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Vacuum barrier

Figure 4.27. (a) Schematic of a STM z- Ft injection spectrum (solid curve). The dashed curves represent typical STM tip displacements observed at a clean metal surface, (b) Energy band diagrams for STM tunnelling through a vacuum barrier into the organic thin film and (c) through a Schottky-like barrier with the tip in contact. In both cases, Ft < 0 relative to Ep is shown. Adapted from Muller et al, 2001. [Pg.194]

Because temperature cannot cross this vacuum barrier, the cooling is further contained within the Dewar. [Pg.311]

To understand how STM works, it is vital to know what is tunneling current, and how it is related to all the experimental observations. Tunneling current is originated from the wavelike properties of particles (electrons, in this case) in quantum mechanics. When an electron is incident upon a vacuum barrier with potential energy larger than the kinetic energy of the electron, there is still a non-zero probability that it may traverse the forbidden region and reappear on the other side of the barrier. It is shown by the leak out electron wave function in Fig. 2. [Pg.2]

Fig. 4. Energy levels in two metals separated by a vacuum barrier. Fig. 4. Energy levels in two metals separated by a vacuum barrier.
Figure 22. The tunneling current, I, measured between two metal electrodes (tungsten en platinum) separated by a vacuum barrier as a function of the difference in electrochemical potential (here denoted as C/emitter-anode) the distance between the two electrodes (12, 20, 17 A) is indicated in the figure. Reprinted from Scanning Probe Microscopy and Spectroscopy , R. Wiesendanger, Cambridge University Press 1994... Figure 22. The tunneling current, I, measured between two metal electrodes (tungsten en platinum) separated by a vacuum barrier as a function of the difference in electrochemical potential (here denoted as C/emitter-anode) the distance between the two electrodes (12, 20, 17 A) is indicated in the figure. Reprinted from Scanning Probe Microscopy and Spectroscopy , R. Wiesendanger, Cambridge University Press 1994...
The pump occupies a volume of approximately 1 ft , with more specific dimensions as shown in Fig. 2. In order to minimize helium consumption, every effort has been made to shield the cold plate and its supply lines from thermal radiation of over 100°K. The cold plate is totally enclosed by chevrons and a conductance-cooled frame. The helium supply line is shielded from atmospheric temperature inside as well as outside of the chamber. This shield is cooled by liquid nitrogen lines. Outside of the chamber the shield also acts as a vacuum barrier. [Pg.482]

Fig. 5.11. Summary of factors limiting photo yield in the heterojunction model. The optical reflectivity is R transport factors in the band-bending region are described by with similar factors Tbs at the Semiconductor surface Barrier, Tabs for electron ABSorption in the (CsO) layer, and Tbv for loss at the (usually unimportant) Vacuum Barrier [5.82]... Fig. 5.11. Summary of factors limiting photo yield in the heterojunction model. The optical reflectivity is R transport factors in the band-bending region are described by with similar factors Tbs at the Semiconductor surface Barrier, Tabs for electron ABSorption in the (CsO) layer, and Tbv for loss at the (usually unimportant) Vacuum Barrier [5.82]...
The rigid substrate, usually containing contoured and deep-draw areas, is mounted to a mated metal mold which has predrilled holes to allow sufficient vacuum draw on the surface of the rigid fiberboard or plastic. Substrates like ABS that are vacuum barriers themselves also require holes to allow vacuum forming. [Pg.444]

Perhaps surprisingly, the mean true wear rate for the conventional polyethylene liners that had been sterilized with gamma radiation in air was not significantly different from that for the liners that had been sterilized with gamma radiation in vacuum-barrier packaging. [Pg.25]

Fig. 7.33. Schematic of typical bayonet joint for cryogenic transfer line. Legend 1, outer line, vacuum shell 2, line coupling 3, warm temperature O-ring seal 4, static gas leg 5, vacuum insulation space 6, vacuum barriers 7, additional liquid seal and 8, liquid line. Fig. 7.33. Schematic of typical bayonet joint for cryogenic transfer line. Legend 1, outer line, vacuum shell 2, line coupling 3, warm temperature O-ring seal 4, static gas leg 5, vacuum insulation space 6, vacuum barriers 7, additional liquid seal and 8, liquid line.
A second point that has to be taken into account in the three-dimensional case is the fact that an electron moving in the vacuum region can only use the energy E associated with its motion perpendicular to the surface to overcome the vacuum barrier. Hence, states bound toward the vacuum side can exist as long as this perpendicular energy is below the vacuum level or equivalently, if their total energy is below the parabola for the escape threshold into vacuum, that is. [Pg.131]


See other pages where Vacuum barrier is mentioned: [Pg.35]    [Pg.193]    [Pg.32]    [Pg.149]    [Pg.151]    [Pg.152]    [Pg.164]    [Pg.2]    [Pg.351]    [Pg.79]    [Pg.599]    [Pg.1090]    [Pg.1091]    [Pg.20]    [Pg.2953]    [Pg.98]    [Pg.62]    [Pg.836]    [Pg.1799]    [Pg.319]    [Pg.123]   
See also in sourсe #XX -- [ Pg.35 ]




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