CN103569361B - A kind of bomb electromagnetism carry device - Google Patents
A kind of bomb electromagnetism carry device Download PDFInfo
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- CN103569361B CN103569361B CN201310568200.2A CN201310568200A CN103569361B CN 103569361 B CN103569361 B CN 103569361B CN 201310568200 A CN201310568200 A CN 201310568200A CN 103569361 B CN103569361 B CN 103569361B
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- electromagnet
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Abstract
A kind of bomb electromagnetism carry device.The invention belongs to bomb carry technology, relate to the improvement to aircraft bomb hanging structure.It is characterized in that: on bomb (3), have two groups of embedded bomb electromagnet, often organize bomb electromagnet to be made up of the first bomb electromagnet (7), the second bomb electromagnet (8) and the 3rd bomb electromagnet (9), the inside face of half built-in type extension internal weapon bays there are two groups to hang and play electromagnet, first group of axial location hanging bullet electromagnet is corresponding with first group of bomb electromagnet, and second group of axial location hanging bullet electromagnet is corresponding with second group of bomb electromagnet.Invention increases carry stress point, simplify carry and throw in structure, alleviating the weight of hanging structure, reduce the requirement to hanging structure material, reduce space in shared machine, reduce the impact on the pneumatic of aircraft and handling stability energy, decrease Radar Cross Section.
Description
Technical field
The invention belongs to bomb carry technology, relate to the improvement to aircraft bomb hanging structure.
Background technology
Current one half built-in type bomb hanging structure is see Fig. 1 and Fig. 2, and it is by wing 1 rack unit 2 of carrier aircraft and formed by the bomb 3 of carry.The lower surface of wing 1 has half built-in type hang internal weapon bays, bomb 3 is hung in internal weapon bays at half built-in type by carry device carry.The upper end of rack unit 2 is connected with the load-carrying member of wing 1 for overall, and the lower end of rack unit 2 is connected with the hanging point of bomb 3.Its shortcoming is: carry stress point is single, and hanging structure design is complicated, weight is large, and hanging structure material requirements is high.Special launching and throwing mechanism must be had simultaneously, launch with throwing mechanism system height large, occupy space in larger machine, can certain influence be had to the pneumatic of aircraft and handling stability, and add Radar Cross Section.
Summary of the invention
The object of the invention is: propose a kind of bomb electromagnetism carry device, to increase carry stress point, simplify carry and throw in structure, alleviate the weight of hanging structure, reduce the requirement to hanging structure material, space in machine shared by reduction, reduces the impact on the pneumatic of aircraft and handling stability energy, reduces Radar Cross Section.
Technical scheme of the present invention is: a kind of bomb electromagnetism carry device, comprise carrier aircraft wing 1 and by the bomb 3 of carry, the lower surface of wing 1 has half built-in type hang internal weapon bays, bomb 3 is hung in internal weapon bays by carry device carry at half built-in type; It is characterized in that: on bomb 3, have two groups of embedded bomb electromagnet, often organize bomb electromagnet to be made up of the first bomb electromagnet 7, second bomb electromagnet 8 and the 3rd bomb electromagnet 9, two groups of bomb electromagnet are arranged before and after the axis of bomb 3, and the first bomb electromagnet 7 is uniform along the semicircumference of bomb 3 to the 3rd bomb electromagnet 9; The inside face of half built-in type extension internal weapon bays has two groups of extensions to play electromagnet, and first group of axial location hanging bullet electromagnet is corresponding with first group of bomb electromagnet, and the axial location of second group of extension bullet electromagnet is corresponding with second group of bomb electromagnet; Often organize extension bullet electromagnet to be made up of the first extension bullet electromagnet 4, second extension bullet electromagnet 5 and the 3rd extension bullet electromagnet 6, the first extension bullet electromagnet 4 is corresponding to the position of the 3rd bomb electromagnet 9 with the first bomb electromagnet 7 respectively to the position of the 3rd extension bullet electromagnet 6; When bomb 3 is in carry state, the first extension plays electromagnet 4 and is all energized to the 3rd bomb electromagnet 9 to the 3rd extension bullet electromagnet 6 and the first bomb electromagnet 7, and the magnetic that bomb electromagnet plays electromagnet with extension is attracting; When bomb 3 is in commit condition, the second extension plays electromagnet 5 and the second bomb electromagnet 8 is energized and magnetic is repelled each other, other extension bullet electromagnet and the equal power-off of bomb electromagnet.
Advantage of the present invention is: propose a kind of bomb electromagnetism carry device, add carry stress point, simplify carry and throw in structure, alleviate the weight of hanging structure, reduce the requirement to hanging structure material, reduce space in shared machine, reduce the impact on the pneumatic of aircraft and handling stability energy, decrease Radar Cross Section.
Accompanying drawing explanation
Fig. 1 is current one half built-in type bomb hanging structure schematic diagram.
Fig. 2 is the P-P cutaway view of Fig. 1.
Fig. 3 is structural representation of the present invention.
Fig. 4 is the K-K cutaway view of Fig. 3.
Detailed description of the invention
Below the present invention is described in further detail.See Fig. 3,4, a kind of bomb electromagnetism carry device, comprise carrier aircraft wing 1 and by the bomb 3 of carry, the lower surface of wing 1 has half built-in type hang internal weapon bays, bomb 3 is hung in internal weapon bays by carry device carry at half built-in type; It is characterized in that: on bomb 3, have two groups of embedded bomb electromagnet, often organize bomb electromagnet to be made up of the first bomb electromagnet 7, second bomb electromagnet 8 and the 3rd bomb electromagnet 9, two groups of bomb electromagnet are arranged before and after the axis of bomb 3, and the first bomb electromagnet 7 is uniform along the semicircumference of bomb 3 to the 3rd bomb electromagnet 9; The inside face of half built-in type extension internal weapon bays has two groups of extensions to play electromagnet, and first group of axial location hanging bullet electromagnet is corresponding with first group of bomb electromagnet, and the axial location of second group of extension bullet electromagnet is corresponding with second group of bomb electromagnet; Often organize extension bullet electromagnet to be made up of the first extension bullet electromagnet 4, second extension bullet electromagnet 5 and the 3rd extension bullet electromagnet 6, the first extension bullet electromagnet 4 is corresponding to the position of the 3rd bomb electromagnet 9 with the first bomb electromagnet 7 respectively to the position of the 3rd extension bullet electromagnet 6; When bomb 3 is in carry state, the first extension plays electromagnet 4 and is all energized to the 3rd bomb electromagnet 9 to the 3rd extension bullet electromagnet 6 and the first bomb electromagnet 7, and the magnetic that bomb electromagnet plays electromagnet with extension is attracting; When bomb 3 is in commit condition, the second extension plays electromagnet 5 and the second bomb electromagnet 8 is energized and magnetic is repelled each other, other extension bullet electromagnet and the equal power-off of bomb electromagnet.
Principle of work of the present invention is: inserted by bomb in half buried extension internal weapon bays, aviation plug is had to be connected between bomb with aircraft, give all bomb electromagnet by aviation plug by aircraft and hang and play electromagnet and power, bomb electromagnet with hang that to play the magnetic of electromagnet attracting, carry on the machine realizing bomb.Aircraft carries bomb and arrives position of dropping a bomb, and the second extension plays electromagnet 5 and the second bomb electromagnet 8 is energized and magnetic is repelled each other, other extension bullet electromagnet and the equal power-off of bomb electromagnet, bomb is ejected half buried extension internal weapon bays, realizes launching and throwing in function.
One embodiment of the present of invention, compared with the existing bomb hanger, weight saving more than 60%, in shared machine, space decreases more than 80%.
Claims (1)
1. a bomb electromagnetism carry device, comprise carrier aircraft wing (1) and by the bomb of carry (3), the lower surface of wing (1) has half built-in type hang internal weapon bays, bomb (3) is hung in internal weapon bays by carry device carry at half built-in type; It is characterized in that: on bomb (3), have two groups of embedded bomb electromagnet, often organize bomb electromagnet to be made up of the first bomb electromagnet (7), the second bomb electromagnet (8) and the 3rd bomb electromagnet (9), two groups of bomb electromagnet are arranged before and after the axis of bomb (3), and the first bomb electromagnet (7) is uniform along the semicircumference of bomb (3) to the 3rd bomb electromagnet (9); The inside face of half built-in type extension internal weapon bays has two groups of extensions to play electromagnet, and first group of axial location hanging bullet electromagnet is corresponding with first group of bomb electromagnet, and the axial location of second group of extension bullet electromagnet is corresponding with second group of bomb electromagnet; Often organize extension bullet electromagnet to be made up of the first extension bullet electromagnet (4), the second extension bullet electromagnet (5) and the 3rd extension bullet electromagnet (6), the first extension bullet electromagnet (4) is corresponding to the position of the 3rd bomb electromagnet (9) with the first bomb electromagnet (7) respectively to the position of the 3rd extension bullet electromagnet (6); When bomb (3) is in carry state, first extension plays electromagnet (4) and is all energized to the 3rd bomb electromagnet (9) to the 3rd extension bullet electromagnet (6) and the first bomb electromagnet (7), and the magnetic that bomb electromagnet plays electromagnet with extension is attracting; When bomb (3) is in commit condition, the second extension plays electromagnet (5) and the second bomb electromagnet (8) is energized and magnetic is repelled each other, other extension bullet electromagnet and the equal power-off of bomb electromagnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310568200.2A CN103569361B (en) | 2013-11-13 | 2013-11-13 | A kind of bomb electromagnetism carry device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310568200.2A CN103569361B (en) | 2013-11-13 | 2013-11-13 | A kind of bomb electromagnetism carry device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103569361A CN103569361A (en) | 2014-02-12 |
| CN103569361B true CN103569361B (en) | 2015-10-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310568200.2A Active CN103569361B (en) | 2013-11-13 | 2013-11-13 | A kind of bomb electromagnetism carry device |
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| Country | Link |
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| CN (1) | CN103569361B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102014004838A1 (en) * | 2014-04-02 | 2015-10-08 | Airbus Defence and Space GmbH | Effector with discardable Tarnschale |
| CN104309806A (en) * | 2014-10-08 | 2015-01-28 | 中国航空工业集团公司西安飞机设计研究所 | Cruise missile carrier vehicle |
| CN106184760A (en) * | 2016-07-29 | 2016-12-07 | 江西洪都航空工业集团有限责任公司 | Airborne missile hanger |
| CN107399437B (en) * | 2017-07-13 | 2020-04-07 | 江西洪都航空工业集团有限责任公司 | Locking transition structure for hanging elastic hook |
| CN108974362A (en) * | 2018-07-20 | 2018-12-11 | 中国空空导弹研究院 | To ammunition locking arrangement and aircraft |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0144265A1 (en) * | 1983-11-29 | 1985-06-12 | R. ALKAN & Cie. | Aircraft external load suspension and release unit with triple escapement rockers |
| FR2791950A1 (en) * | 1999-04-08 | 2000-10-13 | Rafaut & Cie | Bomb carrier mounting for aircraft has beam fitting onto mounting on aircraft with couplings to substitute for existing mounting rings |
| EP1369349A1 (en) * | 2002-06-07 | 2003-12-10 | MBDA France | Weapon provided with a missile and which is mounted on a stealth aircraft, and a weapon system comprising a stealth aircraft and such a weapon |
| CN202642100U (en) * | 2012-05-15 | 2013-01-02 | 湖北三江航天险峰电子信息有限公司 | Guided missile hanging frame swinging-prevention device suitable for various missile diameters |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8418965B2 (en) * | 2009-06-01 | 2013-04-16 | Israel Aerospace Industries Ltd. | Mounting set, system and method |
-
2013
- 2013-11-13 CN CN201310568200.2A patent/CN103569361B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0144265A1 (en) * | 1983-11-29 | 1985-06-12 | R. ALKAN & Cie. | Aircraft external load suspension and release unit with triple escapement rockers |
| FR2791950A1 (en) * | 1999-04-08 | 2000-10-13 | Rafaut & Cie | Bomb carrier mounting for aircraft has beam fitting onto mounting on aircraft with couplings to substitute for existing mounting rings |
| EP1369349A1 (en) * | 2002-06-07 | 2003-12-10 | MBDA France | Weapon provided with a missile and which is mounted on a stealth aircraft, and a weapon system comprising a stealth aircraft and such a weapon |
| CN202642100U (en) * | 2012-05-15 | 2013-01-02 | 湖北三江航天险峰电子信息有限公司 | Guided missile hanging frame swinging-prevention device suitable for various missile diameters |
Non-Patent Citations (1)
| Title |
|---|
| 图解武器挂架;司古;《航空知识》;20060831(第8期);第60-63页 * |
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| Publication number | Publication date |
|---|---|
| CN103569361A (en) | 2014-02-12 |
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