electrodes.
  • Apparatus as recited in claim 5 further including a second plurality of blades mounted for rotation about a like second plurality of parallel axes disposed in substantially a single second plane adjacent and parallel to the plane of said'first plurality of blades, each axis of said second'plurality of blades separated from adjacent axes by a distance comparable to the width of said blades, and
  • Apparatus as recited in claim 1 further including a light'funnel disposed adjacent said mechanical radiant energy modulator and having a configuration selected to provide a predetermined spatial distribution of said modulated radiant energy.
  • Apparatus as recited in claim 24 further including a passband filter disposed over the output end of said light funnel.
  • Apparatus as recited in claim 24 further including heat exchanging fins disposed in heat. transfer relation to said light funnel, and
  • a temperature sensor disposed in proximity to said combustion products exhausting means and coupled to said interrupting means such that a temperature below a preselected level produces an output from said temperature sensor which is operative to activate said interrupting means.

Abstract

A combustion chamber is closed at one end by a highly transparent window. A volatile gas and oxygen are introduced into the combustion chamber. After ignition the gaseous flame heats the combustion chamber to a temperature slightly below the melting point of the chamber. Infrared radiation emitted by the heated combustion chamber walls and passing through the window is mechanically modulated by one or more motor driven shutters.

Description

United States Patent 1 9 [111 3,771,731
Dynervetal. Nov. 13, 1973 MECHANICALLY MODULATED [56] References Cited COMBUSTION HEATED INFRARED UNITED T ES PATENTS RADIATION SOURCE 3,219,827 11/1965 Pittinger 250/85 x [75] inventors: Harry B. Dyner, Newton Centre; $031k et al....l 550%;
c uneeta. 50 322 A Lmwln both of 2,952,762 9/1960 Williams et a1. i 250/85 3,419,709 12/1968 Bell 250/85 X Asgignee; Sanders Associates Inc. Nashua 3,049,962 8/1962 Denecke 240/46.07 X
Primary Examiner-Richard L. Moses [22] Flled' 1972 Attorney-Louis Etlinger [21] Appl. No.: 282,523
- Related U.S. Application Data E b h F d t d b com usloncam er 1s cose a one en ya [63] 5532: 25 of 1970 highly transparent window. A volatile gas and oxygen are introduced into the combustion chamber. After ignition the/gaseous flame heats the combustion cham- [52] ;2 7 her to a temperature slightly below the melting point [51] Int Cl Fzlm of the chamber. Infrared radiation emitted by .the [58] Fieid 2 A heated combustion chamber walls and passing through 240/1 R 1 M 46 07 46 431/356 the window is mechanically modulated by one or more 5 219/354: motor driven shutters.
- 29 Claims, 4 Drawing Figures EXHAUST 3371.731 SHEET 20$ 4 AGENT HARRY B. DYNER JACQUES AF. HILL INVENTORS By 6% a, 7
PATENTEU NEW 1 3 I975 FIG.2
PATENTEDRBY 13 mm 3771; 731
SHEET 30F 4 EXHAUST F|G.3
INVENTORS HARRY B. DYNER JACQUES AF. HILL By A AGENT PATENTEDNUV I 3 I975 3771. 731
SHEET I CF 4 Z EXHAUST MIxER 7l; I46 I56 I30 I I34 I26 '3 OXYGEN L35 I36 FUEL SUPPLY SUPPLY COMBUSTION CHAMBER I40 I l l l l I IGNITE- |42 CAPAC. MODULATOR I44 I54 DRIVE k I MOTORS POWER CONTROL I SOURCE LOGIC START MEANS FIG. 4
INVENTORS HARRY B. DYNER JACQUES A. F. H ILL AGENT MECHANICALLY MODULATED COMBUSTION HEATED INFRARED RADIATION SOURCE This is a continuation, of US. Pat. application Ser. No. 85,065,'filed Oct. 29, 1970 now abandoned.
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates generally to the field of infrared radiation sources and more particularly to a new and novel combustion heated infrared radiation source having a mechanical modulation means.
2. Description of the Prior Art Prior to the present invention the primary sources of infrared radiation have been the electrically powered blackbody and the arc lamp. The primarydrawback with such devices has been their inefficient use of relatively high levels of electrical input power. In some applications where electrical power is at a premium this inefficiency becomes prohibitive. Furthermore, modulation of the infrared radiation output'of the arc lamp has presented non-trivial problems in that the lamp electrodes must be prevented from appearing in the field of view of the device in. order to provide adequate depth of modulation. To provide complex modulation of the arc lamp output also requires modulator electronics of undue complexity. Modulation-of blackbody sources has generally been provided through the use .of rotating choppers which have proven satisfactory. for small apertures. When it is sought, however,vto use large aperture sources therotating chopper becomes too large for practicaluse.
OBJECTS AND SUMMARY OF THE INVENTION From the foregoing it will be understood that among the various objectives of the present invention are:
To provide a new and novel modulated source of infrared energy.
To provide apparatus of the above-described character which requires minimal electrical power.
To provide apparatus of the above-described character having an output aperture of increased area.
To provide apparatus of the above-described character which is of particular adaptability to mobile operation. I a
These and'other objectives are achieved by providing an insulated high temperature, high emissivity ceramic combustion chamber closed at one end by a transparent window. A'combustible fuel is introduced together with oxygen or air into the combustion chamber and ignited. The flame heats the ceramic chamber walls to Slightly under their melting temperature and the combustion products are exhausted through a mixing chamber where they are mixed with cooling air. The heated ceramic walls emit infrared radiation which is transmitted through the window. A motor driven rotating shutter modulator is disposed in front of the exit aperture whichprovides efficient amplitude modulation of the output radiation.
The foregoing as well as other objects, features and advantages of the present invention will become more apparent from the following detailed description taken in conjunction with the appended drawings.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic cross-sectional view of a com- FIG. 2 is a schematic elevation view of a rotating shutter modulator suitable for use with the radiation source of FIG. 1.
FIG. 3 is a schematic cross-sectional view of a mechanically modulated combustion heated infrared radiation source particularly adapted for use in a mobile application.
FIG. 4 is a schematic block diagram of a complete amplitude modulated infrared transmitter incorporating the apparatus of the present invention.
DESCRIPTION OF PREFERRED EMBODIMENT Turning now to FIG. 1 there is schematically illustrated in cross section simplified combustion heated infrared radiation source in accordance with the present invention. The source comprises a high temperature combustion chamber 10 formed of a high emissivity material and closed at one end by a window 12 which is transparent to radiation over a preselected spectral range. Fuel is introduced into the combustion chamber 10 via a burner orifice 14 preferably in a direction relative to the combustion chamber 10 such that rapid mixing and'combustion are achieved. Since the window 12 is in direct contact with the hot combustion gases it is preferred that the oxygen or air necessary to support combustion of the fuel be introduced at a low tempera v ture through a thin cylindrical slit 16 in the source facefrom the hot combustion gases is maximized and the practice of the present-invention.
combustion chamber walls thus comprise the infrared radiating surface.
The combustion products which must be exhausted from the chamber 10 via exhaust nozzle 24 are quite hot and must be cooled before exiting the source. Exhaust cooling air is introduced through ducts 26 to an exhaust gas mixing chamber 28. The exhaust products are thus cooled to a desired temperature determined by the mixture ratio of air to combustion products.
. It has been found by the Applicants that the various forms of zirconium oxide are. particularly useful in the fabrication of the combustion chamberalthough any material capable of withstanding the high combustion temperatures is acceptable in the practice of the invention. It is preferred that the combustion chamber be laid up on a mandrel with zirconium oxide yarn and impregnated with a zirconium oxide cast in a similar manner to that employed with glass-reinforced resin plastics. In this way complex shapes optimized to withstand thermal shock may be easily fabricated.
It is also preferred in the practice of the present invention that a fuel providing as high a flame temperature as possible be employed, however, considerations such as fuel availability and toxicity are factors bearing on practical choices. For example the temperature of an oxy-acetylene flame is 3,360 K and thus acetylene would be a desirable fuel. This fuel is, however, explosive and in some applications, particularly those which are mobile, it is necessary to dissolve the acetylene in acetone which increases the storage weight per pound of usefuel fuel. A relatively new fuel is the so called MAPP gas, a mixture of Methyl acetylene, Allene, Propane and Propylene. This is more stable than acetylene and thus may be stored as a liquid under its own vapor pressure without danger of explosion. Another readily available fuel is liquid propane.
The selection of an operating temperature for the radiation source of FIG. 1 may be made based upon minimum specific fuel consumption consistent with minimum source size and optical aperture. In one embodiment fabricated by the Applicants an operating temperature of 2,400" K for a propane fired device requires a combustion chamber diameter of 1.0 inch. Propane consumption was found to be 0.58 pounds/hour and oxygen consumption 2.1 l pounds/hour. The device thus fabricated produced a total radiation output of 325 watts.
FIG. 2 schematically illustrates a rotatingshutter mechanical modulator which is useful in combination with the radiation source of FIG. 1 in the practice of the present invention. This modulator comprises at least one bank of continuously rotatable blades 30 each mounted between mounting brackets 32 in bearing assemblies 34. The blades 30 are driven in rotation by a motor 36 through an output gear 38 and reduction gear 40. Adjacent blades are driven in opposite directions by the train of substantially identical gears 42. In order to eliminate twisting of the individual blades 30 each is driven from both ends. In addition to driving the gears 42 the motor 36 also drives gear 44 which is coupled by shaft 46 to a gear train substantially identical to that illustrated at 42 and 44 but disposed on the outside of the opposite mounting bracket 32. To further minimize twisting of the blades 30 the bearing assemblies 34 may be slightly preloaded thus placing the-blades 30 under some tension. It has been found by the Applicants that a typical size motor developing 0.5 in-oz of torque at 24,000 rpm and 0.8 in-oz of stall torque is adequate to drive a bank of nine blades 0.315 inch wide disposed on 0.300 inch centers. The bearing assemblies 34 are of standard commercially available type and the gears may be for example standard pressure angle gears. It will be readily apparent that any of a wide variety of bearing assemblies and gears suitable to meet a given modulation frequency requirement could be used.
Also illustrated in FIG. 2 is a second drive motor 46 and an associated gear train 48 identical, to that associated with blades 30 and discussed above. This second motor 46 and gear train 48 are operative to drive a second bank of rotatable blades (obscured by blades 30 and thus not shown). With such a double arrangement of independently driven shutter blades it is possible to modulate the radiation output of an infrared or other optical source with more complex functions. For example drive motor 36 may be operated at a constant speed and thus blades 30 modulate the output radiation at some preselected fixed frequency. The second drive motor 46 may be variable in speed and operate to drive the second bank of shutter blades such as to amplitude modulate the fixed frequency radiation. To achieve the radiating cavity 60 is a circular. cone of double-wall, 62 and 64, construction in order to minimize thermal losses from the back side of the inner wall 62. The inner wall 62 includes a plurality of flow passages 66 for the hot combustion gases to pass from the combustion chamber into the space 68 between the walls 62 and 64 and through a sonic exhaust nozzle 70 at the base of the radiation source.
It would be preferable in the practice of the present invention to insulate the radiating cavity with a single layer of high temperature, high efficiency insulation material. A problem which is encountered, however, is that the most efficient insulating materials generally cannot withstand very high temperatures. Thus it is necessary with high temperature sources to use a layer 72 of' high temperature insulation such as zirconium oxide felt next to the outer cavity wall 64. A sufficient thickness is used to keep the maximum temperature at the outer surface of the layer 72 at a level which is tolerable by a layer 74 of insulation such as silicon dioxide glass which is of higher insulating efficiency but lower temperature capacity than the layer 72 of high temperature insulation. Similarly, a third or outer layer 76 of very high insulating efficiency but low temperature capacity insulation such as MIN-K a very low conductivity insulating material of utility at temperatures less than l,200 'K and commercially available from the Johns-Man'ville Co. may be used if necessary ordesired. The insulated radiating cavity is disposed in a case structure 78 which is provided with a plurality of longitudinal heat exchange fins 80. I
The radiating cavity 60 is closed at its output end by a window 82 which is transparent over the output wavelength range of interest. For example for a radiation output in the visible wavelength band a quartz window would be a logical choice based upon low cost and optimum resistance to thermal shock. Obviously, other window materials would be preferred for other regions of the spectrum. In order to avoid devitrification of the quartz window, the oxygen or air necessary to support combustion withinthe cavity 60 is introduced via an oxygen supply line 84 into a cylindrical slit 86 at the periphery of the window 82. The cold oxygen thus passes over the window 82 and serves to keep the window temperature within acceptable limits. It has been found by the Applicants that this technique is adequate to maintain a window temperature of less than 900 C while the radiating cavity walls were heated to 2,600 K. Further, the radiative output of the source has been found to be substantially unaffected when most of the oxygen is injected over the window 82 as long as combustion is completed within the cavity 60.
The fuel is introduced through fuel supply line 88 to a small orifice 90 disposed tangentially to the inner wall 62 of the radiating cavity 60. For mobile applications propane is a desirable fuel in accordance with the fuel selection criteria discussed above with reference to FIG. 1.
The simplest ignition system of utility in the practice of the present invention is an electrical spark generated by discharging a condenser across a spark gap. To this end copper electrodes 92 and 94 are inserted into the radiation cavity 60 through a high temperature gasket 96 such as a replaceable zirconium oxide insert. The electrodes 92 and 9,4 are coupled at their opposite ends through the housing structure 78 to an electrical connector block 98 of the type known in the art andthe interm] details-of which are thus notspecifically illustrated. Once combustion is initiated within the cavity the electrodes 92 and 94 will begin to melt and ignition will be maintained by the hot cavity wall 62.
Radiation from the heated cavity wall 62 is passed by window 82 and mechanically modulated by a rotating shutter modulator 100 as described with reference to FIG. 2. The electrical coupling to the modulator drive motor(s) is illustrated schematically at 102. If desired a reflective light funnel 104 of any preselected geometry may be used at the output side of the modulator 100 to provide a particular spatial distribution of the modulated output energy. A plurality of heat exchanging fins 106 may also be disposed about the circumference of the light funnel 104. Additionally if required in a given application a suitable filter 108 may be disposed over the light funnel 104 output aperture.
Cooling of the radiation source in the mobile environment is provided by ducted air. The exhaust gases issue from the-exhaust nozzle 70 into a mixing chamber 110 formed as a part' of the housing structure 78. To prevent erosion of the housing structure 78 and to reduce heating of the electrical connector'block 98 a layer 112 of high temperature resistance material may be placed opposite the nozzle 70. Cooling air is admitted via opening 114 in the mixing chamber 110, mixed with the hot exhaust gases and vented to the environment by means of coupling 116. It has been found that the exhaust gases from a propane fired radiation source may be reduced to a temperature of lessthan 250 F by mixing with ram'air at a mass ratio of about 35.
Cooling air is also admitted via airscoops 118 which are formed as a part of an outer shroud 120-. This air passes over the heat exchange fins 106 on light funnel '104, pastthe drive motors of modulator 100 and over the longitudinal heat exchange fins 80 on the housing structure 78. This air may be vented to the environment either directly or via the vent coupling 116.
A thermal switch 121 may be disposed in the exhaust mixing chamber 110 to continuously monitor the exhaust gas temperature. If, for example, the exhaust gas temperature has not risen to a preselected level within a given period of time after an ignition spark across the electrodes 92 and 94 a reignition sequence may be initiated in the manner'to be described hereinbelow. A second thermal switch 122 may be diposed at any convenient positionnear the output window 82. In the event that the window were to break combustion gases would'quickly enter the optical cavity with an attendant temperature rise. Thus the rise in temperature may be used to initiate a shut-off sequence to be prescombustion heated infrared radiation transmitter in accordance with the principles of the present invention. The radiating cavity combustion chamber 124 is coupled by supply lines 126 and 128 to an oxygen and fuel supplies 130 and 132 respectively; each supply line Combustion of the fuel heats the combustion chamber 124 which radiates the infrared. This radiation passes through the combustion chamber window 138 and is modulated by the above-described mechanical modulator 140. The modulator drive motors 142 are driven by any suitable power source 144'.
" The combustion products are coupled from the combustion chamber 124 to the exhaust mixing chamber 146 where they are mixed with cooling air which is provided via air intake 148. The cooled gases are vented to the environment via exhaust coupling 150.
The ignition spark gap 152 is coupled via control logic 154 to the power source 144. The control logic .154 also receives an inputs the electrical signals from the exhaust gas temperature sensor 156, optics temperature sensor 158, and starting means 160. In operation an initial starting signal applied from the starting means 160 to the control logic 154 serves to apply power from source 144 to the modulator drive motors and to initiate the ignition sequence. This sequence includes charging of the ignition capacitor 162 and opening the solenoid valves 134 and 136 in the oxygen and fuel supply lines 126 and 128 respectively. Once the ignition capacitor 162 is fully charged it is discharged across the spark gap 142 in the combustion chamber 124. Assuming proper ignition the temperature of the exhaust gases in the exhaust mixing chamber will rise quickly to an operating level. If this temperature has not risen to a given value within a selected time the exhaust gas temperature'sensor 156 will so indicate and the ignition sequence may be repeated. In such cases the oxygen and fuel solenoid valves 134 and 136 are closed for a period sufficient to vent any combustible gases from the combustion chamber 124, and the above-described ignition sequence repeated. If desired a predetermined number of unsuccessful ignition attempts may serve as the criterion for inactivating the entire system. An automatic inactivation sequence may also be initiated if the optics temperaturesensor 158 detects the conditions indicative of a broken window 138. In such event I the oxygen and fuel solenoid valves 134 and 136 would being provided with a solenoid valve 134 and 136. The
oxygen. supply 130 may be a tank of liquid oxygen or could be a chemicaloxygen generator whereby oxygen ,is generated chemically from sodium chlorate. Such be closed andpower removed from themodulator drive motors 142.
It will thus be seen that the Applicants have provided v a new and novel mechanically modulated combustion heated infrared radiation source wherein the objectives set forth hereinabove are efficiently met. Since certain changes in the above construction will become apparent to those skilled in the art without departing from the scope of the invention it is intended that all matter contained in the foregoing description or shown in the' appended drawings shall be interpreted as illustrative and not in a limiting sense. i i
. Having described what is new and novel and desired to secure by Letters Patent, what is claimedis:
l. A combustion heated source of modulated radiant energy comprising a combustion chamber formed of awhen heated emit radiant energy, a window substantially transparent to said radiant energy closing or end of said combustion chamber, means for introducing a combustible mixture into said combustion chamber, j means for igniting said mixture such that said fuel is burned whereby said combustion chamber is heated and radiant energy is emitted through said window, i
m aterial which i means for exhausting the combustion products from said combustion chamber, and
a mechanical radiant energy modulator.
2. Apparatus as recited in claim 1 further including means for cooling said window.
3. Apparatus as recited in claim 2 wherein said means for introducing a combustible mixture into said combustion chamber includes means for introducing an oxidizing agent into said combustion chamber and means for introducing a combustible fuel into said combustion chamber such that said oxidizing agent and fuel are mixed together.
4. Apparatus as recited in claim 3 wherein said means for cooling said window includes means for passing said oxidizing agent over said window prior to being mixed with said combustible fuel.
5. Apparatus as recited in claim 1 wherein said mechanical radiant energy modulator includes a first-plurality of blades mounted for rotation about a like first plurality of parallel axes disposed in substantially a single first plane adjacent the exterior surface of said window each axis separated from adjacent axes by a distance comparable to the width of said blades, and
means for driving said first pluralityof blades in synchronous rotation such that radiant energy emitted through said window is amplitude modulated as a function of the angular position of said first rotating blades.
6. Apparatus as recited in claim 1 wherein said combustion chamber is formed of zirconium oxide.
7. Apparatus as recited in claim 6 wherein said zirconium oxide combustion chamber is formed of zirconium oxide yarn impregnated with zirconium oxide cast. I
8. Apparatus as recited in claim 1 wherein said combustion chamber is a crucible having an inner and outer wall.
9. Apparatus as recited in claim 8 wherein said inner wall defines a plurality of holes therein such that combustion gas can pass through said holes thereby minimizing thermal losses from the back side of said inner wall.
10. Apparatus as recited in. claim 1 wherein said combustion chamberis a'double-wa'll circular cone having an exhaust passage between said walls and the inner wall having a plurality of apertures therethrough, said exhaust passage terminating in an exhaust nozzle at the end of said combustion chamber opposite said window.
11. Apparatus as recited in claim 1 further including means for cooling said combustion products as they are exhausted from said combustion chamber.
12. Apparatus as recited in claim 11 wherein said combustion products cooling means comprises an exhaust mixing chamber into which said combustion products are introduced, and means'for introducing cooling air into said exhaust mixing chamber at a selected mass ratio to saidcombustion products.
13. Apparatus as recited in claim 12 wherein said cooling air is mixed with said combustion products ata mass ratio of at least thirty five.
14. Apparatus as recited in claim 1 wherein said radiant energy is in the visible wavelength band,
and said window is formed of quartz.
15. Apparatus as recited in claim 3 wherein said fuel introducing means comprises a pressurized container of combustible gas, and a fuel supply line in communication at one end with said container and at the other end with said combustion chamber.
16. Apparatus as recited in claim 15 wherein said fuel supply line is disposed with respect to said combustion chamber such as to introduce said gas tangentially into said chamber.
17. Apparatus as recited in claim 3 wherein said oxidizing agent introducing means comprises a supply of pressurized oxygen, and an oxygen supply line in communication at one end with said oxygen supply and at the other end with said combustion chamber.
18. Apparatus as recited in claim 17 wherein said supply of pressurized oxygen comprises a conainer of liquid oxygen. I
19. Apparatus as recited in claim 18 wherein said supply of pressurized oxygen comprises a chemical oxygen generator.
20. Apparatus as recited in claim 17 furtherincluding a cylindrical slit disposed in said combustion chamber circumferentially abutting said window at the periphery of theinterior surface thereof, said slit being in circumferential communication with said combustion chamber, and said oxidizing agent being introduced into said slit such that said window is cooled thereby and maintained within a preselected temperature limit.
21. Apparatus as recited in claim 1 wherein said igniting means comprises a pair of electrodes inserted into said combustion chamber at the end thereof opposite said window, and means for generating an electrical spark across said electrodes.
22. Apparatus as recited in claim 5 further including a second plurality of blades mounted for rotation about a like second plurality of parallel axes disposed in substantially a single second plane adjacent and parallel to the plane of said'first plurality of blades, each axis of said second'plurality of blades separated from adjacent axes by a distance comparable to the width of said blades, and
means for driving said second plurality of blades in synchronous rotation independently of said first plurality of blades such that amplitude modulated radiation passed by said first plurality of blades is modulated as a function of the angular position of said second rotating blades.
23. Apparatus as recited in claim 22 wherein said means for driving said first plurality of blades operates at a fixed speed and said means for driving said second plurality of blades operates at a variable speed;
24. Apparatus as recited in claim 1 further including a light'funnel disposed adjacent said mechanical radiant energy modulator and having a configuration selected to provide a predetermined spatial distribution of said modulated radiant energy.
25. Apparatus as recited in claim 24 further including a passband filter disposed over the output end of said light funnel.
26. Apparatus as recited in claim 24 further including heat exchanging fins disposed in heat. transfer relation to said light funnel, and
and said oxidizing agent into said combustion chamber, and
a temperature sensor disposed in proximity to said combustion products exhausting means and coupled to said interrupting means such that a temperature below a preselected level produces an output from said temperature sensor which is operative to activate said interrupting means.
29. Apparatus as recited in claim 28 wherein said interrupting means comprises a solenoid valve in each of said fuel and oxidizing agent introducing means.

Claims (29)

1. A combustion heated source of modulated radiant energy comprising a combustion chamber formed of a material which when heated emit radiant energy, a window substantially transparent to said radiant energy closing or end of said combustion chamber, means for introducing a combustible mixture into said combustion chamber, means for igniting said mixture such that said fuel is burned whereby said combustion chamber is heated and radiant energy is emitted through said window, means for exhausting the combustion products from said combustion chamber, and a mechanical radiant energy modulator.
2. Apparatus as recited in claim 1 further including means for cooling said window.
3. Apparatus as recited in claim 2 wherein said means for introducing a combustible mixture into said combustion chamber includes means for introducing an oxidizing agent into said combustion chamber and means for introducing a combustible fuel into said combustion chamber such that said oxidizing agent and fuel are mixed together.
4. Apparatus as recited in claim 3 wherein said means for cooling said window includes means for passing said oxidizing agent over said window prior to being mixed with said combustible fuel.
5. Apparatus as recited in claim 1 wherein said mechanical radiant energy modulator includes a first plurality of blades mounted for rotation about a like first plurality of parallel axes disposed in substantially a single first plane adjacent the exterior surface of said window each axis separated from adjacent axes by a distance comparable to the width of said blades, and means for driving said first plurality of blades in synchronous rotation such that radiant energy emitted through said window is amplitude modulated as a function of the angular position of said first rotating blades.
6. Apparatus as recited in claim 1 wherein said combustion chamber is formed of zirconium oxide.
7. Apparatus as recited in claim 6 wherein said zirconium oxide combustion chamber is formed of zirconium oxide yarn impregnated with zirconium oxide cast.
8. Apparatus as recited in claim 1 wherein said combustion chamber is a crucible having an inner and outer wall.
9. Apparatus as recited in claim 8 wherein said inner wall defines a plurality of holes therein such that combustion gas can pass through said holes thereby minimizing thermal losses from the back side of said inner wall.
10. Apparatus as recited in claim 1 wherein said combustion chamber is a double-wall circular cone having an exhaust passage between said walls and the inner wall having a plurality of apertures therethrough, said exhaust passage terminAting in an exhaust nozzle at the end of said combustion chamber opposite said window.
11. Apparatus as recited in claim 1 further including means for cooling said combustion products as they are exhausted from said combustion chamber.
12. Apparatus as recited in claim 11 wherein said combustion products cooling means comprises an exhaust mixing chamber into which said combustion products are introduced, and means for introducing cooling air into said exhaust mixing chamber at a selected mass ratio to said combustion products.
13. Apparatus as recited in claim 12 wherein said cooling air is mixed with said combustion products at a mass ratio of at least thirty five.
14. Apparatus as recited in claim 1 wherein said radiant energy is in the visible wavelength band, and said window is formed of quartz.
15. Apparatus as recited in claim 3 wherein said fuel introducing means comprises a pressurized container of combustible gas, and a fuel supply line in communication at one end with said container and at the other end with said combustion chamber.
16. Apparatus as recited in claim 15 wherein said fuel supply line is disposed with respect to said combustion chamber such as to introduce said gas tangentially into said chamber.
17. Apparatus as recited in claim 3 wherein said oxidizing agent introducing means comprises a supply of pressurized oxygen, and an oxygen supply line in communication at one end with said oxygen supply and at the other end with said combustion chamber.
18. Apparatus as recited in claim 17 wherein said supply of pressurized oxygen comprises a conainer of liquid oxygen.
19. Apparatus as recited in claim 18 wherein said supply of pressurized oxygen comprises a chemical oxygen generator.
20. Apparatus as recited in claim 17 further including a cylindrical slit disposed in said combustion chamber circumferentially abutting said window at the periphery of the interior surface thereof, said slit being in circumferential communication with said combustion chamber, and said oxidizing agent being introduced into said slit such that said window is cooled thereby and maintained within a preselected temperature limit.
21. Apparatus as recited in claim 1 wherein said igniting means comprises a pair of electrodes inserted into said combustion chamber at the end thereof opposite said window, and means for generating an electrical spark across said electrodes.
22. Apparatus as recited in claim 5 further including a second plurality of blades mounted for rotation about a like second plurality of parallel axes disposed in substantially a single second plane adjacent and parallel to the plane of said first plurality of blades, each axis of said second plurality of blades separated from adjacent axes by a distance comparable to the width of said blades, and means for driving said second plurality of blades in synchronous rotation independently of said first plurality of blades such that amplitude modulated radiation passed by said first plurality of blades is modulated as a function of the angular position of said second rotating blades.
23. Apparatus as recited in claim 22 wherein said means for driving said first plurality of blades operates at a fixed speed and said means for driving said second plurality of blades operates at a variable speed.
24. Apparatus as recited in claim 1 further including a light funnel disposed adjacent said mechanical radiant energy modulator and having a configuration selected to provide a predetermined spatial distribution of said modulated radiant energy.
25. Apparatus as recited in claim 24 further including a passband filter disposed over the output end of said light funnel.
26. Apparatus as recited in claim 24 further including heat exchanging fins disposed in heat transfer relation to said light funnel, and means for flowing cooling air over said heat exchanging fins.
27. Apparatus as recited in Claim 3 further including means for interrupting the introduction of said fuel and said oxidizing agent into said combustion chamber, and a temperature sensor disposed in proximity to said window and coupled to said interrupting means such that a temperature rise of preselected magnitude produces an output from said temperature sensor which is operative to activate said interrupting means.
28. Apparatus as recited in claim 3 further including means for interrupting the introduction of said fuel and said oxidizing agent into said combustion chamber, and a temperature sensor disposed in proximity to said combustion products exhausting means and coupled to said interrupting means such that a temperature below a preselected level produces an output from said temperature sensor which is operative to activate said interrupting means.
29. Apparatus as recited in claim 28 wherein said interrupting means comprises a solenoid valve in each of said fuel and oxidizing agent introducing means.
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US6359710B1 (en) * 1980-08-08 2002-03-19 The United States Of America As Represented By The Secretary Of The Navy IR radiation-seeker missile jammer
US6429446B1 (en) * 1975-04-28 2002-08-06 Bae Systems Information And Electronic Systems Integration, Inc. Multiple infrared missile jammer
US20100040511A1 (en) * 2000-10-04 2010-02-18 Lesieur Roger R Fuel gas reformer assemblage
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US3275829A (en) * 1960-08-15 1966-09-27 Special Devices Inc Cavity radiator with a pyrotechnic charge that remains intact during and after combustion
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6429446B1 (en) * 1975-04-28 2002-08-06 Bae Systems Information And Electronic Systems Integration, Inc. Multiple infrared missile jammer
US6359710B1 (en) * 1980-08-08 2002-03-19 The United States Of America As Represented By The Secretary Of The Navy IR radiation-seeker missile jammer
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US20100040511A1 (en) * 2000-10-04 2010-02-18 Lesieur Roger R Fuel gas reformer assemblage
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