CN113804055B - Compact multi-band day and night intelligent sighting telescope system and assembly method - Google Patents
Compact multi-band day and night intelligent sighting telescope system and assembly method Download PDFInfo
- Publication number
- CN113804055B CN113804055B CN202111177362.4A CN202111177362A CN113804055B CN 113804055 B CN113804055 B CN 113804055B CN 202111177362 A CN202111177362 A CN 202111177362A CN 113804055 B CN113804055 B CN 113804055B
- Authority
- CN
- China
- Prior art keywords
- main support
- visible light
- laser ranging
- sensor
- ranging unit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000034 method Methods 0.000 title claims abstract description 12
- 238000012545 processing Methods 0.000 claims abstract description 19
- 238000007789 sealing Methods 0.000 claims abstract description 5
- 230000003287 optical effect Effects 0.000 claims description 17
- 238000009434 installation Methods 0.000 claims description 9
- 238000003384 imaging method Methods 0.000 claims description 8
- 238000012937 correction Methods 0.000 claims description 6
- 230000000007 visual effect Effects 0.000 claims description 6
- 238000005259 measurement Methods 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 238000004891 communication Methods 0.000 claims description 2
- 238000013519 translation Methods 0.000 claims description 2
- 230000007613 environmental effect Effects 0.000 description 7
- 238000001514 detection method Methods 0.000 description 4
- 230000006870 function Effects 0.000 description 3
- 238000003331 infrared imaging Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008447 perception Effects 0.000 description 2
- 238000012549 training Methods 0.000 description 2
- 206010061619 Deformity Diseases 0.000 description 1
- 206010063385 Intellectualisation Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/32—Night sights, e.g. luminescent
- F41G1/34—Night sights, e.g. luminescent combined with light source, e.g. spot light
- F41G1/36—Night sights, e.g. luminescent combined with light source, e.g. spot light with infrared light source
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/06—Rearsights
- F41G1/14—Rearsights with lens
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/06—Rearsights
- F41G1/16—Adjusting mechanisms therefor; Mountings therefor
- F41G1/26—Adjusting mechanisms therefor; Mountings therefor screw
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/46—Sighting devices for particular applications
- F41G1/473—Sighting devices for particular applications for lead-indicating or range-finding, e.g. for use with rifles or shotguns
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Telescopes (AREA)
Abstract
The invention belongs to the technical field of firearm sighting device, and discloses a compact multi-band day and night intelligent sighting telescope system and an assembly method thereof, wherein the system comprises the following components: the device comprises an infrared sensor, a visible light sensor, a laser ranging unit, an electronic eyepiece, an environment measuring sensor, a core processing module, an operation panel module, a photosensitive unit, a WiFi module, an integrated navigation module, an output interface, a battery pack and a shell component; the shell component consists of a main support, a front cover piece, a rear cover piece and an upper cover piece to form a sealing cavity; the infrared sensor, the visible light sensor and the laser ranging unit are fixed at the front end of the main support frame, the core processing module is arranged in the cavity of the main support frame, the photosensitive unit, the battery pack and the electronic eyepiece are arranged at the rear end of the main support frame, and the WiFi module and the integrated navigation module are arranged on the upper cover piece. The infrared/visible light combined use meets the day and night use performance, the core processing module and the environment measuring sensor improve the autonomy and the intelligence of the sighting telescope system, and the system structure is compact.
Description
Technical Field
The invention belongs to the technical field of firearm sights, and relates to a compact multi-band day and night intelligent sighting telescope system and an assembly method.
Background
Along with the continuous promotion of the disfigurement, informatization and intellectualization of the battlefield environment, the development of a new individual firearm aiming system is urgently needed to improve the environmental perception degree of the battlefield, the day and night shooting precision of the rifle, the information interaction capability and response speed of the battlefield environment and reduce the training intensity of the shooter.
In the current electron gun sighting telescope system, the acquisition of target scene information is realized by means of a visible light sensor or an infrared sensor, further, the enhancement and sharpening processing of a target image are carried out by adopting an FPGA, and a simple character forming picture is overlapped and displayed through an electronic eyepiece system. In order to reduce the power consumption and the volume of the system, the electronic sighting telescope system is generally integrated with fewer environmental information sensing sensors, environmental parameters are set in an external input mode, and a corrected sighting cross is obtained by means of a prefabricated table; the system adopts a visible light sensor or an infrared sensor to save power consumption and volume, the acquisition of target scene information under low illumination is difficult to be realized by adopting the visible light sensor alone, but abundant target scene texture information is difficult to be obtained by adopting the infrared sensor alone in daytime; the sighting telescope system does not have the functions of detecting, identifying and tracking targets; conventional boresight systems lack information storage functionality. The problems can be effectively solved by developing the multiband day and night intelligent aiming system.
The multiband day and night intelligent aiming system is integrated with a visible light imaging sensor, an infrared imaging sensor, an environment information sensing sensor, an integrated navigation assembly, a laser ranging unit and a core processing module. The method comprises the steps of acquiring detailed information of a daytime battlefield environment through a visible light imaging sensor, acquiring night battlefield environment information through an infrared imaging sensor, acquiring the distance of a target through a laser ranging unit, acquiring the temperature, humidity, air pressure, altitude and wind speed and direction of the current region where a shooter is located through an environment information sensing sensor, acquiring the posture of the shooter and the geographic position of the shooter through a combined navigation assembly, and finally collecting the acquired information in a core processing module to realize the detection, identification and tracking of the target, further deriving correction required for shooting the target, guiding the shooting of the shooter, and improving the informatization and intelligent degree of a system.
Disclosure of Invention
Object of the invention
The purpose of the invention is that: aiming at an intelligent day and night sighting system, the system realizes compact configuration and low-power consumption integration by integrating and designing a visible light sensor, an infrared sensor, an environment measuring sensor, an integrated navigation assembly, a laser ranging unit and a core processing module, can finish target detection, identification and tracking between day and night, trajectory calculation and correction, realizes a battlefield local area network information sharing function, and improves informatization and intelligent degree of the system.
(II) technical scheme
In order to solve the technical problems, the invention provides a compact multi-band day and night intelligent sighting telescope system, which comprises an infrared sensor, a visible light sensor, a laser ranging unit, an electronic eyepiece, an environment measuring sensor, a core processing module, an operation panel module, a photosensitive unit, a WiFi module, an integrated navigation module, an output interface, a battery pack and a shell component.
The shell component consists of a main support frame, a front cover piece, a rear cover piece and an upper cover piece, and forms a sealing cavity; the infrared sensor, the visible light sensor and the laser ranging unit are fixedly arranged at the front end of the main support, the photosensitive unit, the electronic eyepiece and the battery pack are arranged at the rear end of the main support, the core processing module is arranged in the cavity of the main support, the output interface is assembled on the side wall of the main support, the WiFi module, the combined navigation module and the operation panel module are arranged on the upper cover piece, and the environment measuring sensor is arranged on the front cover piece. The visible light sensor consists of a TV detector and a TV lens, and is fixedly assembled with the main support respectively.
The environmental measurement sensor is capable of measuring environmental humidity, temperature, and barometric pressure information.
The detector of the visible light sensor can be adjusted in a translational manner relative to the lens in a direction perpendicular to the optical axis.
The visual sensor is consistent with the visual field and the optical axis of the infrared sensor, and the optical axis is parallel to the optical axis of the laser ranging unit.
The core processing module has the capability of detecting, identifying and tracking targets and the capability of trajectory calculation and correction.
The invention also provides a compact multiband day and night intelligent sighting telescope assembly method, which comprises the following steps: when the laser ranging device is assembled, the main support frame is installed in the direction of reference, and the laser ranging unit is installed so that the optical axis direction of the laser ranging unit is consistent with the direction of the main support frame; the infrared sensor is fixed with the main support frame in a shaft hole matching and end face locking mode; a TV lens of the visible light sensor is fixed with the main support frame in a shaft hole matching and end face locking mode; assembling a TV detector of the visible light sensor on the main support, and adjusting the TV detector to enable a scene in the visual field of the visible light sensor to be consistent with a scene in the visual field of the infrared sensor; adjusting the aiming electric cross center of the infrared sensor and the visible light sensor to a position coincident with the optical axis of the laser by means of a reflective collimator through an imaging electronic adjustment method; the electronic eyepiece is fixed with the main support through shaft hole matching and end face locking, and the core processing module is arranged in the main support frame. The battery pack is arranged at the rear end of the main support frame, the output interface is assembled on the side wall of the main support frame, the WiFi module, the integrated navigation module and the operation panel module are arranged on the upper cover member, the environment measuring sensor is arranged on the front cover member, and the front cover member, the upper cover member and the rear cover member are arranged on the main support frame in a sealing mode, so that sealing assembly is achieved.
(III) beneficial effects
The compact multi-band day and night intelligent sighting telescope system and the assembling method provided by the technical scheme aim to solve the problems that the day and night use of a firearm sighting telescope is limited and the intelligent degree is low. The device integrates a visible light imaging sensor, an infrared imaging sensor, an environment measuring sensor, an integrated navigation assembly, a laser ranging unit and a core processing module, so that the day and night use function of the system is realized, and the all-weather combat corresponding capability is improved; acquiring the distance of a target by means of a laser ranging unit, acquiring the temperature, humidity, air pressure, altitude and wind speed and direction of the current shooter region by means of an environment measuring sensor, acquiring the posture of a gun and the geographical position of the shooter by means of an integrated navigation assembly, and finally collecting the acquired information in a core processing module to realize the detection, identification and tracking of the target, automatically acquire the correction required by the shooting of the target, improve the perception capability of an operator to the environment, reduce the training intensity and realize the real-time information sharing of a battlefield; through the integrated design of multiple sensors, the volume weight of the system is reduced, and the operability of the system is improved.
Drawings
FIG. 1 is a three-dimensional block diagram of a compact multi-band diurnal intelligent telescope system of the present invention;
FIG. 2 is an exploded view of the structure of the compact multi-band diurnal intelligent telescope system of the present invention;
FIG. 3 is a three-dimensional model of a primary support frame of the present invention;
FIG. 4 is a three-dimensional model of an assembly fixture of the present invention;
fig. 5 is an assembled schematic view of the compact multi-band diurnal intelligent telescope system of the present invention.
Wherein: the device comprises a 1-infrared sensor, a 2-visible light sensor, a 3-laser ranging unit, a 4-electronic eyepiece, a 5-environment measuring sensor, a 6-core processing module, a 7-operation panel module, an 8-photosensitive unit, a 9-WiFi module, a 10-integrated navigation module, an 11-output interface, a 12-battery pack, a 14-main support frame, a 15-front cover piece, a 16-rear cover piece, a 17-upper cover piece, a 18-TV detector, a 19-TV lens, a 20-output interface cover, a 21-laser fixing frame, a 22-installation adjusting parabolic mirror, a 23-laser target, a 24-assembly tool and a 25-square tube front mirror.
Detailed Description
To make the objects, contents and advantages of the present invention more apparent, the following detailed description of the present invention will be given with reference to the accompanying drawings and examples.
As shown in fig. 1, a three-dimensional structure diagram of the compact multi-band diurnal intelligent sighting telescope system of the present invention includes: the infrared sensor 1, the visible light sensor 2, the laser ranging unit 3, the electronic eyepiece 4, the photosensitive unit 8 and the shell component; the shell component is a sealed cavity, the infrared sensor 1, the visible light sensor 2 and the laser ranging unit 3 are arranged at the front end of the shell component, the detector of the visible light sensor 2 can be adjusted in a translation mode along the direction perpendicular to the optical axis, and the laser ranging unit 3 can perform pitching and azimuth posture adjustment relative to the shell component; the photosensitive unit 8 and the electronic eyepiece 4 are arranged at the rear end of the shell component; the fields of view of the infrared sensor 1 and the visible light sensor 2 are consistent, and the optical axes of the infrared sensor 1, the visible light sensor 2 and the laser ranging unit 3 are parallel.
The housing assembly comprises a main support 14, a front cover 15, a rear cover 16 and an upper cover 17, and the four parts form a sealed cavity; the infrared sensor 1, the visible light sensor 2 and the laser ranging unit 3 are fixedly arranged at the front end of the main support 14, and the photosensitive unit 8 and the electronic eyepiece 4 are arranged at the rear end of the main support 14.
The scope system further includes: the core processing module 6 is arranged in the cavity of the main support frame 14 and is used for carrying out target detection, identification and tracking and carrying out trajectory calculation and correction; an environmental measurement sensor 5 mounted on the front cover 15 for measuring environmental humidity, temperature, and air pressure information; the WiFi module 9, the integrated navigation module 10 and the operation panel module 7 are arranged on the upper cover piece 17 and used for communication, navigation and operation control; an output interface 11, which is assembled on the side wall of the main support frame 14 and is used for connecting external equipment and transmitting data outwards; a battery pack 12 mounted to the rear end of the main support frame 14 for powering the components of the telescope system.
The visual field and the optical axis of the visible light sensor 2 are respectively corresponding to the same as those of the infrared sensor 1.
As shown in fig. 2, an exploded view of the compact multi-band diurnal intelligent sighting telescope system of the present invention, the key components are specifically assembled as follows: the visible light sensor 2 and the infrared sensor 1 are arranged and fixed at the front end of the main supporting frame 14 in a shaft hole matching end face fixing mode; the laser ranging unit 3 and the main support frame 14 are fixedly installed through the laser fixing frame 21, and can perform pitching and azimuth posture adjustment relative to the main support frame 14; the electronic eyepiece 4 is fixedly arranged at the rear end of the main support frame 14 in a shaft hole matching end face fixing mode, and the photosensitive unit 8 is arranged at the rear end of the main support frame 14; the output interface 11 and the output interface cover are mounted on the side wall of the main support 14; the front cover 15, the rear cover 16 and the upper cover 17 are sealingly secured to the main support frame 14 to form a sealed housing assembly.
The visible light sensor 2 comprises a TV detector 18 and a TV lens 19, which are fixedly assembled with the main support 14, respectively, and the TV detector 18 is translationally adjustable with respect to the TV lens 19 in a direction perpendicular to the optical axis.
As shown in fig. 3, a three-dimensional model of the main support frame 14 according to the present invention is shown, the main support frame 14 is made of high-strength aviation aluminum alloy material, the bottom surface of the main support frame is provided with two inclined system installation base surfaces, and the intersection line of the two system installation base surfaces is a system pointing reference, which is used for adjusting the pointing direction of the laser ranging unit 3, the optical axis of the infrared sensor 1 and the optical axis of the visible light sensor 2 in the system, so that the three pointing directions are consistent. The front end face of the main support frame 14 comprises the installation references of the infrared sensor 1, the visible light sensor 2 and the laser ranging unit 3, the middle part of the main support frame 14 is a system electronic bin for installing the core processing module 6, and the rear end of the main support frame 14 is an installation base surface of the electronic eyepiece 4.
As shown in fig. 4, a three-dimensional model of the assembly fixture 24 of the present invention is shown. The top mounting surface of the assembly fixture 24 is attached to two system mounting base surfaces of the main support 14 and is fastened to the main support 14 by screws; one side of the assembly fixture 24 is provided with a leaning surface 1 and a leaning surface 2 which are perpendicular to each other and are parallel to the system pointing reference.
As shown in fig. 5, an assembly scheme of the compact multi-band diurnal intelligent telescope system of the present invention is shown. During assembly, an assembly light path is built, the main support frame 14 is installed and fixed on the assembly tool 24, the perpendicular base surface of the square tube front mirror 25 is tightly adhered to the leaning surface 1 and the leaning surface 2 which are perpendicular to the assembly tool 24, the parabolic mirror 22 is erected and adjusted in front of the system, and the position of the laser target 23 is adjusted, so that the laser target 23 can be clearly observed from the ocular of the square tube front mirror 25. The laser ranging unit 3 is arranged at the installation reference position of the laser ranging unit 3 of the main support 14 through the laser fixing frame 21, so that light emitted by the laser ranging unit 3 is converged on the laser target 23, the posture of the laser ranging unit 3 relative to the main support 14 is adjusted, the laser emitted by the laser ranging unit 3 is converged by the adjusting parabolic mirror 22 and then is focused on the spot center of the laser target 23, the spot center coincides with the dividing cross center in the square tube front mirror 25, and the laser ranging unit 3 is fixed; the infrared sensor 1 and the TV lens 19 of the visible light sensor 2 are assembled on the main support 14 in a shaft hole matching and end surface fixing mode, and the TV detector 18 of the visible light detector 2 is adjusted to enable the imaging scene of the visible light sensor 2 to be identical with the imaging scene of the infrared sensor 1; adjusting digital video electric cross wires of the infrared sensor 1 and the visible light sensor 2 to the center of a light spot on the laser target 23; the electronic eyepiece 4 is fixed on the main support frame 14 in a shaft hole matching and end surface fixing mode, the core processing module 6 is fixed in the inner cavity of the main support frame 14, the photosensitive unit 8, the output interface 11, the battery pack 12 and the output interface cover 20 are installed on the main support frame 14, the environment measuring sensor 5 is installed on the front cover piece, and the WiFi antenna module 9, the integrated navigation module 10 and the operation panel module 7 are installed on the upper cover piece 17; the front cover 15, the upper cover 17 and the rear cover 16 are hermetically mounted on the main support frame 14 to realize a sealed assembly.
The foregoing is merely a preferred embodiment of the present invention, and it should be noted that modifications and variations could be made by those skilled in the art without departing from the technical principles of the present invention, and such modifications and variations should also be regarded as being within the scope of the invention.
Claims (3)
1. A compact multi-band diurnal intelligent telescope system, comprising: the device comprises an infrared sensor (1), a visible light sensor (2), a laser ranging unit (3), an electronic eyepiece (4), a photosensitive unit (8) and a shell component; the shell component is a sealed cavity, the infrared sensor (1), the visible light sensor (2) and the laser ranging unit (3) are arranged at the front end of the shell component, the detector of the visible light sensor (2) can be adjusted in a translation mode along the direction perpendicular to the optical axis, and the laser ranging unit (3) can perform pitching and azimuth posture adjustment relative to the shell component; the photosensitive unit (8) and the electronic eyepiece (4) are arranged at the rear end of the shell component; the visual fields of the infrared sensor (1) and the visible light sensor (2) are consistent, and the optical axes of the infrared sensor (1), the visible light sensor (2) and the laser ranging unit (3) are parallel;
the shell component comprises a main support frame (14), a front cover piece (15), a rear cover piece (16) and an upper cover piece (17), and the four parts form a sealed cavity; the infrared sensor (1), the visible light sensor (2) and the laser ranging unit (3) are fixedly arranged at the front end of the main support (14), and the photosensitive unit (8) and the electronic eyepiece (4) are arranged at the rear end of the main support (14);
the scope system further includes: the core processing module (6) is arranged in the cavity of the main support (14) and is used for detecting, identifying and tracking a target and performing trajectory calculation and correction; an environment measurement sensor (5) mounted on the front cover (15) for measuring information of the environment humidity, temperature and air pressure;
the scope system further includes: the WiFi module (9), the integrated navigation module (10) and the operation panel module (7) are arranged on the upper cover piece (17) and used for communication, navigation and operation control; an output interface (11) which is assembled on the side wall of the main support (14) and is used for connecting external equipment and transmitting data outwards; a battery pack (12) mounted at the rear end of the main support (14) for powering the components of the telescope system;
the fixing mode of the visible light sensor (2) and the infrared sensor (1) and the main support (14) is a shaft hole matching end face fixing mode; the laser ranging unit (3) and the main support frame (14) are fixedly arranged through the laser fixing frame (21), and the laser ranging unit (3) can perform pitching and azimuth posture adjustment relative to the main support frame (14);
the electronic eyepiece (4) is fixedly arranged at the rear end of the main support (14) in a shaft hole matching end face fixing mode, and the photosensitive unit (8) is arranged at the rear end of the main support (14);
the visible light sensor (2) comprises a TV detector (18) and a TV lens (19), which are respectively and fixedly assembled with the main support (14), and the TV detector (18) can be horizontally adjusted along the direction perpendicular to the optical axis relative to the TV lens (19);
the main support frame (14) is made of aviation aluminum alloy materials, two inclined system installation base surfaces are arranged on the bottom surface of the main support frame, and an intersecting line of the two system installation base surfaces is used as a system pointing reference and is used for adjusting the pointing direction of the laser ranging unit (3), the optical axis of the infrared sensor (1) and the optical axis of the visible light sensor (2) in the system so that the three pointing directions are consistent.
2. An assembly method for the compact multi-band diurnal intelligent telescope system as claimed in claim 1, characterized in that the assembly process is: firstly, assembling a main support (14) with an assembling tool (24), attaching a top mounting surface of the assembling tool (24) to two system mounting base surfaces of the main support (14), and fastening the main support (14) through screws; one side of the assembly fixture (24) is provided with a first leaning surface and a second leaning surface which are perpendicular to each other and are parallel to the system pointing reference; the method comprises the steps of sticking a base surface perpendicular to a square tube front mirror (25) and a leaning surface I and a leaning surface II perpendicular to each other of an assembly tool (24), erecting a parabolic mirror (22) in front of a system, and adjusting the position of a laser target (23) so that the laser target (23) is clearly observed from an eyepiece of the square tube front mirror (25); the laser ranging unit (3) is arranged at the installation reference position of the laser ranging unit (3) of the main support (14) through the laser fixing frame (21), light emitted by the laser ranging unit (3) is converged on the laser target (23), the posture of the laser ranging unit (3) relative to the main support (14) is adjusted, laser emitted by the laser ranging unit (3) is converged through the adjustable parabolic mirror (22), then the center of a light spot on the laser target (23) coincides with the center of a division cross in the square tube front mirror (25), and the laser ranging unit (3) is fixed; the method comprises the steps of assembling a TV lens (19) of an infrared sensor (1) and a visible light sensor (2) on a main support (14) in a shaft hole matching and end face fixing mode, and adjusting a TV detector (18) of the visible light detector (2) to enable an imaging scene of the visible light sensor (2) to be identical with an imaging scene of the infrared sensor (1); adjusting digital video electric cross wires of the infrared sensor (1) and the visible light sensor (2) to the center of a light spot on the laser target (23); the electronic eyepiece (4) is fixed on the main support (14) through shaft hole matching and end face fixing, the core processing module (6) is fixed in the inner cavity of the main support (14), the photosensitive unit (8), the output interface (11), the battery pack (12) and the output interface cover (20) are installed on the main support (14), the environment measuring sensor (5) is installed on the front cover (15), and the WiFi module (9), the integrated navigation module (10) and the operation panel module (7) are installed on the upper cover (17); the front cover piece (15), the upper cover piece (17) and the rear cover piece (16) are hermetically mounted on the main support frame (14) to realize sealing assembly.
3. Use of a compact multiband diurnal intelligent telescope system according to claim 1 in the technical field of firearm collimators.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111177362.4A CN113804055B (en) | 2021-10-09 | 2021-10-09 | Compact multi-band day and night intelligent sighting telescope system and assembly method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111177362.4A CN113804055B (en) | 2021-10-09 | 2021-10-09 | Compact multi-band day and night intelligent sighting telescope system and assembly method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113804055A CN113804055A (en) | 2021-12-17 |
| CN113804055B true CN113804055B (en) | 2023-09-26 |
Family
ID=78897482
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111177362.4A Active CN113804055B (en) | 2021-10-09 | 2021-10-09 | Compact multi-band day and night intelligent sighting telescope system and assembly method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113804055B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20240314410A1 (en) * | 2023-03-16 | 2024-09-19 | Lightpath Technologies, Inc. | Thermal imaging including an extended short wave infrared light source |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN213238620U (en) * | 2020-09-30 | 2021-05-18 | 中戈科技有限公司 | Fusion sighting telescope |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5272514A (en) * | 1991-12-06 | 1993-12-21 | Litton Systems, Inc. | Modular day/night weapon aiming system |
| US6204961B1 (en) * | 1995-09-18 | 2001-03-20 | Litton Systems, Inc. | Day and night sighting system |
| CN103676131A (en) * | 2013-12-20 | 2014-03-26 | 河北汉光重工有限责任公司 | High-definition day and night sighting telescope |
| CN105953652A (en) * | 2015-02-11 | 2016-09-21 | 贵州景浩科技有限公司 | Aiming and adjustment method for moving object by using electronic aiming device |
| CN207300050U (en) * | 2017-11-24 | 2018-05-01 | 长沙欣麟餐饮有限公司 | A kind of low-light (level) electronic aiming mirror of day and night compatibility |
| CN109374261B (en) * | 2018-11-22 | 2020-09-11 | 中国航空工业集团公司洛阳电光设备研究所 | Multi-optical-axis consistency detection equipment and method based on target switching |
| CN111609760B (en) * | 2020-06-01 | 2022-07-05 | 中光智控(北京)科技有限公司 | Intelligent sighting telescope shooting time determination method and system |
| CN213021224U (en) * | 2020-09-10 | 2021-04-20 | 浙江荣者光电科技有限公司 | Multifunctional digital night vision sighting telescope |
| CN112378291A (en) * | 2020-09-29 | 2021-02-19 | 江苏北方湖光光电有限公司 | Day and night intelligent sighting device system |
| CN112526489B (en) * | 2020-12-21 | 2023-11-21 | 江苏亮点光电科技有限公司 | Optical axis calibration system and method of laser range finder and laser parameter measurement method |
-
2021
- 2021-10-09 CN CN202111177362.4A patent/CN113804055B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN213238620U (en) * | 2020-09-30 | 2021-05-18 | 中戈科技有限公司 | Fusion sighting telescope |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113804055A (en) | 2021-12-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP7579144B2 (en) | Observation optics with direct active reticle targeting | |
| US8269893B2 (en) | Optical payload electrical system | |
| WO2023134158A1 (en) | Multi-mode aiming device | |
| US20130333266A1 (en) | Augmented Sight and Sensing System | |
| US20120159833A1 (en) | Fire-control system | |
| CN216717147U (en) | Multi-mode sighting device | |
| WO2023134102A1 (en) | Reticle adjustment structure and reticle adjustment method thereof, and multi-mode sighting apparatus | |
| CN210183399U (en) | Infrared and shimmer that possess accurate target positioning function fuse night-time vision device | |
| CN113804055B (en) | Compact multi-band day and night intelligent sighting telescope system and assembly method | |
| CN114205505B (en) | Double-light front aiming device, adjusting method thereof and aiming system | |
| CN111470055A (en) | Photoelectric navigation nacelle and photoelectric navigation system | |
| CN111692916A (en) | Aiming device and aiming method | |
| CN114910919B (en) | Use and target positioning method and device of low-light night vision device | |
| CN205039926U (en) | Automatic aiming system of wheeled combat tank | |
| CN217883616U (en) | Handheld night vision device | |
| CN216086837U (en) | Air command mirror | |
| CN219284494U (en) | Large-area-array refrigeration long-wave thermal infrared imager | |
| CN221303574U (en) | Distance measuring instrument | |
| CN118047062B (en) | Miniaturized unmanned aerial vehicle load based on hyperspectral remote sensing imaging technology | |
| RU2828168C1 (en) | Optical-electronic control system of shipborne artillery installation | |
| US20240070259A1 (en) | Viewing optic with software capabilities implemented by an enabler | |
| US20240068777A1 (en) | Viewing optic with magnification tracking | |
| US20240035778A1 (en) | Illumination device for use with a viewing optic | |
| Randello et al. | Integrated sight: future improvement for Land Warrior | |
| CN117310729A (en) | Distance measuring instrument |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |