CN104976923A - Rack type buoy target used for airplane gunnery training - Google Patents
Rack type buoy target used for airplane gunnery training Download PDFInfo
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- CN104976923A CN104976923A CN201510321245.9A CN201510321245A CN104976923A CN 104976923 A CN104976923 A CN 104976923A CN 201510321245 A CN201510321245 A CN 201510321245A CN 104976923 A CN104976923 A CN 104976923A
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- way pipe
- buoy
- target
- frame
- stent
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Abstract
The invention discloses a rack type buoy target used for airplane gunnery training, which comprises a buoy rack, 3m buoys arranged on the buoy rack and a plurality of anchors used for fixing the buoy rack, wherein the buoy rack comprises m first three-way pipes, m four-way pipes and m second three-way pipes; the two ends of each first three-way pipe are connected with one end of each of the other two first three-way pipes; all the first three-way pipes are connected to form a first annular rack; the two ends of each four-way pipe are connected with one end of each of the other two four-way pipes; all the four-way pipes are connected to form a second annular rack; the two ends of each second three-way pipe are connected with one end of each of the other two second three-way pipes; and all the second three-way pipes are connected to form a third annular rack. The rack type buoy target has the characteristics that the rack type buoy target is light in mass, convenient to move, simple and convenient to maintain, and low in cost, and can be assembled rapidly.
Description
Technical field
The present invention relates to airplane training technical field, especially relate to that a kind of quality is light, conveniently moving, assembling speed fast, keep in repair easy, that cost the is low stent-type buoy target for aircraft gunnery training for aircraft gunnery training.
Background technology
The target that aircraft water training is conventional is steel frame construction, needs to assemble on the coast, on-shore maintenance, and assembly quality is large, and mobile inconvenience, the time that assembly operation spends is long, and cost is high.
Therefore, at present in the urgent need to the target of the fast airplane training of a kind of conveniently moving, assembling speed.
Chinese patent mandate publication number: CN204043522U, authorizes publication date on December 24th, 2014, discloses a kind of paper screen image target, comprises frame and at least two and overlap target sheet systems; Wherein: described frame comprises upper bracket, lower carriage and two side stands to surround between the target sheet field of fire, described upper bracket and two side stands are equipped with light barrier to be in the light to the periphery between the described target sheet field of fire, are provided with the roll shaft vertical with two side stands in described lower carriage; Every suit target sheet system comprises driver element and target sheet, described driver element comprise the axis parallel of two axial lines and described roll shaft target sheet roller, with described target sheet roller drive motors one to one, described target sheet roller can be installed on described upper bracket rotatably around its axial line, and each drive motors target sheet roller corresponding with it is in transmission connection; The one ends wound of described target sheet is on a target sheet roller, and the other end is wound on another root target sheet roller after walking around described roll shaft; In target sheet in each described target sheet system, between the target sheet in two cover target sheet systems of arbitrary neighborhood part overlapping, to make target sheet cover between the target sheet field of fire of described frame.The weak point of this invention is, function singleness cannot be used for aircraft gunnery training.
Summary of the invention
Goal of the invention of the present invention is in order to the deficiency that time is long, cost is high overcoming large, the mobile inconvenience of target assembly quality of the prior art, assembly operation spends, and provides that a kind of quality is light, conveniently moving, assembling speed are fast, keep in repair easy, that cost the is low stent-type buoy target for aircraft gunnery training for aircraft gunnery training.
To achieve these goals, the present invention is by the following technical solutions:
For a stent-type buoy target for aircraft gunnery training, comprise buoy frame, be located at 3m buoy on buoy frame and several anchors for fixed buoy frame; Described buoy frame comprises m the first three-way pipe, m four-way pipe and m the second three-way pipe; Each first three-way pipe two ends are connected with two other the first three-way pipe one end respectively, and all first three-way pipes connect and compose the first toroidal frame; Each four-way pipe two ends are connected with two other four-way pipe one end respectively, and all four-way pipes connect and compose the second toroidal frame; Each second three-way pipe two ends are connected with two other the second three-way pipe one end respectively, and all second three-way pipes connect and compose the 3rd toroidal frame; The diameter of the first toroidal frame, the second toroidal frame, the 3rd toroidal frame reduces successively;
The other two ends of each four-way pipe connect with the other end of the first corresponding three-way pipe and the other end of the 4th three-way pipe respectively, form the m bar radiant tube of buoy frame; Each buoy is connected respectively with in the middle part of each first three-way pipe, the second three-way pipe and four-way pipe; From the buoy that the first three-way pipe connects, be located at the different coating of color respectively with the buoy that the second three-way pipe is connected and the buoy upper surface that is connected with four-way pipe.
The target of stent-type buoy target for providing aircraft to shoot for aircraft gunnery training of the present invention, each anchor is used for buoy frame to be fixed in the waters in precalculated position; Buoy frame is made up of the first toroidal frame, the second toroidal frame, the 3rd toroidal frame and m article of radiant tube, thus makes buoy put up an overall structure for being suspended on the water surface; Each buoy upper surface that first three-way pipe, the second three-way pipe are connected with four-way pipe is located at the different coating of color respectively, make the coating color of the buoy on the first toroidal frame, the second toroidal frame, the 3rd toroidal frame different, thus make pilot can tell the position residing for target center in the air from height, vector aircraft gunnery training.
The present invention can assemble in waterside, then moves to location, certain waters; If training place, away from bank, also can shipping be located to anchor point in-site installation.
Therefore, the present invention has that quality is light, conveniently moving, assembling speed fast, keep in repair easy, that cost is low feature.
As preferably, described first three-way pipe comprise connect with corresponding four-way pipe first be responsible for and be positioned at the first supervisor both sides and two the first side pipes be connected with the first adjacent three-way pipe respectively, two the first side pipes and first be responsible between angle be acute angle.
As preferably, described second three-way pipe comprise connect with corresponding four-way pipe second be responsible for and be positioned at the second supervisor both sides and two the second side pipes be connected with the second adjacent three-way pipe respectively, two the second side pipes and second be responsible between angle be obtuse angle.
As preferably, described four-way pipe comprises straight tube and is located at oliquely downward tilt two inclined tubes of both sides in the middle part of straight tube, and two angles between inclined tube and straight tube are acute angle.
As preferably, described buoy top is cylindrical shape, and buoy bottom is the little cone shape in lower end; Buoy comprises bag and is filled in the high-density polystyrene foam in bag.
As preferably, the coating of the buoy upper surface be connected with the first three-way pipe is white, and the coating of the buoy upper surface is connected with the second three-way pipe is for red, and the coating of the buoy upper surface is connected with four-way pipe is yellow.
As preferably, described anchor is 3 to 8, and each anchor is connected with the first toroidal frame respectively.
As preferably, also comprise flight path indication body and n the anchor for fixing flight path indication body, flight path indication body comprises n direction spaced instruction buoyancy aid successively as indicated; Connected by rope between each instruction buoyancy aid, the instruction buoyancy aid near buoy frame is connected with the first toroidal frame by rope; Instruction buoyancy aid upper surface is provided with and the coating identical with the buoy upper surface color that the second three-way pipe connects; N anchor indicates buoyancy aid bottom to be connected with each respectively.
As preferably, described instruction buoyancy aid upper surface is triangular in shape, and instruction buoyancy aid comprises two indicating modules be connected; Each indicating module includes bag and is filled in the polystyrene foam in bag.
The bag that canvas or similar material are made has non-damageable feature, and polystyrene foam has the advantages that quality is light, cost is low.
As preferably, all connected by loose joint between the first adjacent three-way pipe, each four-way pipe is all connected by loose joint with between the first corresponding three-way pipe, the second three-way pipe, is all connected by loose joint between the second adjacent three-way pipe.
Therefore, the present invention has following beneficial effect: quality is light, conveniently moving, assembling speed are fast, it is easy to keep in repair, product cost is low, maintenance cost is low.
Accompanying drawing explanation
Fig. 1 is a kind of structural representation of the present invention;
Fig. 2 is a kind of structural representation of the first three-way pipe of the present invention;
Fig. 3 is a kind of structural representation of four-way pipe of the present invention;
Fig. 4 is a kind of structural representation of the second three-way pipe of the present invention;
Fig. 5 is a kind of structural representation of flight path indication body of the present invention;
Fig. 6 is a kind of structural representation of buoy of the present invention.
In figure: buoy frame 1, buoy 2, radiant tube 3, first three-way pipe 4, four-way pipe 5, second three-way pipe 6, first toroidal frame 7, second toroidal frame 8, the 3rd toroidal frame 9, first are responsible for the 10, first side pipe 11, second and are responsible for the 12, second side pipe 13, straight tube 14, inclined tube 15, flight path indication body 16, instruction buoyancy aid 17, rope 18.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention will be further described.
Embodiment is as shown in Figure 1 a kind of stent-type buoy target for aircraft gunnery training, comprises buoy frame 1, is located at 36 buoys 2 on buoy frame and 5 anchors for fixed buoy frame; Buoy frame comprises 12 the first three-way pipes, 4,12 four-way pipes 5 and 12 the second three-way pipes 6; Each first three-way pipe two ends are connected with two other the first three-way pipe one end respectively, and all first three-way pipes connect and compose the first toroidal frame 7; Each four-way pipe two ends are connected with two other four-way pipe one end respectively, and all four-way pipes connect and compose the second toroidal frame 8; Each second three-way pipe two ends are connected with two other the second three-way pipe one end respectively, and all second three-way pipes connect and compose the 3rd toroidal frame 9; The diameter of the first toroidal frame, the second toroidal frame, the 3rd toroidal frame reduces successively;
The other two ends of each four-way pipe connect with the other end of the first corresponding three-way pipe and the other end of the 4th three-way pipe respectively, form 12 radiant tubes 3 of buoy frame; Each buoy is connected respectively with in the middle part of each first three-way pipe, the second three-way pipe and four-way pipe; From the buoy that the first three-way pipe connects, be located at the different coating of color respectively with the buoy that the second three-way pipe is connected and the buoy upper surface that is connected with four-way pipe.
As shown in Figure 2, the first three-way pipe comprise connect with corresponding four-way pipe first be responsible for 10 and be positioned at the first supervisor both sides and two the first side pipes, 11, two the first side pipes and first of being connected with the first adjacent three-way pipe be respectively responsible between angle be acute angle.
As shown in Figure 4, the second three-way pipe comprise connect with corresponding four-way pipe second be responsible for 12 and be positioned at the second supervisor both sides and two the second side pipes, 13, two the second side pipes and second of being connected with the second adjacent three-way pipe be respectively responsible between angle be obtuse angle.
As shown in Figure 3, the angle of oliquely downward tilt two inclined tubes 15, two between inclined tube and straight tube that four-way pipe comprises straight tube 14 and is located at both sides in the middle part of straight tube is acute angle.
As shown in Figure 6, buoy top is cylindrical shape, and buoy bottom is the little cone shape in lower end; Buoy comprises bag and is filled in the high-density polystyrene foam in bag.
The coating of the buoy upper surface be connected with the first three-way pipe is white, and the coating of the buoy upper surface be connected with the second three-way pipe is for red, and the coating of the buoy upper surface be connected with four-way pipe is for yellow.Each anchor is connected with each float respectively by the first toroidal frame.
As shown in Figure 5, also comprise flight path indication body 16 and 3 anchors for fixing flight path indication body, flight path indication body comprises 3 direction spaced instruction buoyancy aids 17 successively as indicated; Connected by rope 18 between each instruction buoyancy aid, the instruction buoyancy aid near buoy frame is connected with the first toroidal frame by rope; Instruction buoyancy aid upper surface is provided with and the coating identical with the buoy upper surface color that the second three-way pipe connects; 3 anchors indicate buoyancy aid bottom to be connected with each respectively.
Instruction buoyancy aid upper surface is triangular in shape, and instruction buoyancy aid comprises two indicating modules be connected; Each indicating module includes bag and is filled in the polystyrene foam in bag.
All connected by loose joint between the first adjacent three-way pipe, each four-way pipe is all connected by loose joint with between the first corresponding three-way pipe, the second three-way pipe, is all connected by loose joint between the second adjacent three-way pipe.
The course of work of the present invention is as follows:
Each first three-way pipe, the second three-way pipe are connected respectively with four-way pipe, form buoy frame; 36 buoys are connected respectively on buoy frame, with rope, 3 instruction buoyancy aids are linked in sequence successively, form flight path indication body; Utilize rope to be connected with buoy frame by flight path indication body, form buoy target of the present invention;
Then buoy target is dragged to predetermined waters, utilizes 5 anchors to be fixed by buoy target; Buoy target is suspended on the water surface, and flight path indication body guides aircraft according to guide direction near buoy target;
Aircraft is to floating target shooting, and when each buoy is less than 8 times by the number of times of bullet hits, buoy all can not be scrapped;
If certain buoy quilt attack is ruined, this buoy is removed, changes new buoy into.
Should be understood that the present embodiment is only not used in for illustration of the present invention to limit the scope of the invention.In addition should be understood that those skilled in the art can make various changes or modifications the present invention, and these equivalent form of values fall within the application's appended claims limited range equally after the content of having read the present invention's instruction.
Claims (10)
1. for a stent-type buoy target for aircraft gunnery training, it is characterized in that, comprise buoy frame (1), be located at 3m buoy (2) on buoy frame and several anchors for fixed buoy frame; Described buoy frame comprises m the first three-way pipe (4), m four-way pipe (5) and m the second three-way pipe (6); Each first three-way pipe two ends are connected with two other the first three-way pipe one end respectively, and all first three-way pipes connect and compose the first toroidal frame (7); Each four-way pipe two ends are connected with two other four-way pipe one end respectively, and all four-way pipes connect and compose the second toroidal frame (8); Each second three-way pipe two ends are connected with two other the second three-way pipe one end respectively, and all second three-way pipes connect and compose the 3rd toroidal frame (9); The diameter of the first toroidal frame, the second toroidal frame, the 3rd toroidal frame reduces successively;
The other two ends of each four-way pipe connect with the other end of the first corresponding three-way pipe and the other end of the 4th three-way pipe respectively, form the m bar radiant tube (3) of buoy frame; Each buoy is connected respectively with in the middle part of each first three-way pipe, the second three-way pipe and four-way pipe; From the buoy that the first three-way pipe connects, be located at the different coating of color respectively with the buoy that the second three-way pipe is connected and the buoy upper surface that is connected with four-way pipe.
2. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, described first three-way pipe comprise connect with corresponding four-way pipe first be responsible for (10) and be positioned at the first supervisor both sides and two the first side pipes (11) being connected with the first adjacent three-way pipe respectively, two the first side pipes and first be responsible between angle be acute angle.
3. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, described second three-way pipe comprise connect with corresponding four-way pipe second be responsible for (12) and be positioned at the second supervisor both sides and two the second side pipes (13) being connected with the second adjacent three-way pipe respectively, two the second side pipes and second be responsible between angle be obtuse angle.
4. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, described four-way pipe comprises straight tube (14) and is located at oliquely downward tilt two inclined tubes (15) of both sides in the middle part of straight tube, and two angles between inclined tube and straight tube are acute angle.
5. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, described buoy top is cylindrical shape, and buoy bottom is the little cone shape in lower end; Buoy comprises bag and is filled in the high-density polystyrene foam in bag.
6. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, the coating of the buoy upper surface be connected with the first three-way pipe is white, the coating of the buoy upper surface be connected with the second three-way pipe is for red, and the coating of the buoy upper surface be connected with four-way pipe is for yellow.
7. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, described anchor is 3 to 8, and each anchor is connected with the first toroidal frame respectively.
8. the stent-type buoy target for aircraft gunnery training according to claim 1, it is characterized in that, also comprise flight path indication body (16) and n the anchor for fixing flight path indication body, flight path indication body comprises n direction spaced instruction buoyancy aid (17) successively as indicated; Connected by rope (18) between each instruction buoyancy aid, the instruction buoyancy aid near buoy frame is connected with the first toroidal frame by rope; Instruction buoyancy aid upper surface is provided with and the coating identical with the buoy upper surface color that the second three-way pipe connects; N anchor indicates buoyancy aid bottom to be connected with each respectively.
9. the stent-type buoy target for aircraft gunnery training according to claim 8, is characterized in that, described instruction buoyancy aid upper surface is triangular in shape, and instruction buoyancy aid comprises two indicating modules be connected (19); Each indicating module includes bag and is filled in the polystyrene foam in bag.
10. the stent-type buoy target for aircraft gunnery training according to claim 1 or 2 or 3 or 4 or 5 or 6 or 7 or 8 or 9, it is characterized in that, all connected by loose joint between the first adjacent three-way pipe, each four-way pipe is all connected by loose joint with between the first corresponding three-way pipe, the second three-way pipe, is all connected by loose joint between the second adjacent three-way pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510321245.9A CN104976923B (en) | 2015-06-11 | 2015-06-11 | Stent-type buoy target for aircraft gunnery training |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510321245.9A CN104976923B (en) | 2015-06-11 | 2015-06-11 | Stent-type buoy target for aircraft gunnery training |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104976923A true CN104976923A (en) | 2015-10-14 |
| CN104976923B CN104976923B (en) | 2016-09-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510321245.9A Active CN104976923B (en) | 2015-06-11 | 2015-06-11 | Stent-type buoy target for aircraft gunnery training |
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| CN (1) | CN104976923B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105486176A (en) * | 2015-12-15 | 2016-04-13 | 孟钧 | Portable night live ammunition LED target device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4223412A1 (en) * | 1992-07-16 | 1994-01-20 | Deutsche Aerospace | Practice goal |
| US5435569A (en) * | 1993-06-30 | 1995-07-25 | Zilliox; Kent | Combined water pistol and scoring target |
| KR101290121B1 (en) * | 2011-12-29 | 2013-07-26 | 대덕위즈주식회사 | Divisible of target for tank marksmanship training |
| KR101466733B1 (en) * | 2012-01-10 | 2014-12-02 | 주식회사 비즈모델라인 | Target system of tank marksmanship training |
| CN204043522U (en) * | 2014-09-12 | 2014-12-24 | 北京信安通靶场装备技术有限公司 | Paper screen image target |
| CN204881347U (en) * | 2015-06-11 | 2015-12-16 | 富阳舒力科技有限公司 | A a posture buoy target for aircraft gunnery training |
-
2015
- 2015-06-11 CN CN201510321245.9A patent/CN104976923B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4223412A1 (en) * | 1992-07-16 | 1994-01-20 | Deutsche Aerospace | Practice goal |
| US5435569A (en) * | 1993-06-30 | 1995-07-25 | Zilliox; Kent | Combined water pistol and scoring target |
| KR101290121B1 (en) * | 2011-12-29 | 2013-07-26 | 대덕위즈주식회사 | Divisible of target for tank marksmanship training |
| KR101466733B1 (en) * | 2012-01-10 | 2014-12-02 | 주식회사 비즈모델라인 | Target system of tank marksmanship training |
| CN204043522U (en) * | 2014-09-12 | 2014-12-24 | 北京信安通靶场装备技术有限公司 | Paper screen image target |
| CN204881347U (en) * | 2015-06-11 | 2015-12-16 | 富阳舒力科技有限公司 | A a posture buoy target for aircraft gunnery training |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105486176A (en) * | 2015-12-15 | 2016-04-13 | 孟钧 | Portable night live ammunition LED target device |
| CN105486176B (en) * | 2015-12-15 | 2017-05-17 | 蚌埠天意汽车修理厂 | Portable night live ammunition LED target device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104976923B (en) | 2016-09-14 |
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Address after: Hangzhou City, Zhejiang province Fuyang District 311413 Fuchun street, No. 32-4 Co-patentee after: 94580 TROOP OF THE PLA Patentee after: Hangzhou Fuyang comfort Technology Co., Ltd. Address before: No. 1 Hangzhou Road, 311413 Zhejiang city of Fuyang Province Town Industrial Zone No. 8 Dayuan building second Co-patentee before: 94580 TROOP OF THE PLA Patentee before: FUYANG SHULI TECHNOLOGY CO., LTD. |
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Effective date of registration: 20180202 Address after: Hangzhou City, Zhejiang province Fuyang District 311413 Fuchun street, No. 32-4 Patentee after: Hangzhou Fuyang comfort Technology Co., Ltd. Address before: Hangzhou City, Zhejiang province Fuyang District 311413 Fuchun street, No. 32-4 Co-patentee before: 94580 TROOP OF THE PLA Patentee before: Hangzhou Fuyang comfort Technology Co., Ltd. |