CN208849864U - A kind of new type auto identification thermal imaging system imaging device - Google Patents

A kind of new type auto identification thermal imaging system imaging device Download PDF

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Publication number
CN208849864U
CN208849864U CN201821597300.2U CN201821597300U CN208849864U CN 208849864 U CN208849864 U CN 208849864U CN 201821597300 U CN201821597300 U CN 201821597300U CN 208849864 U CN208849864 U CN 208849864U
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China
Prior art keywords
imaging system
thermal imaging
thermal
fuselage
card slot
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Active
Application number
CN201821597300.2U
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Chinese (zh)
Inventor
苗俊
王璋
石利荣
刘艳娇
姜昌云
尤志鹏
罗艺
刘立文
钱海
陈皓东
袁齐坤
杨子力
李祥贵
凌维周
严光强
周利奎
胡留方
王强
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Qujing Power Supply Bureau Yunnan Power Grid Co Ltd
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Qujing Power Supply Bureau Yunnan Power Grid Co Ltd
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Priority to CN201821597300.2U priority Critical patent/CN208849864U/en
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Publication of CN208849864U publication Critical patent/CN208849864U/en
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Abstract

The utility model discloses a kind of new type auto identification thermal imaging system imaging devices, including handle component, thermal imaging system, display device, handle component is connect with thermal imaging system by the first clamping structure, thermal imaging system is connect with display device by the second clamping structure, thermal imaging system includes camera lens, fuselage and tail piece, camera lens, tail piece is all made of sealing ring sealing means and is mounted on fuselage both ends, screw connection is coated with silica gel sealing, epoxy resin paint and wax are coated on the shell of fuselage, and thermal window is additionally provided in the shell side of thermal imaging system fuselage, shield is installed outside camera lens, shield and the removable connection of camera lens;The utility model passes through the handle component outside setting; the function of thermal imaging system can be extended; the shell side of fuselage is equipped with thermal window; rotatable cooling fin is equipped at thermal window; it can effectively be radiated; cooling fin can also be rotated to thermal window is completely closed simultaneously, fuselage interior element can be protected.

Description

A kind of new type auto identification thermal imaging system imaging device
Technical field
The utility model is more particularly to a kind of new type auto identification thermal imaging system imaging device.
Background technique
The existing generally existing following problem of thermal imaging system: thermal imaging system in the prior art, due to the limitation of volume, in Portion can not place excessive device.And be integral between existing thermal imaging system display device and thermal imaging system, work as display device It, can not be real-time when shooting certain angle due to the limitation of shooting visual angle for user when being built between thermal imaging system Observe the content of shooting.In addition, there is the storage of display device when to be split type.Existing thermal imaging system camera lens is protected Shield window is not easy to replace, and measure is not effectively protected when being hit by the external world in camera lens;Metal shell outside thermal imaging system It is difficult to work without interruption for a long time under relatively rugged environment, such as in the environment of high humility and highly corrosive gas.
Utility model content
The technical problem to be solved by the utility model is to provide a kind of new type auto identification thermal imaging system imaging devices.
To achieve the goals above, the utility model uses following technical scheme:
A kind of new type auto identification thermal imaging system imaging device, including handle component, thermal imaging system, display device, handle component It is connect with thermal imaging system by the first clamping structure, thermal imaging system is connect with display device by the second clamping structure, and thermal imaging system includes Camera lens, fuselage and tail piece, camera lens, tail piece are all made of sealing ring sealing means and are mounted on fuselage both ends, and screw connection is all It is coated with silica gel sealing, epoxy resin paint and wax are coated on the shell of fuselage, and be additionally provided in the shell side of thermal imaging system fuselage Thermal window, camera lens are equipped with shield, shield and the removable connection of camera lens outside.
Further, the first clamping structure includes the first buckle and the first card slot, the first buckle and the first card slot phase interworking It closes.
Further, the first buckle of the first clamping structure is arranged at handle component, and the first card slot is arranged in thermal imaging system First buckle of place or the first clamping structure is arranged at thermal imaging system, and the first card slot is arranged at handle component.
Further, the second clamping structure includes the second buckle and the second card slot, the second buckle and the second card slot phase interworking It closes.
Further, the second buckle of the second clamping structure is arranged at thermal imaging system, and the second card slot is arranged in display device Place or the second buckle are arranged at display device, and the second card slot is arranged at thermal imaging system.
Further, the second clamping structure includes the toggle being arranged at thermal imaging system, and toggle head is arc-shaped and is equipped with card Slot is provided with torsional spring between toggle and thermal imaging system.
Further, rotatable cooling fin is equipped at thermal window.
The beneficial effects of the utility model are:
(1) the utility model is by the handle component outside setting, using the first clamping structure by thermal imaging system and handle portion Part is clamped, and electric interfaces are arranged in clamping structure, can be extended to the function of thermal imaging system, such as extension battery Capacity increases control function etc., and clamping structure is by the way of buckle and card slot, easy assembly and disassembly.
(2) the utility model is conveniently shown by the second clamping structure of setting by thermal imaging system and the removable connection of display device Display device and thermal imaging system can be separated, release the limitation of shooting angle, expanded by the assembly and disassembly of showing device and thermal imaging system Operator observes the visual range of shooting.Moreover, display device and thermal imaging system separation, facilitate subsequent maintenance and carrying.
(3) the utility model camera lens, tail piece are all made of sealing ring sealing means and are mounted on fuselage both ends, screw connection It is coated with silica gel sealing, epoxy resin paint and wax are coated on the shell of fuselage, thermal imaging system uses all-sealed structure, has good Waterproof and dampproof performance, can protect interior arrangement from corrosion.
(4) shield is installed outside the utility model camera lens, the setting of the removable connection of the two, shield can be effective Prevent direct sunlight camera lens and sleet from drenching camera lens, to ensure that image quality.
(5) shell side of the utility model thermal imaging system fuselage is equipped with thermal window, and being equipped at thermal window can be rotated Cooling fin, cooling fin to thermal window can be rotated and be open maximum, effectively radiated, while cooling fin can also be rotated extremely It completely closes thermal window, when blowing and raining, the protective effect to fuselage interior element can be played.
Detailed description of the invention
Fig. 1 is that the utility model first buckles the structural schematic diagram that handle component is arranged in.
Fig. 2 is that the utility model second buckles the structural schematic diagram that display device is arranged in.
Figure label: handle component 1, thermal imaging system 2, display device 3, camera lens 4, fuselage 5, shield 7, the first buckle 8, the One card slot 9, toggle 11, torsional spring 12, the second buckle 21, the second card slot 22, thermal window 23, cooling fin 24.
Specific embodiment
The technical solution of the utility model is described in further details below in conjunction with attached drawing, it is noted that specific Embodiment is the detailed description to the utility model, is not construed as the restriction to the utility model.
The new type auto identification thermal imaging system imaging device of one kind of the utility model, as shown in Figs. 1-2, including handle component 1, thermal imaging system 2, display device 3, handle component 1 and thermal imaging system 2 are by the removable connection of the first clamping structure, thermal imaging system 2 and aobvious For showing device 3 by the removable connection of the second clamping structure, thermal imaging system includes camera lens 4, fuselage 5 and tail piece, camera lens 4, tail piece It is all made of sealing ring sealing means and is mounted on 5 both ends of fuselage, screw connection is coated with silica gel sealing, applies on the shell of fuselage 5 There are epoxy resin paint and wax, and be additionally provided with thermal window 23 in the shell side of thermal imaging system fuselage 5, is equipped with outside camera lens 4 anti- Shield 7, shield 7 and the removable connection of camera lens 4.The setting of shield 7 can effectively prevent direct sunlight camera lens and sleet Camera lens is drenched, to ensure that image quality.
By the handle component 1 outside setting, thermal imaging system 2 and handle component 1 are clamped using the first clamping structure, And electric interfaces are set in clamping structure, the function of thermal imaging system can be extended, such as extension battery capacity, increase control Function processed etc..
As a preferred mode, the first clamping structure includes the first buckle 8 and first card slot 9, and first buckles 8 and the One card slot 9 cooperates.First 8 both sides of the edge of buckle slope inwardly, and transversal cross-section is trapezoidal, as shown in Figure 1.Clamping structure It is easy to disassemble by the way of buckle and card slot.
As a preferred mode, the first buckle 8 of the first clamping structure is arranged at handle component, the first card slot 9 It is arranged at thermal imaging system or the first buckle 8 of the first clamping structure is arranged at thermal imaging system, the first card slot 9 is arranged in handle At component.The first buckle 8 of the first clamping structure is arranged at handle component in the present embodiment, and the first card slot 9 is arranged in thermal imagery At instrument, as described in Figure 1.
As a preferred mode, the second clamping structure includes the second buckle 21 and the second card slot 22, the second buckle 21 It cooperates with the second card slot 22.The setting of second clamping structure facilitates the assembly and disassembly of display device 3 and thermal imaging system 4, can To separate display device 3 and thermal imaging system 4, the limitation of shooting angle is released, expands the visual range that operator observes shooting. Moreover, display device 3 and thermal imaging system 4 separate, facilitate subsequent maintenance and carrying.
As a preferred mode, the second buckle 21 of the second clamping structure is arranged at thermal imaging system, the second card slot 22 It is arranged at display device 3 or the second buckle 21 is arranged at display device 3, the second card slot 22 is arranged at thermal imaging system 2. The second buckle 21 is arranged at display device 3 in the present embodiment, and the second card slot 22 is arranged at thermal imaging system 2.
As a preferred mode, the second clamping structure includes the toggle 11 being arranged at thermal imaging system fixed column 10, institute State 11 head of toggle it is arc-shaped and be equipped with card slot, torsional spring 12 is provided between toggle 11 and thermal imaging system 4, display device 3 is inserted into heat After picture instrument 4, through the card slot clamping of toggle 11 display device 3, when needing to extract, it is only necessary to stir toggle 11, can incite somebody to action Display device 3 ejects, and then toggle 11 is replied under the restoring force of torsional spring 12.The setting of toggle 11 is convenient for user's operation, letter It is single quick.
As a preferred mode, the first locking device is equipped between handle component and thermal imaging system.Locking device can be with It is locked using mode in the prior art, the setting of locking device can increase between handle component and thermal imaging system after combination Tightness, the combination both made is stronger.
As a preferred mode, the second locking device is equipped between thermal imaging system and display device.Second locking device Can be identical as the first locking device, locking principle is identical;Locking device can be locked using mode in the prior art. The setting of locking device can increase the tightness after combining between display device and thermal imaging system, keep the combination of the two more firm Gu.
As a preferred mode, rotatable cooling fin 24 is equipped at thermal window 23.The both ends of cooling fin 24 can It is rotatably connected on 23 both ends of thermal window.Cooling fin 24 to thermal window 23 can be rotated to be open maximum, effectively radiated, together When can rotate cooling fin 24 to completely closing thermal window 23, when blowing and raining, the guarantor to fuselage interior element can be played Shield effect.

Claims (7)

1. a kind of new type auto identification thermal imaging system imaging device, which is characterized in that including handle component, thermal imaging system, display device, Handle component is connect with thermal imaging system by the first clamping structure, and thermal imaging system is connect with display device by the second clamping structure, heat As instrument includes camera lens, fuselage and tail piece, camera lens, tail piece are all made of sealing ring sealing means and are mounted on fuselage both ends, screw Junction is coated with silica gel sealing, and epoxy resin paint and wax, and the shell side of thermal imaging system fuselage are coated on the shell of fuselage On be additionally provided with thermal window, shield, shield and camera lens removable connection are installed outside camera lens.
2. the new type auto identification thermal imaging system imaging device of one kind according to claim 1, which is characterized in that the first clamping knot Structure includes the first buckle and the first card slot, and the first buckle cooperates with the first card slot.
3. the new type auto identification thermal imaging system imaging device of one kind according to claim 2, which is characterized in that the first clamping knot First buckle of structure is arranged at handle component, and the first card slot is arranged at thermal imaging system or the first card of the first clamping structure Button is arranged at thermal imaging system, and the first card slot is arranged at handle component.
4. the new type auto identification thermal imaging system imaging device of one kind according to claim 1, which is characterized in that the second clamping knot Structure includes the second buckle and the second card slot, and the second buckle cooperates with the second card slot.
5. the new type auto identification thermal imaging system imaging device of one kind according to claim 4, which is characterized in that the second clamping knot Second buckle of structure is arranged at thermal imaging system, and the second card slot is arranged at display device or the second buckle setting is filled in display Place is set, the second card slot is arranged at thermal imaging system.
6. the new type auto identification thermal imaging system imaging device of one kind according to claim 1, which is characterized in that the second clamping knot Structure includes the toggle being arranged at thermal imaging system, and toggle head is arc-shaped and is equipped with card slot, and torsion is provided between toggle and thermal imaging system Spring.
7. the new type auto identification thermal imaging system imaging device of one kind according to claim 1, which is characterized in that at thermal window Equipped with rotatable cooling fin.
CN201821597300.2U 2018-09-29 2018-09-29 A kind of new type auto identification thermal imaging system imaging device Active CN208849864U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821597300.2U CN208849864U (en) 2018-09-29 2018-09-29 A kind of new type auto identification thermal imaging system imaging device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821597300.2U CN208849864U (en) 2018-09-29 2018-09-29 A kind of new type auto identification thermal imaging system imaging device

Publications (1)

Publication Number Publication Date
CN208849864U true CN208849864U (en) 2019-05-10

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Family Applications (1)

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Country Link
CN (1) CN208849864U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113411480A (en) * 2021-06-22 2021-09-17 歌尔科技有限公司 Image pickup apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113411480A (en) * 2021-06-22 2021-09-17 歌尔科技有限公司 Image pickup apparatus

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