CN104266552B - Sky puts pull-type gun infrared laser target - Google Patents
Sky puts pull-type gun infrared laser target Download PDFInfo
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- CN104266552B CN104266552B CN201410385175.9A CN201410385175A CN104266552B CN 104266552 B CN104266552 B CN 104266552B CN 201410385175 A CN201410385175 A CN 201410385175A CN 104266552 B CN104266552 B CN 104266552B
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Abstract
The invention provides a kind of linkage for throwing in and discharge software target, comprising: pull bar and movable hook, one end of pull bar is rotationally connected with movable one end hooked, and the movable other end hooked has upper projection and lower projection; Before input software target, upper projection pins the bonnet in the target cabin holding software target; When throwing in software target, pull bar moves forward, and drive activity hooks and moves down, upper projection release bonnet, and software target is released, and when activity hook moves down, lower projection catches on the front end of software target, and software target launches flight; When discharging target, pull bar moves backward, and movable hook moves up, and unclamps the software target front end of having caught on, and software target departs from lower projection.The present invention both can release software target when putting target and stopping again, can cast software target again when reclaiming, and was conducive to reclaiming hardware target, and met the demand to the source of infrared radiation.
Description
Technical field
The present invention relates to aviation target technical field, particularly a kind of sky puts pull-type gun infrared laser target.
Background technology
At present, to tow target with having for the target of gun air firing and sky puts target two kinds.
Wherein, towing target in ground is by the target of tug plane from rope start runway, and tow target owing to rising to aerial range from ground rope start, towing aircraft fuel consumption is large, and airborne period is short this kind of Target tool and the long-time friction loss of high velocity air also very large; Target is rolling start on runway, and vibration causes greatly can not assembling as precision equipments such as infra-red radiations, limits some target signature devices and installs use additional as equipment such as infra-red radiation, laser diffusions.Towing target due to ground is a kind of target with the visual attack of optical sighting device, and not there is the target signature such as infra-red radiation, laser diffusion, the aircraft that therefore can not be used for equipping photo-electric fire control system is practiced shooting, and this fire control system is based on the Novel fire Ore-controlling Role in infrared survey target bearing, Laser Measuring target range principle.In addition, towing target by tug plane from rope start runway to air target spatial domain for practicing shooting in ground, and then tows back to airport and cast, and easily occurs that target comes off problem, jeopardizes ground staff and property safety in whole process.
Sky puts target and target is first placed in the target cabin of aircraft, taking aerial target area to just releases for practicing shooting, such oil plant is economized, target consumption is few, and can equip various precision equipment, as infra-red radiation, the infrared targets simulator such as laser diffusion, adapt to all kinds of new-type fire control system demand of new machine, and the precision instruments such as the missdistance indicator for recording shot orbit can be filled, complete detection assessment pilot shooting parameter.In addition, sky puts target in the process of round target area, and target is placed in target cabin, can not self falling, and therefore its security is fine.
On the other hand, sky is put target and also be there is certain technical problem, namely sky puts target owing to being equipped with missdistance indicator, direct collection trajectory parameter, instead of the large target of 1: 1 is scored with bullet direct hit target, therefore target body is very little, brings certain difficulty to so again the aerial visualization target of pilot.For this reason, the target of a software is devised to increase the visual range of pilot to target specially at hardware target rear, this software target just thinks that target releasing is just released after putting in place, for visual, and first to reclaim this software target when reclaiming target, and current software target can not come off, be connected with hardware target always, recovery target is made troubles.
Sky of the prior art puts target except there is the technical problem of In-Flight Deployment and input, also need to solve the technical problem of the source of infrared radiation under aloft high velocity air, because the so-called source of infrared radiation is exactly thermal source, aloft in high velocity air, air velocity is large, per secondly reach 167m/s, any point thermal source is all dispelled, and conventional heating system is all inadvisable.
Summary of the invention
(1) technical problem that will solve
The problem that the present invention primarily solves be how to make software target aloft put target complete after Automatic-expanding, and can self falling when reclaiming, the problem that the present invention will solve further is how to realize the source of infrared radiation of target aloft under high velocity air.
(2) technical scheme
To achieve these goals, the invention provides a kind of linkage for throwing in and discharge software target, comprising: pull bar and movable hook, wherein, one end that one end of described pull bar and described activity hook is rotationally connected, and the other end that described activity hooks has upper projection and lower projection; Before the described software target of input, described upper projection pins the bonnet in the target cabin holding described software target; When throwing in described software target, described pull bar moves forward, and drives described activity to hook and moves down, described upper projection discharges described bonnet, and described software target is released, when described activity hook moves down, described lower projection catches on the front end of described software target, and described software target launches flight; When discharging described target, described pull bar moves backward, and described activity hooks and moves up, and unclamps the software target front end of having caught on, and described software target departs from described lower projection.
Preferably, be rotationally connected described in as being connected by bearing pin.
Present invention also offers a kind of transmission mechanism for throwing in and discharge software target, comprise: one or more any one linkage aforementioned and pull bar, wherein, the other end of pull bar described in described linkage is connected with described pull bar, by the forward and backward movement of the described pull bar described pull bar of forward and backward mobile drive.
Preferably, also comprise: motor, for driving the forward and backward movement of described pull bar.
Preferably, also comprising: slip cap, being sheathed on described pull bar outside, for guiding described pull bar forward and backward movement.
Present invention also offers a kind of sky and put pull-type gun infrared laser target, comprise: any one transmission mechanism aforementioned, software target, hardware target, target cabin and bonnet, wherein, described target cabin is placed in described hardware target rear end, for holding described software target, described bonnet covers at rear portion, described target cabin.
Preferably, also comprise: as the turbojet of the source of infrared radiation, it is placed in described hardware target.
Preferably, described bonnet is semi-spherical rear cover, and described hemispherical is protruding outside towards described target cabin.
Preferably, described software target is made up of polyamide fibre sieve.
Preferably, also comprise: for recording the missdistance indicator of shooting grade, Digital Transmission radio station and battery, it is placed in described hardware target.
(3) beneficial effect
The present invention has significant advantage and beneficial effect compared to existing technology: 1, both can releasing software target again when putting target and stopping, can cast software target again when reclaiming, be conducive to reclaiming hardware target; 2, the demand to the source of infrared radiation is met.
Accompanying drawing explanation
With reference to the accompanying drawings and further describe the present invention in conjunction with example.Wherein:
Fig. 1 shows the example arrangement schematic diagram of transmission mechanism for throwing in and discharge software target of the present invention;
Fig. 2 shows the example arrangement schematic diagram of linkage for throwing in and depart from software target of the present invention;
Label declaration: projection, 9-bearing pin under the movable hook of 1-linkage, 2-pull bar, 3-motor, 4-slip cap, 5-pull bar, 6-, the upper projection of 7-, 8-.
Detailed description of the invention
Below in conjunction with drawings and Examples, the specific embodiment of the present invention is described in further detail.Following examples for illustration of the present invention, but are not used for limiting the scope of the invention.
The invention provides a kind of sky and put pull-type gun infrared laser target, comprising: hardware target, target cabin, software target, bonnet and transmission mechanism.
Wherein, described hardware target can be the cylindrical rectification body of a tool.
Wherein, described target cabin is placed in described hardware target rear end, for holding described software target.
Wherein, described software target is for increasing visual range and establishing, can being made up of polyamide fibre sieve, aloft can in 3km visual finding.
Wherein, described bonnet covers at rear portion, described target cabin, and it can be hemispherical, and described hemispherical is protruding outside towards described target cabin.
As shown in Figure 1, described transmission mechanism comprises: linkage 1 and pull bar 2.
Wherein, described linkage 1 is for throwing in and release software target, and it can be one, also can be multiple, and as shown in Figure 2, each linkage 1 comprises: pull bar 5 and movable hook 6.
Wherein, one end of described pull bar 5 is connected with described pull bar 2, by the forward and backward movement of the described pull bar 2 described pull bar 5 of forward and backward mobile drive.
Wherein, one end that the other end of described pull bar 5 and described activity hook 6 is rotationally connected, and such as, can be connected by bearing pin 9.
The other end of described activity hook 6 has upper projection 7 and lower projection 8.
Before the described software target of input, described upper projection 7 pins the bonnet in the target cabin holding described software target.
When throwing in described software target, described pull bar 5 moves forward, drive described activity to hook 6 to move down, described upper projection 7 discharges described bonnet, described software target is released, when described activity hook 6 moves down, described lower projection 8 catches on the front end of described software target, and described software target launches flight.
When discharging described target, described pull bar 5 moves backward, and described activity hooks 6 and moves up, and unclamps the software target front end of having caught on, and described software target departs from described lower projection 8.
As shown in Figure 1, described transmission mechanism can also comprise motor 3, for driving the forward and backward movement of described pull bar 2.
As shown in Figure 1, described transmission mechanism can also comprise slip cap 4, is sheathed on described pull bar 5 outside, for guiding described pull bar 5 forward and backward movement.
According to the present invention, described target can also comprise: as a small sized turbine jet engine of the source of infrared radiation, it is placed in described hardware target, can produce infra-red radiation.
According to the present invention, described target can also comprise: for recording the missdistance indicator of shooting grade, Digital Transmission radio station and battery, it is placed in described hardware target.
Introduce the use of putting pull-type gun infrared laser target according to sky provided by the invention below:
Before flight, energising checks whether every technical parameter of target conforms with the regulations; Fuel is filled up to small sized turbine jet engine; Software target to be rolled well in the target cabin being installed to target rear end and to lock bonnet; Cart rope and target are connected; Target is installed on the saddle in tug plane target cabin, now software target be placed on hardware target rear end target cabin in and live with a semi-spherical rear cover and pinned by the upper projection 7 of the activity hook 6 of linkage.
After arriving target area awing, pilot presses and transfers target button, and target is thrown off from the latch hook the saddle of target cabin; And the winch under airflow function in target cabin starts, and releases cart rope; Under cart rope traction, target flies to the back lower place; When cart rope is put into 500m place, target stops, and at this moment the pull bar 5 of transmission mechanism moves forward, movable hook 6 moves down, and bonnet unblanks to fly, and software target is released, when activity hook 6 moves down, its lower projection 8 has caught on again the front end of software target, and therefore software target flies with hardware target; Small sized turbine jet engine is aloft lighted a fire simultaneously, sends infra-red radiation, enters for target state.During shooting, shot orbit is constantly recorded by missdistance indicator, assesses for after aircraft landing.
After task completes, pilot presses and receives target button, and in target cabin, winch rotates and reclaims cart rope; At this moment the pull bar 5 of transmission mechanism moves backward, and movable hook 6 moves up, and opens the software target front end of originally catching on, and software target breaks off relations and flies; Then the towed wire saws of target reclaims, until on the saddle of target cabin; Aircraft is given an encore landing afterwards, from missdistance indicator, read shooting grade.Again prepare aerial mission next time.
In addition, in case of emergency, urgent throwing target button can be pressed by pilot, release target.
It should be noted that, " forward ", " backward ", " upwards " mentioned in the present invention, " downwards " are relative concept, namely " forward " represent relative both direction with " backward ", " upwards " represents relative both direction with " downwards ", and not represents absolute direction.
Description of the invention provides in order to example with for the purpose of describing, and is not exhaustively or limit the invention to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Selecting and describing embodiment is in order to principle of the present invention and practical application are better described, and enables those of ordinary skill in the art understand the present invention thus design the various embodiments with various amendment being suitable for special-purpose.
Claims (10)
1. for throwing in and discharge a linkage for software target, it is characterized in that, comprising: pull bar and movable hook, wherein, one end that one end of described pull bar and described activity hook is rotationally connected, and the other end that described activity hooks has upper projection and lower projection; Before the described software target of input, described upper projection pins the bonnet in the target cabin holding described software target; When throwing in described software target, described pull bar moves forward, and drives described activity to hook and moves down, described upper projection discharges described bonnet, and described software target is released, when described activity hook moves down, described lower projection catches on the front end of described software target, and described software target launches flight; When discharging described target, described pull bar moves backward, and described activity hooks and moves up, and unclamps the software target front end of having caught on, and described software target departs from described lower projection.
2. linkage as claimed in claim 1, is characterized in that: described in be rotationally connected as being connected by bearing pin.
3. one kind for throwing in and discharge the transmission mechanism of software target, it is characterized in that, comprise: one or more linkage as claimed in claim 1 or 2 and pull bar, wherein, the other end of pull bar described in described linkage is connected with described pull bar, by the forward and backward movement of the described pull bar described pull bar of forward and backward mobile drive.
4. transmission mechanism as claimed in claim 3, is characterized in that, also comprise: motor, for driving the forward and backward movement of described pull bar.
5. the transmission mechanism as described in claim 3 or 4, is characterized in that, also comprises: slip cap, is sheathed on described pull bar outside, for guiding described pull bar forward and backward movement.
6. a sky puts pull-type gun infrared laser target, it is characterized in that, comprise: transmission mechanism, software target, hardware target, target cabin and bonnet any one of claim 3 ~ 5, wherein, described target cabin is placed in described hardware target rear end, for holding described software target, described bonnet covers at rear portion, described target cabin.
7. sky as claimed in claim 6 puts pull-type gun infrared laser target, and it is characterized in that, also comprise: as the turbojet of the source of infrared radiation, it is placed in described hardware target.
8. sky as claimed in claims 6 or 7 puts pull-type gun infrared laser target, and it is characterized in that: described bonnet is semi-spherical rear cover, described semi-spherical rear cover is protruding outside towards described target cabin.
9. sky as claimed in claim 8 puts pull-type gun infrared laser target, it is characterized in that: described software target is made up of polyamide fibre sieve.
10. sky as claimed in claim 9 puts pull-type gun infrared laser target, it is characterized in that, also comprises: for recording the missdistance indicator of shooting grade, Digital Transmission radio station and battery, it is placed in described hardware target.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410385175.9A CN104266552B (en) | 2014-08-07 | 2014-08-07 | Sky puts pull-type gun infrared laser target |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410385175.9A CN104266552B (en) | 2014-08-07 | 2014-08-07 | Sky puts pull-type gun infrared laser target |
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| Publication Number | Publication Date |
|---|---|
| CN104266552A CN104266552A (en) | 2015-01-07 |
| CN104266552B true CN104266552B (en) | 2016-01-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410385175.9A Active CN104266552B (en) | 2014-08-07 | 2014-08-07 | Sky puts pull-type gun infrared laser target |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106767181A (en) * | 2017-01-13 | 2017-05-31 | 河北环航科技股份有限公司 | A kind of plug-in target nacelle of aviation |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020107844A1 (en) * | 2018-11-26 | 2020-06-04 | 北京金朋达航空科技有限公司 | Infrared enhancer with controllable radiation power |
| CN112285677B (en) * | 2020-10-29 | 2024-02-02 | 中国航空工业集团公司洛阳电光设备研究所 | Testing device for external field shrinkage ratio laser cooperative target |
| CN112859929B (en) * | 2021-03-04 | 2024-08-16 | 闽南科技学院 | Remote control system for air-to-air missile trawl |
Citations (5)
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|---|---|---|---|---|
| WO1990005890A1 (en) * | 1988-11-21 | 1990-05-31 | Air Target Sweden Ab | A device for the release of aerial towed targets |
| JP2000346600A (en) * | 1999-06-07 | 2000-12-15 | Mitsubishi Heavy Ind Ltd | Pod towed for optical measuring |
| DE10021999A1 (en) * | 2000-05-05 | 2001-11-08 | Comet Gmbh Pyrotechnik Appbau | Infrared-emitting target for aircraft; has towing line fixed to target, forming loop passing though lug of aircraft and releasably fixed at other end to target, to be released by heat of target charge |
| CN2535760Y (en) * | 2002-03-22 | 2003-02-12 | 常铁铮 | High-speed air target device |
| JP4712507B2 (en) * | 2005-10-07 | 2011-06-29 | ダイセル化学工業株式会社 | Connection and disconnection device |
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2014
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Patent Citations (5)
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|---|---|---|---|---|
| WO1990005890A1 (en) * | 1988-11-21 | 1990-05-31 | Air Target Sweden Ab | A device for the release of aerial towed targets |
| JP2000346600A (en) * | 1999-06-07 | 2000-12-15 | Mitsubishi Heavy Ind Ltd | Pod towed for optical measuring |
| DE10021999A1 (en) * | 2000-05-05 | 2001-11-08 | Comet Gmbh Pyrotechnik Appbau | Infrared-emitting target for aircraft; has towing line fixed to target, forming loop passing though lug of aircraft and releasably fixed at other end to target, to be released by heat of target charge |
| CN2535760Y (en) * | 2002-03-22 | 2003-02-12 | 常铁铮 | High-speed air target device |
| JP4712507B2 (en) * | 2005-10-07 | 2011-06-29 | ダイセル化学工業株式会社 | Connection and disconnection device |
Non-Patent Citations (1)
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| "一种新型可展开空靶的初步设计与动力学分析";关富玲 等;《工程设计学报》;20131028;第20卷(第5期);第398-403页 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106767181A (en) * | 2017-01-13 | 2017-05-31 | 河北环航科技股份有限公司 | A kind of plug-in target nacelle of aviation |
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| Publication number | Publication date |
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| CN104266552A (en) | 2015-01-07 |
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