Abstract:
An infrared imaging device and method for making infrared detector(s) having at least one anode, at least one cathode with a substrate electrically connected to a plurality of doped carbon nanostructures; and bias circuitry for applying an electric field between the anode and the cathode such that when infrared photons are absorbed by the nanostructures the emitted field current is modulated. The detectors can be doped with cesium to lower the work function.

Description:
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH 
       [0001]    This invention was made with United States Government support under Contract No. DE-AC05-00OR22725 between the United States Department of Energy and U.T. Battelle, LLC. The United States Government has certain rights in this invention. 
     
    
     BACKGROUND OF THE INVENTION 
       [0002]    There are three basic performance levels in the IR camera market today. First, there are the high performance IR cameras that typically employ IR detectors that are wavelength-selective (e.g., HgCdTe, InSb). These cameras possess several of the following characteristics: high-speed, high-sensitivity, large format, windowing, snapshot mode, and external synchronization. However, they are costly, largely because they require cryogenic cooling (to reduce noise, etc), and HgCdTe is difficult to control during manufacturing. These cameras are typically used in aerospace, military, and research applications. The cost of a high-performance IR camera can range between $70K and $170K. Second, there are the general-purpose IR cameras that are primarily used for predictive maintenance (PM). These cameras must be radiometric but do not require high-speed. The cost of PM cameras range between $40K and $70K. Finally, there are the low-cost uncooled IR cameras, typically based on microbolometer or pyroelectric technology. These cameras detect wavelengths from 3 μm and longer. They operate at low video frame rates and offer a much poorer image due to non-uniformity between pixels. These cameras are used in qualitative applications such as surveillance, fire rescue, and automobile night vision. Uncooled IR cameras cost around $15K. This invention targets the low-cost, uncooled IR detector camera niche. An uncooled IR detector camera that can purchased for around $1000 would be a unique instrument and would revolutionize the IR camera market in much the same way as the development of the uncooled microbolometer camera has over the last five years. Low cost is the key that opens the door to hundreds of markets. 
         [0003]    U.S. Pat. No. 6,861,790 to Iwasa teaches a cold cathode element for flat panel displays. The cold cathode element consists of an aluminum substrate on which amorphous carbon film containing cesium is grown using vapor deposition. Several small conical projections of cesium oxide are formed on the film. The “projections” or nanostructures on the substrate are formed of cesium oxide but the type of nanostructure (e.g., nanotube, nanoflake, nanofiber, etc.) is not specified. Iwasa teaches only a basic method of producing low work function field emission and no circuitry for producing a practical device is included. 
         [0004]    U.S. Pat. No. 6,400,088 to Livingston et al. teaches an infrared (IR) detector consisting of an anode, a cathode on which is deposited a forest of carbon nanotubes, and bias circuitry for applying an electric field between the anode and the cathode such that when IR photons are absorbed by the nanotubes, photoelectrons are created. Livingston fails to teach that cesium is added to the nanotubes. 
         [0005]    U.S. Pat. No. 5,908,699 to Kim teaches a cold cathode element for flat panel displays consisting of an amorphous carbon matrix having cesium dispersed therein, with the cesium present in substantially non-crystalline form. A method of producing the cesium oxide and a method of designing a single electron emission device for improved brightness is also specified. 
         [0006]    Field emission properties of carbon nanotubes have been extensively studied for the fabrication of cold cathodes for field emission displays. However, application of this technology to infrared imaging has not been investigated. 
       BRIEF SUMMARY OF THE INVENTION 
       [0007]    An infrared imaging device and method for making infrared detector(s) having at least one anode, at least one cathode with a substrate electrically connected to a plurality of doped carbon nanostructures; and bias circuitry for applying an electric field between the anode and the cathode such that when infrared photons are absorbed by the nanostructures the emitted field current is modulated. The detectors can be doped with cesium to lower the work function. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0008]      FIG. 1  is a conceptual diagram of a single infrared sensor. 
           [0009]      FIG. 2  is a graph of the required (local) electric field as a function of wavelength. 
           [0010]      FIG. 3  is a SEM of carbon nanoflakes, carbon nanofibers, and carbon. nanotubes 
           [0011]      FIG. 4  is a schematic of the pixilated detector array concept. 
           [0012]      FIG. 5  is an illustration of a detector array fabrication process. 
           [0013]      FIG. 6  are schematics of top anode assembly for carbon nanotube IR detector array. 
           [0014]      FIG. 7  is a pixel multiplexing scheme 
           [0015]      FIG. 8  is a graph of noise as a function of vacuum level for carbon nanotubes. 
           [0016]      FIG. 9  is a graph of 1/f noise in single-wall nanotubes. 
           [0017]      FIG. 10  is a schematic of a method for achieving high vacuum in array device. 
           [0018]      FIG. 11  is an illustration of a readout circuit for a single detector. 
       
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
       [0019]    Doped carbon nanostructures are fabricated as low work-function field emitters, in which the incoming infrared energy is used to modulate the emitted field current. Two physical effects are exploited: (1) the reduction in work function when a more electropositive material is used to coat a material, and (2) the reduction in effective work function with increased electric field. The work function of carbon is ˜4.6 eV. 
         [0020]    It is known that adsorbed layers of electropositive elements, such as cesium, can enhance cathode performance. Enhanced thermionic and field emission from cesiated tungsten filaments were demonstrated by Langmuir and Kingdon in 1923 and Haefer in 1940. When a surface is coated with a thin layer of electropositive (relative to the substrate) material, the work function is reduced. 
         [0021]    Kim et. al. have investigated the effect of electric field on the effective work function of capped carbon nanotubes. The effective work function is defined as the difference in energy between the Fermi level and the lowest unoccupied molecular orbital (LUMO). They show that the work function decreases linearly with increasing electric field. The effective work function approaches zero at a high electric field, and electrons can be emitted more easily. 
         [0022]    The surface electronic properties of cesiated (doped) carbon films on Si (100) substrates have been investigated by co-deposition of neutral Cs and Cs− ion beams at different energies (25-150 eV). At the Cs− ion beam energy of 150 eV, the work function of the surface decreases to 1.1 eV. Post oxidation of the surface lowers the work function to 1.05 eV. This oxygen treated cesiated carbon film is a reliable cold-cathode electron emitter due to the extremely high thermal stability of the low work function. 
         [0023]      FIG. 1  shows a conceptual diagram of the infrared sensor. This imaging device comprises patterned metal to form an anode  10  with an IR transmissive window  16  made from glass or ceramic disposed on the anode, a cathode  12  having a silicon dioxide layer on a silicon substrate and doped carbon nanostructures  14  with a suitable electric field that will provide a sufficiently low work function of the order of the incoming infrared IR energy. This enables the field emission current to be modulated by the incident IR energy. 
         [0024]    Photoemission in a material is presumed to occur if the impinging photon energy is sufficiently high to raise an electron to an energy level above the peak of the barrier above the surface of the material. In a high electric field, the barrier height can be substantially reduced, resulting in cold (or thermally assisted) field emission. At high electric fields, the surface barrier is lowered by the Schottky effect, in which the electron is attracted to the surface by its image charge. The surface barrier is effectively reduced below the nominal work function by an amount equal to: 
         [0000]      φ d   =e √{square root over ( eE   f /4πε 0 )}  (1) 
         [0000]    where: 
         [0025]    e is the electron charge (1.6×10 −19  C); 
         [0026]    E f  is the electric field (V/m); 
         [0027]    ε 0  is the permittivity of free space (8.85×10 −12  F/m). 
         [0000]    Thus, an incoming photon with energy E will be able to eject an electron if: 
         [0000]        E≧Φ−φ   d   (2) 
         [0000]    Inserting the values of e and ε 0  into equation (1), we have: 
         [0000]    
       
         
           
             
               
                 
                   
                     φ 
                     d 
                   
                   = 
                   
                     
                       
                         1.6 
                         × 
                         
                           10 
                           
                             - 
                             19 
                           
                         
                          
                         
                           
                             
                               1.6 
                               × 
                               
                                 10 
                                 
                                   - 
                                   19 
                                 
                               
                                
                               
                                 E 
                                 f 
                               
                             
                             
                               4 
                                
                               
                                   
                               
                                
                               π 
                               × 
                               8.85 
                               × 
                               
                                 10 
                                 
                                   - 
                                   12 
                                 
                               
                             
                           
                         
                       
                        
                       
                         
 
                       
                       ∴ 
                       
                         φ 
                         d 
                       
                     
                     = 
                     
                       5.056 
                       × 
                       
                         10 
                         
                           - 
                           24 
                         
                       
                        
                       
                         
                           
                             E 
                             f 
                           
                         
                         . 
                       
                     
                   
                 
               
               
                 
                   ( 
                   3 
                   ) 
                 
               
             
           
         
       
     
         [0000]    Equation 3 has units of energy (charge×volts). By definition, 1 eV is 1.6×10 −19  J, which is the energy given to an electron by accelerating it through 1 volt of electric potential difference. Thus, the value of equation (3) in eV is equal to: 
         [0000]    
       
         
           
             
               
                 
                   
                     ∴ 
                     
                       φ 
                       d 
                     
                   
                   = 
                   
                     
                       
                         
                           
                             5.056 
                             × 
                             
                               10 
                               
                                 - 
                                 24 
                               
                             
                              
                             
                               
                                 E 
                                 f 
                               
                             
                           
                           
                             1.6 
                             × 
                             
                               10 
                               
                                 - 
                                 19 
                               
                             
                           
                         
                          
                         
                             
                         
                          
                         eV 
                       
                        
                       
                         
 
                       
                       ∴ 
                       
                         φ 
                         d 
                       
                     
                     = 
                     
                       3.79 
                       × 
                       
                         10 
                         
                           - 
                           5 
                         
                       
                        
                       
                         
                           E 
                           f 
                         
                       
                        
                       
                           
                       
                        
                       eV 
                     
                   
                 
               
               
                 
                   ( 
                   4 
                   ) 
                 
               
             
           
         
       
     
         [0000]    The energy (in eV) of a 5 μm wavelength IR photon is given by: 
         [0000]        E=hc/λq   (5) 
         [0000]    where:
 
h=Planck&#39;s constant (6.626×10 −34  Js)
 
c=speed of light (2.9979×10 8  m/s)
 
λ=wavelength (m)
 
q=1.6×10 −19  J
 
Thus, 5 μm IR radiation has an energy of ˜0.25 eV.
 
Equations (2) and (4) show that, by reducing the work function of the carbon nanostructures to 1.1 eV, the minimum electric field necessary to produce field emission from an infrared photon of λ is given by:
 
         [0000]    
       
         
           
             
               
                 
                   
                     
                       
                         
                           E 
                           f 
                         
                       
                       ≥ 
                       
                         
                           ( 
                           
                             1.1 
                             - 
                             
                               
                                 hc 
                                 / 
                                 λ 
                               
                                
                               
                                   
                               
                                
                               q 
                             
                           
                           ) 
                         
                         
                           3.79 
                           × 
                           
                             10 
                             
                               - 
                               5 
                             
                           
                         
                       
                     
                      
                     
                       
 
                     
                     ∴ 
                     
                       
                         E 
                         f 
                       
                       ≥ 
                       
                         
                           696 
                            
                           
                             [ 
                             
                               1.1 
                               - 
                               
                                 ( 
                                 
                                   1.242 
                                   / 
                                   λ 
                                 
                                 ) 
                               
                             
                             ] 
                           
                         
                          
                         
                             
                         
                          
                         V 
                          
                         
                           / 
                         
                          
                         µ 
                          
                         
                             
                         
                          
                         m 
                       
                     
                   
                   , 
                   
                     where 
                      
                     
                         
                     
                      
                     λ 
                      
                     
                         
                     
                      
                     is 
                      
                     
                         
                     
                      
                     in 
                      
                     
                         
                     
                      
                     
                       microns 
                       . 
                     
                   
                 
               
               
                 
                   ( 
                   6 
                   ) 
                 
               
             
           
         
       
     
         [0028]      FIG. 2  is a plot of the required field as a function of wavelength (equation 6). Note that equation 6 gives the required local field strength. The global field strength can be much lower than that predicted by equation 6, while still achieving the higher local field strength required because of the very high field enhancement properties of carbon nanostructures, especially carbon nanotubes. A field amplification factor of greater than 500 is easily achievable, resulting in a much lower required electric field.  FIG. 3  shows scanning electron microscope (SEM) pictures of various carbon nanostructures. 
         [0029]    A method for using an array of carbon nanotubes for infrared imaging is shown in  FIG. 4 . A “pixel”  48  of this imaging array consists of a forest of doped, vertically aligned single wall nanotubes (SWNTs) or multi-wall nanotubes (MWNTs), hereinafter referred to as doped vertically aligned carbon nanotubes (DVACNTs)  44 . An anode  40  having an IR transmissive window  46  is disposed atop the structure. The center-to-center distance between the DVACNTs (pitch) is approximately 4 μm. This pitch is selected to reduce electrostatic screening effects (which diminishes the field enhancement factor) while at the same time increasing field penetration as well as optimizing field emission current. 
         [0030]    A method for fabricating a detector array consisting of several pixels is shown in  FIGS. 5 and 6 . The fabrication is in two parts: the bottom cathode section ( FIG. 5 ) and the top anode section ( FIG. 6 ). The cathode section fabrication process begins with depositing a layer of silicon oxide  51  on a silicon substrate  53 , then etching out pixel-size circular islands in the silicon. An array of circular metal catalysts  55  (for growing the nanotubes) are then formed in these holes by first depositing a thin film of metal on the silicon oxide/silicon surface, then etching away the unwanted parts to expose back the silicon oxide and silicon surfaces. The CNT  54  forests are grown from the exposed metal pads on each island of silicon, and then doped with cesium via chemical vapor deposition (CVD) or ion implantation. 
         [0031]    The top anode grid of the field emission pixel array is assembled separately from the bottom section. The grid consists of electrically conductive anodes  60  connected by rows or columns to an edge connection with insulating material  65  placed to isolate individual pixel cells and prevent crosstalk. The anodes  60 , connecting wires  63 , and insulator  65  are deposited on an infrared transparent window  66 . These components are shown in  FIG. 6(   a ). The fabricated top assembly is attached to the cathode section and vacuum sealed by a low-temperature glass melt bead  67 . The electronics for each pixel or for rows or columns of pixels are placed beneath the pixel region in the vacuum zone [ FIG. 6(   b )]. 
         [0032]    A signal multiplexing method can be applied by sequencing the anode voltage  72  row-by-row while observing the field emission current  74  in each column as shown in  FIG. 7 . Each pixel of the array is individually addressable by that method. Alternatively, individual current preamplifiers can be placed under each pixel-cell allowing the columnar signal brought to the edge to be at a higher level and therefore less susceptible to noise and distributed capacitance. 
         [0033]    The presence of electronegative atoms and other contamination on the carbon nanotubes leads directly to excess noise and thereby reduces the signal-to-noise ratio in the field emission current of the detector. The vacuum level, therefore, is an important factor in the noise observed in field emission current. At lower vacuum pressure levels, the molecular adsorption rate (and subsequent desorption) becomes higher, which affects emitter stability. N. de Jonge et al., “Low noise and stable emission from carbon nanotube electron sources,” Applied Physics Letters 87, 133118 (2005) measured noise as a function of vacuum level.  FIG. 8 , adapted from N. de Jonge et al., illustrates the lowering of noise with decreased pressure. (The curves, derived from points shown in  FIG. 10(   b ) of the cited paper, represent four different nanotube devices.) A vacuum pressure of 3×10 −8  Torr means that roughly a monolayer of residual gas atoms forms on the emitter surface about every minute. It is clear that achieving and maintaining a high vacuum condition (greater than 10 −9  Torr) on the carbon nanotubes is necessary for high signal-to-noise performance. Note that other noise sources also exist such as Johnson (from thermal agitation), shot, avalanche, burst, and 1/f. Each noise type must be dealt with uniquely. The 1/f noise, which appears dominant as shown in  FIG. 9  [from P. G. Collins et al., “1/f Noise in Carbon Nanotubes,” Applied Physics Letters, Vol. 76, No. 7 (2000)], is mitigated by synchronous modulation/demodulation methods (such as used in a lock-in amplifier). 
         [0034]    A method for achieving high vacuum conditions in an array is depicted in  FIG. 10 . The steps to achieving high vacuum levels are similar to methods used in fabrication of electronic vacuum tube devices. First, a vacuum is pulled on the entire array  102  of pixels using the vacuum connection  108  shown. A roughing pump in conjunction with either turbo or diffusion pumps brings the vacuum state in the range of 10 −8  Torr. Second, the entire array  102  is baked out at elevated temperature. A target for bake-out temperature is 300° C. although materials of construction may require bake-out at low temperatures. Note that the lower the temperature, the longer the bake-out time becomes. Third, the vacuum connection  108  is sealed after sufficient bake out thus isolating the array device. Fourth, the getters  109  are activated by a localized induction (or microwave) heaters. Getter flashing captures additional oxygen and other contaminant gases. The getter is positioned to deposit on the device walls so that there is no interference with carbon nanotubes, field emission, or the optics that pass the infrared light. Vacuum levels after the gettering step approach 10 −10  Torr. The getter material is chosen so that gettering is continued for the life of the detector array. Note that in the construction of the array, individual pixels must have gas communication back to the vacuum connection. Evacuation to the desired high vacuum level must occur for all pixels. 
         [0035]      FIG. 11  illustrates the readout circuitry using the basic detector cell. Readout methods for the single detector (or detector array) are not limited to the circuit shown in  FIG. 11 . Claimed techniques and configurations include the following:
       Measurement of small field emission current (nano- to micro-amps) using complementary metal oxide semiconductor (CMOS) input transimpedance preamplifier   Measurement of field emission current using junction field effect transistor (JFET) input stage of transimpedance preamplifier   Measurement of field emission current using bipolar junction transistor (BJT) transimpedance preamplifier   Measurement of field emission current using gallium arsenide (GaAs) transistor transimpedance preamplifier         
         [0040]    Readout circuit configurations include:
       Pulsed bias voltage and current input measurement stage with synchronous modulation and demodulation (lock-in amplifier)   Electronics (transimpedance preamplifier) mounted directly under each pixel (Pixel as described by a sparse forest of carbon nanotubes). Indium bump.   Preamplifier stages mounted at edge of circuit board. Matrix addressed by application of external bias voltage on an orthogonal matrix.   Charged coupled array placed under each pixel. The integrated charge accumulated is stepped out of the array and read by a charge sensitive preamplifier.       
 
         [0045]    While there has been shown and described what are at present considered the preferred embodiments of the invention, it will be obvious to those skilled in the art that various changes and modifications can be made therein without departing from the scope.