1460706556-98ab4be6-a656-4973-bb7b-1a0e44dc791a

1. A composition comprising:
a liquid hydrocarbon, a phosphate ester, a crosslinker, and a hydrocarbon foaming agent.
2. A fluid including the composition according to claim 1.
3. A foamed fluid including the composition according to claim 1.
4. A well service fluid including the composition according to claim 1.
5. The well service fluid according to claim 4 wherein the amount of the phosphate ester is less than the amount required to gel the composition without the foaming agent.
6. The well service fluid according to claim 4, wherein the crosslinker is an aluminum salt or ferric salt.
7. The well service fluid according to claim 4, wherein the crosslinker is aluminum acetate, aluminum sulfate, aluminum chloride, ferric nitrate, ferric sulfate or ferric chloride.
8. The well service fluid according to claim 4, wherein the liquid hydrocarbon is an aliphatic hydrocarbon.
9. The well service fluid according to claim 4, wherein the foaming agent is a fluoro-based compound.
10. The well service fluid according to claim 4, wherein the foaming agent is a silicone-based compound.
11. The well service fluid according to claim 4, further including a chemical breaker.
12. The well service fluid according to claim 11, wherein the chemical breaker is calcium oxide or magnesium oxide.
13. The well service fluid according to claim 4 further including a defoaming agent.
14. The well service fluid according to claim 13 wherein the defoaming agent is a short chain alcohol.
15. The well service fluid according to claim 14 wherein the alcohol is methanol or ethanol.
16. The use of the fluid composition according to claim 4, for hydraulic fracturing, drilling, wellbore cleanout or pipeline cleaning.
17. A well service fluid according to claim 4 wherein the crosslinker is an aluminum salt or ferric salt, and the foaming agent is a fluoro-based compound.
18. A well service fluid according to claim 17 wherein the foaming agent is a silicone-based compound.
19. A well service fluid according to claim 4 wherein the crosslinker is selected from the group comprising aluminum acetate, aluminum sulfate, aluminum chloride, ferric nitrate, ferric sulfate and ferric chloride, and the foaming agent is a fluoro-based or silicone-based compound.
20. A well service fluid according to claim 19 further including a breaker.
21. A well service fluid according to claim 19 further including a defoaming agent.
22. A method for defoaming a foamed hydrocarbon-based well service fluid comprising the step of adding a short chain alcohol.
23. The method according to claim 22, wherein the defoaming agent is methanol or ethanol.

The claims below are in addition to those above.
All refrences to claims which appear below refer to the numbering after this setence.

1. A method for depositing a thin film on a flexible substrate, comprising:
introducing a first precursor gas into a first precursor zone;
introducing a second precursor gas into a second precursor zone spaced apart from the first precursor zone, the second precursor gas being different from and reactive with-the first precursor gas;
guiding a flexible substrate back and forth between the first and second precursor zones, using a plurality of turning guides at least some of which are located in the first and second precursor zones, and each time through a different one of a series of flow-restricting passageways of an isolation zone that is interposed between the first and second precursor zones, so that:
(i) the substrate transits through the first and second precursor zones and the isolation zone multiple times,
(ii) the first precursor gas adsorbs to the surface of the substrate during transit of the substrate through the first precursor zone, and
(iii) during a subsequent transit of the substrate through the second precursor zone the second precursor gas reacts with the adsorbed first precursor at the surface of the substrate to thereby deposit a thin film on the substrate;

introducing an inert gas into the isolation zone; and
generating a first pressure differential between the isolation zone and the first precursor zone and a second pressure differential between the isolation zone and the second precursor zone, the pressure differentials sufficient to inhibit migration of the first and second precursor gases out of the respective first and second precursor zones that results in exposure of the substrate to a reactive mixture of nonadsorbed amounts of the first and second precursor gases.
2. The method of claim 1, further comprising guiding the substrate back and forth between the second precursor zone and a third precursor zone into which a third precursor gas different from the second precursor gas is introduced.
3. The method of claim 1, in which generating the pressure differentials includes pumping from the first and second precursor zones.
4. The method of claim 1, in which generating the pressure differentials includes injecting the inert gas into the passageways.
5. The method of claim 1, in which the guiding of the substrate back and forth between the first and second precursor zones includes continuously advancing the substrate along a serpentine transport path.
6. The method of claim 5, in which the substrate is transported along the serpentine path in a first direction to complete a first pass, and subsequently rewinding the substrate along the serpentine path in a second direction opposite the first direction to complete a second pass.
7. The method of claim 6, further comprising, in an interval between the first and second passes, switching at least one of the first and second precursor gases to a different precursor gas.
8. The method of claim 1, further comprising introducing a dopant into one of the first and second precursor zones.
9. The method of claim 1, further comprising adjusting a length of at least some of the transits through the first precursor zone.
10. The method of claim 1, further comprising:
exhausting a flow of the first precursor gas from the first precursor zone; and
trapping the exhausted first precursor gas.
11. The method of claim 10, further comprising recycling the trapped first precursor gas into the first precursor zone.
12. The method of claim 1, further comprising:
paying out the substrate from a coil to a first end of the isolation zone; and
coiling the substrate from a second end of the isolation zone opposite the first end.
13. The method of claim 1, further comprising heating at least one of the first and second precursor zones.
14. The method of claim 1, further comprising heating the substrate.
15. The method of claim 1, further comprising introducing a radical into one of the first and second precursor zones.
16. The method of claim 1, in which the substrate traverses back and forth between the first and second precursor zones at least ten times.
17. The method of claim 1, further comprising introducing a third precursor gas into a third precursor zone interposed in the substrate path between the first and second precursor zones so that the isolation zone straddles the third precursor zone.
18. The method of claim 17, further comprising generating a third pressure differential between the isolation zone and the third precursor zone to inhibit the third precursor gas from migrating out of the third precursor zone and mixing with the first and second precursor gases within one of the zones, thereby inhibiting reactions within the zones between nonadsorbed amounts of the precursor gases.
19. The method of claim 1, where generating the first pressure differential includes removing a portion of the inert gas from the first precursor zone, and where generating the second pressure differential includes removing another portion of the inert gas from the second precursor zone.
20. The method of claim 1, further comprising exhausting gases from the first and second precursor zones at an exhaust pressure lower than respective operating pressures of the first and second precursor zones.
21. The method of claim 1, where the first and second precursor zones are contained within a process vessel, and the pressure differentials are sufficient to inhibit exposure of the substrate to a reactive mixture of the first and second precursor gases within the process vessel.
22. A method for depositing a thin film on a flexible substrate, comprising:
introducing a first precursor gas into a first precursor zone;
introducing a second precursor gas into a second precursor zone spaced apart from the first precursor zone;
introducing a third precursor gas into a third precursor zone interposed between the first and second precursor zones, the third precursor being reactive with the first precursor gas, the third precursor zone being spaced apart from the first precursor zone to define a first isolation region therebetween, and the third precursor zone being spaced apart from the second precursor zone to define therebetween a second isolation region therebetween;
guiding a flexible substrate back and forth between the first and second precursor zones and through the third precursor zone, using a plurality of turning guides at least some of which are located in the first and second precursor zones, so that the substrate transits through the first, second, and third precursor zones multiple times, the flexible substrate traveling each time through a different one of a first series of flow-restricting passageways of the first isolation region and each time through a different one of a second series of flow-restricting passageways of the second isolation region so that the substrate transits through the first and second isolation regions multiple times, wherein the first precursor gas adsorbs to the surface of the substrate during transit of the substrate through the first precursor zone, and during a subsequent transit of the substrate through the third precursor zone the third precursor gas reacts with the adsorbed first precursor at the surface of the substrate;
introducing an inert gas into the first isolation region; and
generating a first pressure differential between the first isolation region and the first precursor zone and a second pressure differential between the first isolation region and the third precursor zone, the first and second pressure differentials sufficient to inhibit migration of the first and third precursor gases out of the respective first and third precursor zones that results in exposure of the substrate to a reactive mixture of nonadsorbed amounts of the first and third precursor gases.
23. The method of claim 22, in which the reaction of the third precursor gas with the adsorbed first precursor deposits a first thin film on the substrate, a monolayer of the second precursor gas adsorbs to the first thin film during a transit of the substrate through the second precursor zone, and during a second subsequent transit of the substrate through the third precursor zone, the third precursor gas reacts with the adsorbed second precursor to thereby deposit a second thin film on the first thin film.
24. The method of claim 23, in which the first and second precursor gases are different.
25. The method of claim 22, further comprising:
introducing the inert gas into the second isolation region; and
generating a third pressure differential between the second isolation region and the second precursor zone, and in which a fourth pressure differential is generated between the second isolation region and the third precursor zone, the third and fourth pressure differentials sufficient to inhibit migration of the second and third precursor gases out of the respective second and third precursor zones that results in exposure of the substrate to a reactive mixture of nonadsorbed amounts of the second and third precursor gases.
26. The method of claim 25, in which generating the first, second, third, and fourth pressure differentials includes injecting the inert gas into the first and second isolation regions at a supply pressure greater than respective operating pressures of the first, second, and third precursor zones and then, from each of the first, second, and third precursor zones, removing exhaust gases at respective exhaust pressures lower than the respective operating pressures of the first, second, and third precursor zones.
27. The method of claim 22, in which the guiding of the substrate back and forth between the first and second precursor zones and through the third precursor zone includes continuously advancing the substrate along a serpentine transport path.
28. The method of claim 27, in which the substrate is transported along the serpentine path in a first direction to complete a first pass, and subsequently rewinding the substrate along the serpentine path in a second direction opposite the first direction to complete a second pass.
29. The method of claim 28, further comprising, in an interval between the first and second passes, switching at least one of the first, second, and third precursor gases to a different precursor gas.
30. The method of claim 22, further comprising introducing a dopant into one of the first, second, and third precursor zones.
31. The method of claim 22, further comprising adjusting a length of at least some of the transits through the first precursor zone.
32. The method of claim 22, further comprising:
exhausting a flow of the first precursor gas from the first precursor zone; and
trapping the exhausted first precursor gas.
33. The method of claim 32, further comprising recycling the trapped first precursor gas into the first precursor zone.
34. The method of claim 22, in which the first and second isolation regions form an isolation zone straddling the third precursor zone.
35. The method of claim 34, further comprising:
paying out the substrate from a coil to a first end of the isolation zone;
coiling the substrate from a second end of the isolation zone opposite the first end.
36. The method of claim 22, further comprising introducing a radical into one of the first, second, and third precursor zones.
37. The method of claim 22, further comprising exhausting gases from the first and third precursor zones at an exhaust pressure lower than respective operating pressures of the first and third precursor zones.
38. The method of claim 22, where generating the first pressure differential includes removing a portion of the inert gas from the first precursor zone, and where generating the second pressure differential includes removing another portion of the inert gas from the third precursor zone.
39. The method of claim 22, where at least two of the precursor zones are contained within a process vessel, and where the pressure differentials related to those two precursor zones are sufficient to inhibit exposure of the substrate to a reactive mixture of the respective precursor gases within the process vessel.
40. A method for depositing a thin film on a flexible substrate, comprising:
introducing a first precursor gas into a first precursor zone;
introducing a second precursor gas into a second precursor zone spaced apart from the first precursor zone, the second precursor gas being different from and reactive with the first precursor gas;
guiding a flexible substrate back and forth between the first and second precursor zones, using a plurality of turning guides at least some of which are located in the first and second precursor zones, and each time through a different one of a series of flow-restricting passageways of an isolation zone that is interposed between the first and second precursor zones, so that:
(i) the substrate transits through the first and second precursor zones and the isolation zone multiple times,
(ii) the first precursor gas adsorbs to the surface of the substrate during transit of the substrate through the first precursor zone, and
(iii) during a subsequent transit of the substrate through the second precursor zone the second precursor gas reacts with the adsorbed first precursor at the surface of the substrate to deposit a thin film on the substrate;

introducing an inert gas into the isolation zone; and
removing a portion of the inert gas from the first precursor zone so that inert gas flows into the first precursor zone from the isolation zone, thereby inhibiting migration of the first precursor gas out of the first precursor zone.
41. The method of claim 40, where the first and second precursor zones are included in a process vessel, and where inhibiting migration of the first precursor gas includes inhibiting exposure of the substrate to a reactive mixture of nonadsorbed amounts of the first and second precursor gases within the process vessel.
42. A method for depositing a thin film on a flexible substrate, comprising:
introducing a first precursor gas into a first precursor zone;
introducing a second precursor gas into a second precursor zone spaced apart from the first precursor zone, the second precursor gas being different from the first precursor gas;
introducing an inert gas into an isolation zone interposed between the first and second precursor zones;
in a process vessel comprising the first and second precursor zones and the isolation zone, guiding a flexible substrate back and forth between the first and second precursor zones, using a plurality of turning guides at least some of which are located in the first and second precursor zones, and each time through the isolation zone and through a different one of a series of flow-restricting passageways of the isolation zone, so that the substrate transits the first and second precursor zones and the isolation zone multiple times; and
building up a thin film on a surface of the substrate via reaction of amounts of each precursor adsorbed on the surface from multiple, sequential transits of the first and second precursor zones without exposing the substrate to a reactive mixture of non-adsorbed amounts of the precursors within the process vessel.
43. The method of claim 42, further comprising:
removing a portion of the inert gas from the first precursor zone so that inert gas flows into the first precursor zone from the isolation zone, inhibiting migration of the first precursor gas out of the first precursor zone, thereby inhibiting exposure of the substrate to a reactive mixture of non-adsorbed amounts of the precursors within the process vessel.

1460706552-767eec02-ae20-42ed-b818-00e2fd712114

1. A computer program product embodied on a computer readable medium, comprising:
computer code for communicating with a mobile device having a wireless communication channel, utilizing a vehicular assembly; and
computer code for performing at least one vehicular assembly function, utilizing the wireless communication channel of the mobile device.
2. The computer program product of claim 1, wherein the communication between the mobile device and the vehicular assembly is wired.
3. The computer program product of claim 1, wherein the communication between the mobile device and the vehicular assembly is wireless.
4. The computer program product of claim 1, wherein the at least one vehicular assembly function utilizes data received over the wireless communication channel.
5. The computer program product of claim 4, wherein the data includes updated traffic data.
6. The computer program product of claim 4, wherein the data includes updated roadway data.
7. The computer program product of claim 4, wherein the data includes social network data.
8. The computer program product of claim 7, wherein the social networking data includes a location of predetermined persons.
9. The computer program product of claim 7, wherein the social networking data includes a destination of predetermined persons.
10. The computer program product of claim 7, wherein the social networking data includes a traveling speed of predetermined persons.
11. The computer program product of claim 4, wherein the data is automatically provided.
12. The computer program product of claim 4, wherein a user requests the data.
13. The computer program product of claim 12, wherein the user requests the data using functionality associated with the vehicular assembly.
14. The computer program product of claim 1, wherein the at least one vehicular assembly function includes a navigation function.
15. The computer program product of claim 1, wherein the at least one vehicular assembly function includes a communication function between a local person and a remote person.
16. The computer program product of claim 1, wherein the at least one vehicular assembly function includes a display function.
17. The computer program product of claim 1, wherein the at least one vehicular assembly function includes an audible function.
18. The computer program product of claim 1, wherein the at least one vehicular assembly function utilizes GPS data received by the vehicular assembly.
19. The computer program product of claim 1, wherein the wireless communication channel includes a broadband wireless channel.
20. The computer program product of claim 1, wherein the wireless communication channel includes a cellular wireless channel.
21. A method, comprising:
communicating with a mobile device having a wireless communication channel, utilizing a vehicular assembly; and
performing at least one vehicular assembly function, utilizing the wireless communication channel of the mobile device.
22. A vehicular assembly system, comprising:
an interface for communicating with a mobile device having a wireless communication channel, utilizing a vehicular assembly; and

a processor for performing at least one vehicular assembly function, utilizing the wireless communication channel of the mobile device.

The claims below are in addition to those above.
All refrences to claims which appear below refer to the numbering after this setence.

1. A DCAC power inverter control unit of a resonant power converter circuit, wherein said power converter circuit comprises two independent DCAC power inverter stages for supplying a multi-primary winding transformer and wherein said DCAC power inverter stages are inductively coupled by a first and a second winding of an interphase transformer which is designed to balance differences in output currents (I1, I2) of the two DCAC power inverter stages.
2. The DCAC power inverter control unit according to claim 1,
wherein said resonant power converter circuit is a DCDC converter for use in a high-voltage generator circuitry.
3. The DCAC power inverter control unit according to claim 2,
wherein said multi-primary winding transformer is designed for high-voltage operation.
4. The DCAC power inverter control unit according to claim 3,
wherein said high-voltage generator circuitry serves for supplying an output power for an X-ray radiographic imaging system, 3D rotational angiography device or X-ray computed tomography device of the fan- or cone-beam type.
5. The DCAC power inverter control unit according to claim 1,
wherein said DCAC power inverter control unit is adapted to minimize a magnitude of the inverter output currents’ difference value (\u0394I) to a value which ensures that the interphase transformer is not operated in a saturated state by controlling switching states andor switching times of the DCAC power inverter stages dependent on this current difference (\u0394I), thus enabling zero current operation.
6. The DCAC power inverter control unit according to claim 5,
wherein the first winding of the interphase transformer is connected in series to at least one resonant tank circuit serially connected to a first primary winding of the multi-winding transformer at an output port of a first one of said DCAC power inverter stages and wherein the second winding of the interphase transformer is connected in series to at least one further resonant tank circuit serially connected to a second primary winding of the multi-winding transformer.
7. A resonant power converter circuit comprising two independent DCAC power inverter stages for supplying a mufti-primary winding transformer, wherein said DCAC power inverter stages are inductively coupled by a first and a second winding of an interphase transformer which is designed to balance differences in output currents (I1, I2) of the two DCAC power inverter stages.
8. The resonant power converter circuit according to claim 7,
wherein said resonant power converter circuit is a DCDC converter for use in a high-voltage generator circuitry.
9. The resonant power converter circuit according to claim 8,
wherein said mufti-primary winding transformer is designed for high-voltage operation.
10. The resonant power converter circuit according to claim 9,
wherein said high-voltage generator circuitry serves for supplying an output power for an X-ray radiographic imaging system, 3D rotational angiography device or X-ray computed tomography device of the fan- or cone-beam type.
11. The resonant power converter circuit according to claim 7,
comprising a DCAC power inverter control unit which is adapted to minimize a magnitude of the inverter output currents’ difference value (\u0394I) to a value which ensures that the interphase transformer is not operated in a saturated state by controlling switching states andor switching times of the DCAC power inverter stages dependent on this current difference (\u0394I), thus enabling zero current operation.
12. The resonant power converter circuit according to claim 11,
wherein the first winding of the interphase transformer is connected in series to at least one resonant tank circuit serially connected to a first primary winding of the multi-winding transformer at an output port of a first one of said DCAC power inverter stages and wherein the second winding of the interphase transformer is connected in series to at least one further resonant tank circuit serially connected to a second primary winding of the multi-winding transformer.
13. A device selected from a group consisting of an X-ray radiographic imaging system, a 3D rotational angiography device, and an X-ray computed tomography device, comprising a resonant power converter circuit for supplying an output power for use in a high-voltage generator circuitry which provides a supply voltage for operating an X-ray tube, wherein said resonant power converter circuit comprises two independent DCAC power inverter stages for supplying a multi-primary winding transformer and wherein said DCAC power inverter stages are inductively coupled by a first and a second winding of an interphase transformer which is designed to balance differences in output currents (I1, I2) of the two DCAC power inverter stages.
14. The device according to claim 13, further comprising:
a DCAC power inverter control unit which is adapted to minimize a magnitude of the inverter output currents difference value (\u0394I) to a value which ensures that the interphase transformer is not operated in a saturated state by controlling switching states andor switching times of the DCAC power inverter stages dependent on this current difference (\u0394I), thus enabling zero current operation.
15. The device according to claim 14,
wherein the first winding of the interphase transformer is connected in series to at least one resonant tank circuit serially connected to a first primary winding of the multi-winding transformer at an output port of a first one of said DCAC power inverter stages and wherein the second winding of the interphase transformer is connected in series to at least one further resonant tank circuit serially connected to a second primary winding of the multi-winding transformer.
16. A method for controlling a resonant power converter circuit for supplying an output power for use in a high-voltage generator circuitry of an X-ray radiographic imaging system, 3D rotational angiography device or X-ray computed tomography device of the fan- or cone-beam type, said resonant power converter circuit comprising two independent DCAC power inverter stages for supplying a multi-primary winding transformer and said DCAC power inverter stages being inductively coupled by a first and a second winding of an interphase transformer for balancing differences in resonant output currents (I1, I2) of the two DCAC power inverter stages, wherein said first winding is connected in series to a first primary winding of the mufti-winding transformer at an output port of a first one of said DCAC power inverter stages and wherein said second winding is connected in series to a second primary winding of the multi-winding transformer,
said method comprising the steps of
continuously detecting the two inverters’ resonant output currents (I1, I2) during an initiated X-ray imaging session while symmetrizing current flows at the output ports of the two DCAC power inverter stages by using said interphase transformer,
calculating a magnitude of a current difference (\u0394I) which is obtained by subtracting the resonant current (I2) at an port of a second one of the two DCAC power inverter stages from the resonant current (I1) at the output port of the first one of these two DCAC power inverter stages, and
controlling switching states andor switching times of the two DCAC power inverter stages dependent on the calculated difference (\u0394I) of the detected inverter output currents (I1, I2) such that said current difference takes on a minimum value which ensures that the interphase transformer is not operated in a saturated state, thus enabling zero current operation.
17. A non-transitory computer program product for implementing a method of controlling a resonant power converter circuit supplying an output power for use in a high-voltage generator circuitry of an X-ray radiographic imaging system, 3D rotational angiography device or X-ray computed tomography device of the fan- or cone-beam type when running on an operational control unit of such a system or device,
wherein said resonant power converter circuit comprises two independent DCAC power inverter stages for supplying a multi-primary winding transformer and said DCAC power inverter stages being inductively coupled by a first and a second winding of an interphase transformer for balancing differences in resonant output currents (I1, I2) of the two DCAC power inverter stages, wherein said first winding is connected in series to a first primary winding of the multi-winding transformer at an output port of a first one of said DCAC power inverter stages and wherein said second winding is connected in series to a second primary winding of the muiti-winding transformer,
said computer program product executing the steps of
calculating a magnitude of a current difference (\u0394I) which is obtained by subtracting the resonant current (I2) detected at an output port of a second one of the two DCAC power inverter stages from the resonant current (I1) detected at the output port of the first one of these two DCAC power inverter stages, said currents being symmetrized by means of said interphase transformer, and
controlling switching states andor switching times of the two DCAC power inverter stages dependent on the calculated difference (\u0394I) of the detected inverter output currents (I1, I2) such that said current difference takes on a minimum value which ensures that the interphase transformer is not operated in a saturated state, thus enabling zero current operation.