CN106275489A - A kind of airborne missile carry visualization device - Google Patents
A kind of airborne missile carry visualization device Download PDFInfo
- Publication number
- CN106275489A CN106275489A CN201610834136.1A CN201610834136A CN106275489A CN 106275489 A CN106275489 A CN 106275489A CN 201610834136 A CN201610834136 A CN 201610834136A CN 106275489 A CN106275489 A CN 106275489A
- Authority
- CN
- China
- Prior art keywords
- quick
- hanger
- image
- fixing device
- release
- 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.)
- Granted
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/32—Ground or aircraft-carrier-deck installations for handling freight
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
Abstract
A kind of visualization device for airborne missile carry, including minisize pick-up head, location laser lamp, quick-release fixing device, image procossing transport module, power module, electric power connection line and image-receptive display device.Minisize pick-up head, location laser lamp, image image procossing transport module, power module are embedded in quick-release fixing device.Quick-release fixing device is arranged on guided missile hanger, and image-receptive display device is arranged on bomb truck operating board.Quick-release fixing device uses the inserted-link type abutting joint mode containing fixing hoodle, and bottom is agreed with body surface, and is provided with quick-release button, for docking fixing unblock.Minisize pick-up head provides the hanger at visual angle vertically upward and the position relationship image of hanging point, laser lamp instruction hanger level of relative position on hanger.Device uses wireless video transmission technology by carry image transmitting to display device, and bomb truck operator carries out visualizing the operation of guided missile carry accordingly.
Description
Technical field
The present invention relates to guided missile docking technique field, more particularly, it relates to a kind of be applicable to airborne missile carry can
Depending on gasifying device.
Background technology
The work of airborne missile carry is the important content of fighter plane combat readiness, and its carry speed directly affects fighting capacity
Formation speed.The work of airborne missile carry is through jacking apparatus (generally bomb truck) lifting guided missile, by body top
Two hanger docking enter at the hanging point of aircraft hanger, and are snapped in by hanger in the bayonet socket within hanging point, but due to guided missile one
As missile wing is installed, jacking apparatus operator are blocked by body and missile wing, are hardly visible the relative position of hanger and hanging point
Relation, needs commanding to utilize gesture and password commander operator to carry out missile position adjustment, until by two hangers simultaneously
Docking enters hanging point, such as Fig. 1.Owing to mating operation requires precision accurately, and two hangers need to be directed at entrance correspondence simultaneously and hang
Point, " password adjustment " operational approach of existing employing often leads to adjust overlong time, and even the failure of docking carry, needs to put down
Guided missile docks again, has had a strong impact on work efficiency.It addition, built-in type will be the major way of airborne missile carry, its hanging point
Hidden inside magazine, commanding is also difficult to the relative position relation observing hanger with hanging point, and existing extension bullet pattern will no longer
It is suitable for.
Use visualization technique to can effectively solve the problem that the problem of operator's visual perception weak effect, the most once it has been proposed that
Image collecting device is set in guided missile side, but hanger 2 is due to by missile wing serious shielding, when particularly body is close to hanger,
Still it is difficult in outside gather image, follow-up adds a sonde-type photographic head 2, be deep into the internal hanger 2 that gathers of missile wing
Docking scheme picture, such as Fig. 2.Although this method can obtain extension and play image, promote and hang bullet intuitive, but preliminary preparation is adjusted
The angle of whole probe 2 is relatively complicated, needs adjustment personnel and image viewing personnel repeatedly to confirm best angle, and it is equal to obtain image
For oblique viewing angle, accuracy is not enough.Therefore guided missile carry visualization device pair accurately more convenient, more directly perceived is designed
Promote carry work efficiency particularly important.
Summary of the invention
The technical problem existed for prior art, the present invention provides a kind of quick, image easy to loading and unloading the most accurately
Airborne missile carry visualization device.
For solving above-mentioned technical problem, miniature image acquisition transmission equipment is installed on hanger (1), passes through by this device
WIFI Radio Transmission Technology is by Image Real-time Transmission to reception display device, such as Fig. 3.This device is mainly by with lower part group
Become: minisize pick-up head (2), location laser lamp (3), quick-release fixing device (4), image procossing transport module (5), power module
(6), electric power connection line (7) and image-receptive display device (8).Wherein, minisize pick-up head (2), location laser lamp (3), image
Image procossing transport module (5), power module (6) are embedded in quick-release fixing device (4).
Quick-release fixing device (4) uses left and right two parts docking pluggable mode to be fixed on hanger (1), plug fixing and
Location uses hoodle lock mode, and device bottom surface uses the curved surface agreed with body surface.Quick-release fixing device (4) outside is provided with
Quick-release button, realizes the unblock of inserted link locking by pressing hoodle.
Minisize pick-up head (2) and location laser lamp (3) are arranged on the left-half upper surface of quick-release fixing device (4), and
Vertically upward, minisize pick-up head (2) use wide-angle lens, location laser lamp (3) light vertically upward with hanger (1) left surface phase
Cut.
Image procossing transport module (5) is embedded in quick-release fixing device (4) left-half, is used for processing minisize pick-up head
(2) image that gathers also is sent out by WIFI wireless radio frequency modules.
Power module (6) is embedded in quick-release fixing device (4) right half part, by electric power connection line (7) to miniature video camera
Head (2) and image procossing transport module (5) are powered.
Signal receiving processing module is integrated by image-receptive display device (8) with display module, is arranged on extension bullet
On car operating board.
It is an advantage of the current invention that:
(1) image aspects is reasonable, accurate positioning.Visual image uses vertical visual angle upwards, and utilizes location laser lamp to exist
Accurately indicate the vertical position of hanger on hanger, thus clearly demonstrate the relative position relation of two hangers and its hanging point, just
Make adjustment in time in operator；
(2) easy installation and removal.Have only to during installation be inserted in hanger, then by left-right parts the quick-release fixing device opened
Insert docking, and be close to missile airframe surface, can be fixed, finally image-receptive display device is positioned over bomb truck behaviour
Making platform, turning on the power button can start working, and step is simple.During dismounting, one hand simultaneously is only needed to press quick-release fixing device
The quick-release button of left-half both sides, extracts right half part simultaneously, the most complete.
Accompanying drawing explanation
Fig. 1 is that bullet schematic diagram hung by airborne missile；
Fig. 2 is that bullet visualization scheme schematic diagram hung by conventional airborne missile；
Fig. 3 is the composition schematic diagram of the present invention；
Fig. 4 is the structural representation of quick-release fixing device；
Fig. 5 is the profile of quick-release fixing device butted part；
Fig. 6 is the appearance schematic diagram of quick-release button and return spring.
Detailed description of the invention
The present invention is further detailed explanation with detailed description of the invention below in conjunction with the accompanying drawings.
Fig. 4 is the structural representation of quick-release fixing device.Quick-release fixing device (4) is formed by by left and right two parts, uses
Inserted link plug-in assembles, and right half part, equipped with two inserted links (401), corresponding to two jacks (402) of left-half, inserted link sets
There is hoodle (403), the location after inserted link (401) inserts and locking；The outside of right half part is provided with power knob (404)；
The both sides of left-half are provided with quick-release button (405), the unblock locked for hoodle (403), and surface is provided with minisize pick-up head (2)
Installing hole (406) and location laser lamp (3) installing hole (407)；Device bottom surface (408) employing and body surface are agreed with mutually
Columnar surface.
Fig. 5 is the profile of quick-release fixing device (4) left-right parts plug docking, and inserted link hoodle (403) lower end is provided with bullet
Spring (409), is provided with hoodle lock hole (410) in jack；Quick-release button (405) is positioned at hoodle lock hole (410) top, and quick-release is pressed
Button (405) afterbody inserts in hoodle lock hole (410), and quick-release button lower end is provided with return spring (411)；Quick-release button installing hole
(412) slightly larger than return spring (411) diameter, return spring (411) diameter is slightly larger than hoodle lock hole (410)；Quick-release button
The installation inner chamber (413) that diameter is bigger it is provided with between installing hole (412) and hoodle lock hole (410).
Fig. 6 is the appearance schematic diagram of quick-release button (407) and return spring (411), and quick-release button (407) head is dome
Shape, middle part is cylinder, and middle and lower part is round platform, and afterbody is cylinder；Linear diameter and return spring (411) diameter phase in round platform
Deng, spacing for return spring (411), midline is provided with the flexure strip (414) of multiple circumferential arrangement, quick-release button (405)
After inserting in installing hole (412), flexure strip (414) flicks, and withstands installation inner chamber (413) outside, for quick-release button (405)
The most spacing.
Minisize pick-up head (2) is respectively positioned on longitudinally asymmetric of quick-release fixing device (4) with the central shaft positioning laser lamp (3)
In, vertically upward, minisize pick-up head (2) is positioned at outside, location laser lamp (3), uses wide-angle lens, it is possible to clearly obtain hanger
And the real time imaging of the airborne hanger in top (1), location laser lamp (3) is arranged on below hanger (1) left side, laser beam vertically to
Upper tangent with hanger (1) side, its luminous point on hanger i.e. orients the vertical projection on hanger of hanger (1) left surface,
So that it is determined that go out the relative position relation of hanger (1) and hanging point.
Image procossing transport module (5) is carried out AD by video decoding chip, dsp chip, main control chip, video transmission chip
Conversion, compression coding, focus on, signal modulation and sending function.
Power module (6) is embedded in quick-release fixing device (4) right half part, by electric power connection line (7) to miniature video camera
Head (2) and image procossing transport module (5) are powered.
Image-receptive display device (8) is arranged on bomb truck operating board, including WIFI signal receiving processing module with aobvious
Show that module, signal receiving processing module include that video reception chip, main control chip realize signal reception, demodulation, DA conversion
Function.Display module uses 17 high brightness indicators.Image-receptive display device (8) lower section is provided with power knob.
Installation steps are as follows: the quick-release fixing device (4) opened be inserted on hanger (1), make bottom surface (408) be close to body
Two inserted links (403) on right side are docked along body surface and insert corresponding jack (402) so that hoodle (403) enters hoodle by surface
In lock hole (411), quick-release fixing device (4) can block hanger, then image-receptive display device (8) is positioned over extension bullet
Car operating platform, installation.
Demounting procedure is as follows: operator's left hand presses two of quick-release fixing device (4) left-half both sides soon simultaneously
Unloading button (405), then the right hand extracts quick-release fixing device (4) right half part, can pull down quick-release fixing device (4).
Use step: after guided missile is adjusted to below hanger by bomb truck operator, quick-release fixing device (4) and image are connect
Receive display device (8), by above-mentioned installation method, fastening is installed, then both power knobs are all opened, start system, system
Automatically carry out signal connection, image display would indicate that double width video image, it is possible to former and later two hangers is clearly seen
With the relative position relation of hanging point, bomb truck operator carries out missile position adjustment accordingly, until the laser spots of two width images is all
It is in the position to the front, centre of hanging point, it is possible on Chui Zhi, lift guided missile, when hanger has just enter into hanging point, presses quick-release fixing device
(4) power knob (404) on, closes closed system, and unloads quick-release fixing device (4), then bomb truck by above-mentioned method for dismounting
Operator continues to lift guided missile on vertical, completes the carry of guided missile.
Particular embodiments described above, has been carried out the purpose of the present invention, technical scheme and beneficial effect the most in detail
Describe in detail bright, be it should be understood that the specific embodiment that the foregoing is only the present invention, be not limited to the present invention, all
Within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, should be included in the guarantor of the present invention
Within the scope of protecting.
Claims (5)
1. the visualization device for airborne missile carry, it is characterised in that: include minisize pick-up head (2), location laser
Lamp (3), quick-release fixing device (4), image procossing transport module (5), power module (6), electric power connection line (7) and image-receptive
Display device (8)；Minisize pick-up head (2), location laser lamp (3), image image procossing transport module (5), power module (7) are all
It is embedded in quick-release fixing device；Quick-release fixing device (4) is arranged on guided missile hanger (1), and image-receptive display device (8) is pacified
It is contained on bomb truck operating board；Minisize pick-up head (2) provides hanger (1) and the hanging point position graph of a relation picture at visual angle vertically upward,
The level of relative position of location laser lamp (3) luminous point instruction hanger (1) on hanger；Use wireless video transmission technology by real
Time image transmitting in display device (8), bomb truck operator carries out visualization accordingly and hangs spring operation and make.
A kind of visualization device for airborne missile carry the most according to claim 1, it is characterised in that: described is fast
Unload fixing device (4) to be made up of left and right two parts, use double inserted link (401) plug-in to assemble, the location of inserted link (401) and locking
Using cylinder lock with balls fixed pattern, the unblock of inserted link uses quick-release push button, quick-release button (405) middle part to use truncated conical shape design, profit
Spacing in installing hole with return spring (411) and flexure strip (414).
A kind of visualization device for airborne missile carry the most according to claim 1, it is characterised in that: described is micro-
Type photographic head (2) with location laser lamp (3) central shaft be respectively positioned in longitudinally asymmetric of quick-release fixing device (4), vertically to
On；Minisize pick-up head (2) is positioned at outside, location laser lamp (3), uses wide-angle lens, it is possible to clear acquisition hanger and top are airborne
The real time imaging of hanger；Location laser lamp (3) is arranged on the left of hanger lower section, laser beam vertically upward with hanger side phase
Cut.
A kind of visualization device for airborne missile carry the most according to claim 1, it is characterised in that: described figure
As receiving and displaying device (8) includes WIFI signal receiving processing module and display module, display module uses 17 high brightness to show
Show device；It is provided with power knob below image-receptive display device.
A kind of visualization device for airborne missile carry the most according to claim 1, it is characterised in that: described electricity
Source module (6) is embedded in quick-release fixing device right half part, is passed minisize pick-up head and image procossing by electric power connection line (7)
Defeated module is powered.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610834136.1A CN106275489B (en) | 2016-09-20 | 2016-09-20 | A kind of airborne missile carry visualization device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610834136.1A CN106275489B (en) | 2016-09-20 | 2016-09-20 | A kind of airborne missile carry visualization device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106275489A true CN106275489A (en) | 2017-01-04 |
| CN106275489B CN106275489B (en) | 2018-04-27 |
Family
ID=57711971
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610834136.1A Expired - Fee Related CN106275489B (en) | 2016-09-20 | 2016-09-20 | A kind of airborne missile carry visualization device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106275489B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2018127071A (en) * | 2017-02-08 | 2018-08-16 | ルーチェサーチ株式会社 | Unmanned flight vehicle |
| CN110228599A (en) * | 2019-07-09 | 2019-09-13 | 成都立航科技股份有限公司 | A kind of bomb truck is hung automatically plays detection device and method |
| CN110228600A (en) * | 2019-07-09 | 2019-09-13 | 成都立航科技股份有限公司 | A kind of automatic hanging device of bomb truck and method |
| CN110606221A (en) * | 2019-09-19 | 2019-12-24 | 成都立航科技股份有限公司 | Automatic bullet hanging method for bullet hanging vehicle |
-
2016
- 2016-09-20 CN CN201610834136.1A patent/CN106275489B/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2018127071A (en) * | 2017-02-08 | 2018-08-16 | ルーチェサーチ株式会社 | Unmanned flight vehicle |
| CN110228599A (en) * | 2019-07-09 | 2019-09-13 | 成都立航科技股份有限公司 | A kind of bomb truck is hung automatically plays detection device and method |
| CN110228600A (en) * | 2019-07-09 | 2019-09-13 | 成都立航科技股份有限公司 | A kind of automatic hanging device of bomb truck and method |
| CN110228600B (en) * | 2019-07-09 | 2024-02-20 | 成都立航科技股份有限公司 | Automatic bullet hanging device and method for bullet hanging vehicle |
| CN110606221A (en) * | 2019-09-19 | 2019-12-24 | 成都立航科技股份有限公司 | Automatic bullet hanging method for bullet hanging vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106275489B (en) | 2018-04-27 |
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Granted publication date: 20180427 Termination date: 20200920 |
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| CF01 | Termination of patent right due to non-payment of annual fee |