CN204834564U - Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier - Google Patents
Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier Download PDFInfo
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- CN204834564U CN204834564U CN201520626829.2U CN201520626829U CN204834564U CN 204834564 U CN204834564 U CN 204834564U CN 201520626829 U CN201520626829 U CN 201520626829U CN 204834564 U CN204834564 U CN 204834564U
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- anode
- microchannel
- microchannel plate
- positive pole
- transmission
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Abstract
Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier belongs to the photoelectrical technique field. Prior art need use three optical antenna, and this makes optical transmitter and receiver volume and weight obviously increase, and the structure is complicated, and it is very big to debug the degree of difficulty. The utility model discloses its component parts includes window, photocathode, microchannel plate, positive pole, and microchannel plate has multistagely, and it has the voltage that the direction is the same to add between photocathode, microchannel plate at different levels, positive pole, by positive pole output photocurrent, a serial communication port, the positive pole comprises transmission -type positive pole, positive pole microchannel plate, the quick positive pole in position, transmission -type positive pole, the quick positive pole in position lie in respectively positive pole microchannel plate openly, the back, the electron beam focusing extremely lies in between last one -level microchannel plate and the transmission -type positive pole, by transmission -type positive pole output laser communication pilot light photocurrent, laser communication fixes a position bare electric current by the output of the quick positive pole in position. Trail the essence and unite two into one with communication to reduced by an optical antenna.
Description
Technical field
The utility model relates to a kind of microchannel photomultiplier for space optical communication with composite waveguide anode, belongs to field of photoelectric technology.
Background technology
In laser space communication process, in order to realize the milliradian even fine registration of microradian magnitude, the laser communication optical transmitter and receiver used have employed two-stage combined type APT system (acquiringtrackingpointing, acquisition and tracking is aimed at).So-called two-stage combined type APT system comprises rough tracking and follows the tracks of two parts with essence.Rough tracking part is that CCD looks in the distance automatic tracking system, and smart tracking section is the high speed tracking system that PZT (quick titling mirror) coordinates 4QD (4 quadrant detector).Rough tracking completes the coarse alignment to beacon beam, makes optical transmitter and receiver target maintain CCD field of view center scope, so guarantee target can not fly out essence follow the tracks of field range.Essence is followed the tracks of by 4QD detector high-speed inspection Communication ray, and according to result of detection control PZT adjustment in real time Communication ray light path, is maintained in field of view of receiver by Communication ray.Rough tracking follows the tracks of with essence the optical antenna that two parts respectively have oneself.To set up between the optical transmitter and receiver participating in communication and while keeping fine registration, import microchannel photomultiplier (MCP-PMT) into by another optical antenna received communication light, realized opto-electronic conversion and the enhancing of Communication ray by microchannel photomultiplier.Its structure of existing microchannel photomultiplier is, window, photocathode, microchannel plate, anode is followed successively by from light incident direction, microchannel plate has multistage, as 2 ~ 3 grades, anode is positioned at the rear end face of afterbody microchannel plate, described anode is transmission anode, is added with the identical high pressure in direction between photocathode, microchannel plate at different levels, anode, by anode output photoelectric stream.
Very necessary owing to arranging two-stage combined type APT system, in laser communication optical transmitter and receiver, three simultaneous reality of optical antenna almost cannot change, this makes optical transmitter and receiver volume and weight obviously increase, structure also becomes complicated certainly, debuging of these optical antennas, comprise the precision adjustment of three optical axises, difficulty is very large.
Utility model content
In order to reduce the quantity of optical antenna in laser communication optical transmitter and receiver, we have invented a kind of microchannel photomultiplier for space optical communication with composite waveguide anode, the microchannel photomultiplier of the utility model is while reception, conversion, strengthening laser communication signal, essence can be realized follow the tracks of, compared to prior art, smart tracking and communication is united two into one, decreases an optical antenna.
Its part of microchannel photomultiplier having a composite waveguide anode for space optical communication of the utility model comprises window, photocathode, microchannel plate, anode, microchannel plate has multistage, the identical voltage in direction is added with, by anode output photoelectric stream between photocathode, microchannel plate at different levels, anode; It is characterized in that, described anode is made up of transmission anode, anode microchannel plate, position-sensitive anode, transmission anode, position-sensitive anode lay respectively at anode microchannel plate front, the back side, Electron Beam Focusing pole is between afterbody microchannel plate and transmission anode, by transmission anode Output of laser signal of communication light photoelectric current, locate light photoelectric current by the communication of position-sensitive anode Output of laser.
Its technique effect of the utility model is, when laser space communication optical transmitter and receiver adopt the utility model there is the microchannel photomultiplier of composite waveguide anode time, still complete the coarse alignment to beacon beam by rough tracking system, make optical transmitter and receiver target maintain CCD field of view center scope, so guarantee target can not fly out essence follow the tracks of field range.The incident microchannel photomultiplier optical antenna of Communication ray, focuses on photocathode surface, concurrent raw opto-electronic conversion.Photocathode is according to incoming communications light light spot shape electron emission, and these electronics accelerating impact microchannel plate step by step under highfield effect, electron multiplication occurs, and forms high energy electron cloud.This high energy electron cloud continues acceleration and hits transmission anode under the effect of highfield.The effect of Electron Beam Focusing pole is modulation high energy electron cloud wavefront, makes it converge, improves energy density, project afterwards on transmission anode.Most of electronics in the high energy electron cloud that kinetic energy is high is transmitted formula anode and collects, and Output of laser signal of communication light photoelectric current, complete the extraction of laser communication signal.Fraction electron transit transmission anode in the high energy electron cloud that kinetic energy is high, electron multiplication is again obtained afterwards in the process by anode microchannel plate, finally collected by position-sensitive anode, and Output of laser communication location light photoelectric current, the optical axis completing incoming communications light thus is accurately located.Visible, the composite waveguide anode be made up of transmission anode, anode microchannel plate, position-sensitive anode makes the microchannel photomultiplier in optical transmitter and receiver while reception, conversion, strengthening laser communication signal, essence can be realized follow the tracks of, compared to prior art, smart tracking and communication is united two into one, thus decreases an optical antenna.
Accompanying drawing explanation
Fig. 1 is the microchannel photomultiplier structural representation for space optical communication with composite waveguide anode of the utility model, and this figure doubles as Figure of abstract.Fig. 2 is a kind of position sensing structure of the position-sensitive anode in the utility model---spline shape structural representation.
Embodiment
Its part of microchannel photomultiplier having a composite waveguide anode for space optical communication of the utility model comprises window 1, photocathode 2, microchannel plate 3, anode, as shown in Figure 1, microchannel plate 3 has multistage, the identical voltage in direction is added with, by anode output photoelectric stream between photocathode 2, microchannel plate at different levels 3, anode.Described anode is made up of transmission anode 4, anode microchannel plate 5, position-sensitive anode 6, transmission anode 4, position-sensitive anode 6 lay respectively at anode microchannel plate 5 front, the back side, Electron Beam Focusing pole 7 is between afterbody microchannel plate 3 and transmission anode 4, by transmission anode 4 Output of laser signal of communication light photoelectric current, locate light photoelectric current by the communication of position-sensitive anode 6 Output of laser.
Described photocathode 2 thickness is 5mm, and diameter is 25mm, is a kind of GaAs photocathode.
Described microchannel plate 3 diameter is 27mm, and effective aperture is 18.4mm, and passage aperture is 6 μm, and access opening is apart from being 8 μm, and thickness is 0.3mm, and draw ratio is 50, is a kind of microchannel plate with ion feedback preventing film, and its photoelectron incident end face sputters the SiO having 4nm thick
2layer.
Described Electron Beam Focusing pole 7 is by two identical copper ring plates coaxially to be formed from the mode of arrangement, and described copper ring plate external diameter is 29.5mm, and internal diameter is 24.5mm, and thickness is 2mm, and copper disk surfaces sputters SiO
2layer.
Described transmission anode 4 is 0.4 μm of thick Al film, is plated in anode microchannel plate 5 front.
Described anode microchannel plate 5 diameter is 27mm, and effective aperture is 18.4mm, and passage aperture is 6 μm, and access opening is apart from being 8 μm, and thickness is 0.3mm, and draw ratio is 50.
Described position-sensitive anode 6 is 2 μm of thick Cu films, and be plated in anode microchannel plate 5 back side, Cu film surface sputtering has SiO
2layer.The position sensing structure of position-sensitive anode 6 has two kinds.
One is four-quadrant construction, the Cu film of position-sensitive anode 6 is divided into four regions insulated from each other by the cross raceway groove of 20 μm wide, the photoelectric current exported by these four regions insulated from each other is tried to achieve laser communication according to quadrant detection method and is located light facula position, and then coaxially regulates and controls.
Another kind is wedge strip structure, and as shown in Figure 2, the Cu film of position-sensitive anode 6 is divided into three regions insulated from each other by the wedge strip-shaped channel of 20 μm wide, is defined as W quadrant, S quadrant, Z quadrant respectively; W quadrant by one group of mutual conduction, shape is identical, measure-alike, axis spacing is identical, the wedge area of axis being parallel forms, the axis of described wedge area is parallel with Y direction, the Y-axis coordinate figure at the tip of each wedge area is identical, and the direction from the tip of wedge area to tail end is identical with Y direction; S quadrant by one group of mutual conduction, shape is identical, length is identical, axis spacing is identical, the bar-shaped zone of axis being parallel forms, the axis of described bar-shaped zone is parallel with Y direction, the Y-axis coordinate figure of the lower end of each bar-shaped zone is identical, and the width along each bar-shaped zone of X-direction increases gradually; Each wedge area described and each bar-shaped zone described intert and distribute, and the region between each wedge area described and each bar-shaped zone described is Z quadrant.By the photoelectric current I that described three regions insulated from each other export
w, I
s, I
zthe absolute position (x, y) of laser communication location light spot center is calculated by following formula:
And then coaxially regulate and control.
Described photocathode 2 approaches with first order microchannel plate 3, and afterbody microchannel plate 3 is positioned at beyond Electron Beam Focusing pole 7 object space two times of focal lengths, and transmission anode 4 is positioned in the image planes of Electron Beam Focusing pole 4.
Pressure reduction between photocathode 2 and first order microchannel plate 3 incident end face is 300V; Pressure reduction between each microchannel plate 3 incident end face and outgoing end face is 1000V; Pressure reduction between afterbody microchannel plate 3 outgoing end face and the previous copper ring plate of Electron Beam Focusing pole 7 is 2000V; Pressure reduction between two copper ring plates of Electron Beam Focusing pole 7 is 1000V; Pressure reduction between a rear copper ring plate of Electron Beam Focusing pole 7 and transmission anode 4 is 3000V; Pressure reduction between transmission anode 4 and position-sensitive anode 6 is 600V.
Claims (8)
1. one kind has the microchannel photomultiplier of composite waveguide anode for space optical communication, its part comprises window, photocathode, microchannel plate, anode, microchannel plate has multistage, the identical voltage in direction is added with, by anode output photoelectric stream between photocathode, microchannel plate at different levels, anode; It is characterized in that, described anode is made up of transmission anode, anode microchannel plate, position-sensitive anode, transmission anode, position-sensitive anode lay respectively at anode microchannel plate front, the back side, Electron Beam Focusing pole is between afterbody microchannel plate and transmission anode, by transmission anode Output of laser signal of communication light photoelectric current, locate light photoelectric current by the communication of position-sensitive anode Output of laser.
2. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 1, it is characterized in that, described Electron Beam Focusing pole (7) is by two identical copper ring plates coaxially to be formed from the mode of arrangement, and copper disk surfaces sputters SiO
2layer.
3. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 1, is characterized in that, described transmission anode (4) is one deck Al film, is plated in anode microchannel plate (5) front.
4. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 1, it is characterized in that, described position-sensitive anode (6) is one deck Cu film, is plated in anode microchannel plate (5) back side, and Cu film surface sputtering has SiO
2layer.
5. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 4, it is characterized in that, the position sensing structure of position-sensitive anode (6) is four-quadrant construction, and the Cu film of position-sensitive anode (6) is divided into four regions insulated from each other by cross raceway groove.
6. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 4, it is characterized in that, the position sensing structure of position-sensitive anode (6) is wedge strip structure, the Cu film of position-sensitive anode (6) is divided into three regions insulated from each other by wedge strip-shaped channel, is defined as W quadrant, S quadrant, Z quadrant respectively; W quadrant by one group of mutual conduction, shape is identical, measure-alike, axis spacing is identical, the wedge area of axis being parallel forms, the axis of described wedge area is parallel with Y direction, the Y-axis coordinate figure at the tip of each wedge area is identical, and the direction from the tip of wedge area to tail end is identical with Y direction; S quadrant by one group of mutual conduction, shape is identical, length is identical, axis spacing is identical, the bar-shaped zone of axis being parallel forms, the axis of described bar-shaped zone is parallel with Y direction, the Y-axis coordinate figure of the lower end of each bar-shaped zone is identical, and the width along each bar-shaped zone of X-direction increases gradually; Each wedge area described and each bar-shaped zone described intert and distribute, and the region between each wedge area described and each bar-shaped zone described is Z quadrant.
7. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 1, it is characterized in that, described photocathode (2) and first order microchannel plate (3) approach, afterbody microchannel plate (3) is positioned at beyond Electron Beam Focusing pole (7) object space two times of focal lengths, and transmission anode (4) is positioned in the image planes of Electron Beam Focusing pole (4).
8. the microchannel photomultiplier for space optical communication with composite waveguide anode according to claim 1, is characterized in that, the pressure reduction between photocathode (2) and first order microchannel plate (3) incident end face is 300V; Pressure reduction between each microchannel plate (3) incident end face and outgoing end face is 1000V; Pressure reduction between the previous copper ring plate of afterbody microchannel plate (3) outgoing end face and Electron Beam Focusing pole (7) is 2000V; Pressure reduction between two copper ring plates of Electron Beam Focusing pole (7) is 1000V; Pressure reduction between a rear copper ring plate of Electron Beam Focusing pole (7) and transmission anode (4) is 3000V; Pressure reduction between transmission anode (4) and position-sensitive anode (6) is 600V.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520626829.2U CN204834564U (en) | 2015-08-19 | 2015-08-19 | Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier |
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|---|---|---|---|
| CN201520626829.2U CN204834564U (en) | 2015-08-19 | 2015-08-19 | Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier |
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| CN204834564U true CN204834564U (en) | 2015-12-02 |
Family
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| CN201520626829.2U Withdrawn - After Issue CN204834564U (en) | 2015-08-19 | 2015-08-19 | Be used for space optical communications to have compound waveguide anodal microchannel photomultiplier |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105070629A (en) * | 2015-08-19 | 2015-11-18 | 长春理工大学 | Micro-channel photomultiplier with composite waveguide anode for spatial optical communication |
-
2015
- 2015-08-19 CN CN201520626829.2U patent/CN204834564U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105070629A (en) * | 2015-08-19 | 2015-11-18 | 长春理工大学 | Micro-channel photomultiplier with composite waveguide anode for spatial optical communication |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20151202 Effective date of abandoning: 20170613 |
|
| AV01 | Patent right actively abandoned |