1460736641-56a35094-73fe-452f-9d46-2931815bb8ee

1. A method for controlling, from a remote station, a camera on board a mobile station transmitting to the remote station images including at least one target object to be located in a zone explored by the camera, the method comprising:
estimating, with the remote station, a period of latency L between the despatch of a command from the mobile station and the execution of the said command by the mobile station;
transmitting, with the mobile station, a first image acquired by the camera at an instant T-L to the remote station,;
transmitting, with the remote station, a position of the target object in the said-first image to the mobile station; and
comparing, with the mobile station, the position of the target object in the first image with the position of the target object in at least a second image acquired after the first image, wherein if the compared positions are identical in the two images realigned in relation to one another the mobile station transmits the position to the remote station for validation,
and wherein if the compared positions are not identical in the two images, the mobile station determines, in real time, independently, a predicted trajectory of the target object in the second image, and controls the on-board camera in real time in order to track the target object over the predicted trajectory.
2. A method according to claim 1, in which the trajectory of the target object in the second image is determined by a predictive computation according to a position and movement vector of the target object at an instant T-L.
3. A method according to claim 2, characterised in that it also includes the further comprising:
in the remote station:
realigning the first image and the second image;
determining the position and speed vector of all objects moving in the scene observed by the camera;
determining the position and speed vector of the target object in the first image, either among the moving objects, or among background elements;
calculating a prediction of the position and speed of the target object at instant T+L;
transmitting a designated position, the predicted position and the predicted speed vector of the target object to the mobile station.
4. A method according to claim 3, further comprising readjustment of the first image and of the second image by estimation of the a transient homography.
5. A method according to claim 4, further comprising recording the transient homographies, image by image, and an overall position of the mobile objects from instant T-L to instant T+L in the mobile station.
6. A method according to claim 1, in which the latency time L is estimated by time-stamping of data and by synchronization of the said-remote and mobile stations.
7. A method according to claim 1, in which the target object is fixed or mobile.
8. A method according to claim 7, in which if the target object is mobile and if its trajectory leaves the field of view of the camera’s field of view at an instant t between T-L and T+L, the position of the said-target object is estimated in the mobile station by a predictive calculation according to its position and its speed vector at instant t.
9. A method according to claim 1, in which the camera is on board a drone.
10. A method according to claim 1, in which the target object is an individual, a vehicle, or an aircraft.
11. A device for controlling, from a remote station, a camera on board a mobile station transmitting to the remote station images including at least one target object to be located in a zone explored by the camera, the device comprising:
means for estimating the period of latency L between the despatch of a command from the mobile station, and the execution of the command by the said mobile station;
wherein the mobile station comprises:
means for comparing a position of the target object in a first image acquired by the camera at an instant T-L with the position of the object in at least a second image acquired after the first image,
means for predictive calculation, wherein the means for predictive calculation is configured to determine, in real time, a predicted trajectory of the target object in the second image,
means for controlling, in real time, the on-board camera to the target object in the predicted trajectory.
12. A computer program product recorded on a non-transitory recording medium and including instructions to control, when it is executed on a computer, a camera on board a mobile station from a remote station, where the mobile station transmits to the remote station images including at least one target object to be located in a zone explored by the camera,
the computer program product comprising:
a first executable module in the remote station comprising:
computer-readable instructions causing the first executable module to estimate the period of latency L between the despatch of a command from the mobile station and the execution of the command by the mobile station,
computer-readable instructions causing the first executable module to determine the movement from one image to another of the fixed objects and of the mobile objects in order to facilitate the designation of the target object,
a second executable module in the mobile station including:
computer-readable instructions causing the second executable module to compare a position of the target object in a first image acquired by the camera at an instant T-L with the position of the object in at least a second image acquired after the first image,
computer-readable instructions causing the second executable module to determine in real time a predicted trajectory of the target object in the second image, and

computer-readable instructions causing the second executable module to control, in real time, the on-board camera to track the target object in the predicted trajectory.
13. A method according to claim 2, in which the camera is on board a drone.
14. A method according to claim 3, in which the camera is on board a drone.
15. A method according to claim 4, in which the camera is on board a drone.
16. A method according to claim 5, in which the camera is on board a drone.
17. A method according to claim 6, in which the camera is on board a drone.
18. A method according to claim 7, in which the camera is on board a drone.
19. A method according to claim 8, in which the camera is on board a drone.

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

1. A system of introducing a linear accelerator particle beam for low contaminate processing, the system comprising:
a particle accelerator including at least an ion source for generating a plurality of charged particles, and an apparatus for accelerating and confining the plurality of charged particles in a first particle beam, the first particle beam being outputted to a first exit aperture in a first spatial direction;
a beam filter apparatus coupled to the first exit aperture to receive the first particle beam, the beam filter apparatus including a first chamber of a first mass-selection device to process the first particle beam and generate a second particle beam, the second particle beam including substantially a first ionic specie and being outputted to a second exit aperture in a second spatial direction different from the first spatial direction;
an end-station including a second chamber coupled to the beam filter apparatus to receive the second particle beam, the second chamber configured to house a workpiece having a planar surface configured to receive the second particle beam for implanting the first ionic specie.
2. The system of claim 1 further comprising an apparatus configured to perform a controlled cleaving of a film of material from the workpiece, the film having a thickness corresponding to a depth of implantation of the particles from the second beam.
3. The system of claim 1 wherein the first chamber is associated with a first pressure and the second chamber is associated with a second pressure, the first pressure being set to be at least 10\xd7 lower relative to the second pressure.
4. The system of claim 3 wherein the second pressure in the second chamber is about (1\xd710\u22123) torr and lower.
5. The system of claim 1 wherein the apparatus for accelerating and confining the plurality of charged particles in a first particle beam is a linear accelerator (linac) system.
6. The system of claim 5 wherein the linac system comprises a stage selected from a radio frequency quadrupole (RFQ) stage, a RF-Focused Interdigitated (RFI) stage, a Drift-Tube Linac (DTL) stage, or a Quadrupole-Focused Interditigated (QFI) stage.
7. The system of claim 1 wherein the apparatus for accelerating and confining the plurality of charged particles in a first particle beam comprises a cyclotron or a DC electrostatic particle accelerator.
8. The system of claim 1 wherein the first particle beam is in an energy level ranging from 0.5 MeV to 5 MeV.
9. The system of claim 1 wherein the first particle beam comprises the first ionic specie and a plurality of contaminate species originated from either the ion source or generated during the propagation through the linear accelerator.
10. The system of claim 9 wherein the plurality of contaminate species is selected from the group of Hydrogen isotope specie, Helium specie, Oxygen specie, Nitrogen specie, Carbon specie, Aluminum Specie, Iron Specie, Copper Specie, and constituent elements of aluminum and steel alloys.
11. The system of claim 1 wherein the mass-selection device comprises a magnetic sector, an electric sector, or any combination of an electric sector, a magnetic sector, electricmagnetic (E\xd7B), and one or more drift channels.
12. The system of claim 1 wherein the mass-selection device is based on a mechanism for differentiating particles by charge-to-mass ratio.
13. The system of claim 1 wherein the first spatial direction relative to the second spatial direction forms an angle in a horizontal plane or in a vertical plane.
14. The system of claim 13 wherein the angle is about 45 degrees, about 90 degrees, or about 135 degrees.
15. The system of claim 1 wherein the beam filter apparatus is a two-stage mass-selection device further comprising a third chamber housing a second mass-selection device coupled to the first mass-selection device in series to produce the second particle beam.
16. The system of claim 15 wherein the third chamber is associated with a third pressure that is set to be lower relative to the second pressure.
17. The system of claim 1 wherein the end-station is part of a cluster tool configured to integrate with a plurality of chambers including the second chamber.
18. The system of claim 17 wherein the second chamber is configured to couple with one or more load locks for loading inout the workpiece.
19. The system of claim 1 wherein the workpiece is a thick film on a substrate, a tile workpiece, a wafer workpiece, or a bulk workpiece.
20. The system of claim 19 wherein the bulk workpiece comprises a shaped ingot of single-crystalline or polycrystalline silicon, germanium, IIIV group compound semiconductor.
21. The system of claim 20 wherein the plurality of bulk workpieces are loaded on a rack that is movable in a plane allowing the second particle beam effectively scanning over all the planar surfaces of the plurality of bulk workpieces.
22. A system of introducing an accelerator particle beam for low contaminate processing, the system comprising:
a particle accelerator apparatus configured to generate a first particle beam;
a beam filter coupled to the linear accelerator apparatus to receive the first particle beam, the beam filter being in a first chamber and configured to generate a second particle beam with substantially a first ionic specie;
an end-station including a second chamber coupled to the first chamber for extracting the second particle beam, the second particle beam being irradiated onto a planar surface of a workpiece loaded in the second chamber for implanting the first ionic specie.
23. The system of claim 1 further comprising an apparatus configured to perform a controlled cleaving of a film of material from the workpiece, the film having a thickness corresponding to a depth of implantation of the particles from the second beam.
24. The system of claim 22 wherein the first chamber is associated with a first pressure and the second chamber is associated with a second pressure, the first pressure lower relative to the second pressure.
25. The system of claim 24 wherein the second pressure is about 1\xd710\u22123 torr and lower.
26. The system of claim 22 wherein the particle accelerator comprises a RF accelerator such as an RF linac or a cyclotron, or comprises a DC electrostatic accelerator.
27. The system of claim 22 wherein the first particle beam is in an energy level ranging from 1 MeV to 5 MeV.
28. The system of claim 22 wherein the first particle beam comprises the first ionic specie and a plurality of contaminate species originated from either the ion source or generated during the propagation through the linear accelerator.
29. The system of claim 22 wherein the plurality of contaminate species is selected from Hydrogen isotope specie, Helium specie, Oxygen specie, Nitrogen specie, Carbon specie, Aluminum specie, Iron specie, Copper specie, elements of aluminum and steel alloys.
30. The system of claim 22 wherein the beam filter comprises a magnetic sector, an electric sector, or any combination of an electric sector, a magnetic sector, electricmagnetic sectors, and one or more drift channels for separating the first ionic specie from the first particle beam.
31. The system of claim 22 wherein the beam filter is based on a mechanism of generating separate trajectories with different radius of curvature for particles with different charge-to-mass ratio.
32. A method of introducing a accelerator particle beam for low contaminate processing, the method comprising:
generating a plurality of ionic particles by an ion source, the plurality of ionic particles comprising multiple species including a first ionic specie;
accelerating and confining the plurality of ionic particles to a first particle beam with energy level of the first specie at least in a range of 0.5 MeV to 5 MeV using a linear accelerator;
extracting the first particle beam into a first chamber;
processing the first particle beam in the first chamber to separate the first ion specie from the multiple species;
extracting a second particle beam into a second chamber, the second particle beam comprising substantially the first ion specie only;
irradiating the second particle beam to implant the first ion specie into one or more planar surfaces of one or more bulk workpieces loaded in the second chamber.
33. The method of claim 32 wherein the accelerating and confining the plurality of ionic particles to a first particle beam comprises:
extracting the plurality of ionic particles from the ion source through a low energy beam transport unit;
accelerating and confining the plurality of ionic particles in a multi-stage radio frequency (RF) quadrupole (RFQ) linear accelerator (linac), a cyclotron, or a DC electrostatic accelerator; and
generating the first particle beam.
34. The method of claim 32 wherein the processing the first particle beam in the first chamber to separate the first ion specie from the multiple species further comprises:
receiving the first particle beam;
guiding the first particle beam into a beam filter;
guiding the first ionic specie through the beam filter while dumping the rest of the multiple species.
35. The method of claim 34 wherein the beam filter comprises a mass-selection device based on a mechanism for differentiating particles by charge-to-mass ratio.
36. The method of claim 35 wherein the charge-to-mass selection device comprises a combination of one or more electric sectors, one or more magnetic sectors, and one or more drift channels.
37. The method of claim 32 wherein the extracting a second particle beam into a second chamber comprises:
receiving a plurality of first ionic specie particles to form a second particle beam;
outputting the second particle beam through a high-energy beam transport unit at a second exit aperture of the first chamber, the second exit aperture being connected to the second chamber;
expanding optionally the second particle beam to obtain a desired beam diameter.
38. The method of claim 32 wherein the irradiating the second particle beam to implant the first ion specie into one or more planar surfaces comprises:
directing the second particle beam to a spot of the one or more planar surfaces in substantially perpendicular direction;
scanning the second particle beam to move the spot over the entire one or more planar surfaces;
controlling a dosage by adjusting at least a beam current, a beam diameter, and a scanning speed.
39. The method of claim 32 wherein the one or more bulk workpieces can be ingots of single-crystalline or polycrystalline silicon, germanium, IIIV group compound semiconductor, or silicon carbide (SiC).
40. The method of claim 32 wherein the second chamber belongs to a cluster tool configured to perform other processes including surface re-polishing, post-processing, and controlled cleaving or direct film transferring.
41. The method of claim 32 wherein the first chamber is associated with a first pressure and a second chamber is associated with a second pressure.
42. The method of claim 41 wherein the second pressure is about 1\xd710\u22123 torr or lower.
43. The method of claim 42 wherein the first pressure is one or two orders of magnitude lower than the second pressure.
44. The system of claim 1 further comprising a beam scanner configured to alter over time a location that the second particle beam impinges upon the workpiece.
45. The method of claim 32 further comprising translating the bulk workpieces along at least one axis during impingement of the second particle beam.
46. An apparatus comprising:
a linear accelerator having an inlet in vacuum communication with an ion source and an outlet in vacuum communication with an inlet of a beam filter;
an end station in vacuum communication with an outlet of the beam filter and configured to support a target workpiece;
a host computer comprising,
a processor in electronic communication with at least one element selected from the ion source, the linear accelerator, the beam filter, and the end station, and
a computer readable storage medium in electronic communication with the processor and having stored thereon code configured to instruct the processor to,
cause the ion source to generate a plurality of ionic particles comprising multiple species including a first ionic specie,
cause the linear accelerator to accelerate the plurality of ionic particles to a particle beam with energy level of the first specie at least in a range of 0.5 MeV to 5 MeV,
cause the beam filter to process the particle beam in the first chamber to separate the first ion specie from the multiple species, and
irradiate the particle beam to implant the first ion specie into one or more planar surfaces of one or more workpieces loaded in the end station.
47. The apparatus of claim 46 wherein the computer readable storage medium further comprises code to instruct scanning of the first ion species over the surface of the workpiece during the irradiation.
48. The apparatus of claim 46 wherein the computer readable storage medium further comprises code to instruct translation of the workpiece along one or more axes during the irradiation.
49. The apparatus of claim 46 wherein:
the beam filter comprises a first chamber magnetic communication with an analyzing magnet; and
the computer readable storage medium further comprises code to instruct the analyzing magnet to apply a magnetic field to the first chamber.
50. The apparatus of claim 46 wherein the computer readable storage medium further comprises code to instruct that the first chamber to be maintained at a first pressure lower than a second pressure of the end station.
51. A method of forming a thin film, the method comprising:
generating a high energy particle beam;
passing the high energy particle beam through a filter to remove unwanted contamination from the particle beam;
directing the decontaminated particle beam at a surface of a substrate;
forming a cleave region in the substrate from particles implanted from the beam; and
performing a controlled cleaving in the cleave region to remove a thin film of material from the substrate.
52. The method of claim 51 wherein a thickness of the thin film is at least about 10 \u03bcm.

1460736633-84c93c21-c09f-4765-a0eb-a141e6f657c7

1. A leadthrough element for a waterproof leadthrough of a first line, the leadthrough element comprising:
a top and a bottom; and
a first recess extending from the bottom to the top and configured to lead the first line through the leadthrough element,
wherein the leadthrough element is configured such that the first line exits from the top of the leadthrough element in such a way that after exiting, the first line runs flat along the top of the leadthrough element,
wherein the top of the leadthrough element has a groove-shaped indentation located so that the indentation receives the first line immediately after the exit of the first line from the first recess and directs the first line along the top of the leadthrough element.
2. The leadthrough element of claim 1,
wherein the leadthrough element is configured to cause the first line to exit in a first direction from the leadthrough element, and the leadthrough element is configured to cause a second line to exit in a second direction from the leadthrough element, wherein the first direction is opposite to the second direction.
3. The leadthrough element of claim 1,
wherein the first line is comprised of electrical cables, and each cable includes at least one conductor; and
the leadthrough element comprises at least one additional first recess, the first recess and the additional first recess each configured to provide a seat for each of the electrical cables and to provide waterproofness or airtightness of the leadthrough when the electrical cables are subjected to mechanical loads.
4. The leadthrough element of claim 1,
wherein the first recess is configured for leading through a single line.
5. The leadthrough element of claim 1,
wherein the leadthrough element comprises a first and a second component operative to be compressed during installation of the leadthrough element,
the first component comprises a first part of the first recess for leading through the first line,
the second component comprises a second part of the first recess, and
the first and the second parts of the first recess are dimensionally smaller than the first line so that when the first and second components are compressed during installation of the leadthrough element, pressure is exerted onto the first line sufficient to close off the first line so as to provide a tight seal against contact areas of the first recess.
6. The leadthrough element of claim 5,
wherein the first component comprises a plurality of the first recesses, and
the second component comprises projections configured to be received during installation of the leadthrough element in the plurality of the first recesses of the first component so as to prevent slipping of the first and second components in relation to each other.
7. The leadthrough element of claim 1,
wherein the first recess has a contact area, and
the contact area of the first recess comprises an adhesive operative to provide a tight seal of the first line in the first recess.
8. The leadthrough element of claim 1,
wherein the leadthrough element is configured for placement in an opening in a dividing wall, and
wherein outside edges of the leadthrough element form second recesses in the form of grooves in the leadthrough element, such that the second recesses are configured to receive portions of the dividing wall to provide a tight seal.
9. The leadthrough element of claim 1,
wherein the leadthrough element is at least partly made from plastic or metal.
10. The leadthrough element of claim 9,
wherein the plastic is selected from the group consisting of polyamide, silicon, olefin copolymers (EPDM), hard rubber, soft rubber, polyvinyl chloride (PVC) and polypropylene (PP).
11. The leadthrough element of claim 1,
wherein the leadthrough element is configured for installation in a floor of an aircraft and for leading through electrical lines in an aircraft.
12. The leadthrough element of claim 1,
wherein the leadthrough element is designed for installation in a floor of an AIRBUS A380 aircraft and for leading through In Flight Entertainment electrical lines for In Flight Entertainment control devices.
13. The leadthrough element of claim 1,
wherein the first recess has a bent shape configured to provide for the exit of the first line at less than 90 degrees with respect to the top of the leadthrough element.
14. The leadthrough element of claim 1,
wherein the groove-shaped indentation is configured to receive at least most of a depth of the first line.
15. In a combination, the leadthrough element of claim 1 and the first line led through the first recess and out the top of the leadthrough element, the leadthrough element and the first line cooperating such that after exit of the first line, the first line runs flat along the top of the leadthrough element.
16. A leadthrough element for a waterproof leadthrough of a first line, the leadthrough element comprising:
a top and a bottom; and
a first recess extending from the bottom to the top and configured to lead the first line through the leadthrough element;
the leadthrough element is configured such that the first line exits from the top of the leadthrough element in such a way that after exiting, the first line runs flat along the top of the leadthrough element; and
the leadthrough element is further configured to cause the first line to exit in a first direction from the leadthrough element, and the leadthrough element is configured to cause a second line to exit in a second direction from the leadthrough element, wherein the first direction is opposite to the second direction.
17. A leadthrough element for a waterproof leadthrough of a first line, the leadthrough element comprising:
a top and a bottom; and
a first recess extending from the bottom to the top and configured to lead the first line through the leadthrough element, wherein the first line comprises electrical cables, each cable including at least one conductor; and
at least one additional first recess, the first recess and the additional first recess each configured to provide a seat for each of the electrical cables and to provide waterproofness or airtightness of the leadthrough when the electrical cables are subjected to mechanical loads,
the leadthrough element configured such that the first line exits from the top of the leadthrough element in such a way that after exiting, the first line runs flat along the top of the leadthrough element.

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

What is claimed is:

1. A method of insulating an electric motor stator for a pump with resin, the method comprising:
providing a resin fixture comprising a tube comprising longitudinally spaced holes, a first plug at a first end, a second plug at a second end, the second plug including a valve, and a rubber cover over the tube;
placing the resin fixture inside the stator’s bore;
placing a first end plug at a first end of the stator and a second end plug at a second end of the stator;
placing an outer cover around the stator and between the end plugs;
placing a first inner spacer ring at the first end of the stator and a second inner spacer ring at the second end of the stator, the inner spacer rings being placed between lead wires of the stator and the resin fixture adjacent the first and second end plugs;
placing a first outer spacer ring at the first end of the stator and a second outer spacer ring at the second end of the stator, the outer spacer rings being placed between lead wires of the stator and the outer cover adjacent the first and second end plugs;
inflating the rubber cover through the valve; and
providing resin into the outer cover.
2. A method in accordance with claim 1 wherein the outer cover comprises plastic tape wrapped around the stator between the end plugs.
3. A method in accordance with claim 1 wherein the outer cover comprises a mold that comprises a rigid material between the end plugs.
4. A method in accordance with claim 1 wherein the tube comprises metal.
5. A method in accordance with claim 1 wherein the resin is moved over the stator via a vacuum pump coupled to a hole defined in one of the outer spacer rings.
6. A method in accordance with claim 1 wherein the resin is moved over the stator via a pressure pump coupled to a hole defined in one of the outer spacer rings.
7. A method in accordance with claim 1 further comprising coupling the end plugs with support bolts.
8. A resin fixture for insulating an electric motor stator with resin, the resin fixture comprising:
a tube comprising longitudinally spaced holes;
a first plug at a first end of the tube;
a second plug at a second end of the tube, the second plug including a valve; and
a rubber cover over the tube.
9. A resin fixture in accordance with claim 8 wherein the valve is Schrader valve.
10. A resin fixture in accordance with claim 8 further comprising Teflon over the rubber cover.
11. A resin fixture in accordance with claim 8 wherein the rubber cover is coupled to the tube with cement.
12. A resin fixture in accordance with claim 8 wherein the tube comprises metal.
13. A system for insulating an electric motor stator for a pump with resin, the system comprising:
a resin fixture for placement with the stator’s bore, the resin fixture comprising:
a tube comprising longitudinally spaced holes;
a first plug at a first end of the tube;
a second plug at a second end of the tube, the second plug including a valve; and
a rubber cover over the tube;

a first end plug at a first end of the stator and a second end plug at a second end of the stator;
an outer cover around the stator and between the end plugs;
a first inner spacer ring at the first end of the stator and a second inner spacer ring at the second end of the stator, the inner spacer rings being placed between lead wires of the stator and the resin fixture adjacent the first and second end plugs; and
a first outer spacer ring at the first end of the stator and a second outer spacer ring at the second end of the stator, the outer spacer rings being placed between lead wires of the stator and the outer cover adjacent the first and second end plugs.
14. A system in accordance with claim 13 wherein the outer cover comprises plastic tape wrapped around the stator between the end plugs.
15. A system in accordance with claim 13 wherein the outer cover comprises a mold that comprises a rigid material between the end plugs.
16. A system in accordance with claim 13 wherein the tube comprises metal.
17. A system in accordance with claim 13 wherein resin is moved over the stator via a vacuum pump coupled to a hole defined in one of the outer spacer rings.
18. A system in accordance with claim 13 wherein resin is moved over the stator via a pressure pump coupled to a hole defined in one of the outer spacer rings.
19. A system in accordance with claim 13 further comprising support bolts that couple the end plugs to each other.