CN106184760A - Airborne missile hanger - Google Patents
Airborne missile hanger Download PDFInfo
- Publication number
- CN106184760A CN106184760A CN201610607540.5A CN201610607540A CN106184760A CN 106184760 A CN106184760 A CN 106184760A CN 201610607540 A CN201610607540 A CN 201610607540A CN 106184760 A CN106184760 A CN 106184760A
- Authority
- CN
- China
- Prior art keywords
- right baffle
- plate
- hanger
- missile
- guided missile
- 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.)
- Pending
Links
- 230000006698 induction Effects 0.000 claims abstract description 32
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Particle Accelerators (AREA)
Abstract
A kind of airborne missile hanger, is connected to main drop in beam both sides including main drop in beam, right baffle-plate, right baffle plate, right baffle-plate and right baffle plate, is respectively disposed with magnetic induction coil or induction machine in right baffle-plate, right baffle plate and main drop in beam.The mechanical force carry guided missile that conventional hanger uses abandoned by this airborne missile hanger, uses the carry that electromagnetic force is guided missile to provide and supports.Under airborne missile hanger power on condition, magnetic induction coil or induction machine produce magnetic attraction, and magnetic induction coil or induction machine on main drop in beam, right baffle-plate, right baffle plate adsorb guided missile firmly.Left baffle can effectively prevent guided missile from vacillating now to the left, now to the right.This airborne missile hanger can meet the carry requirement of dissimilar guided missile, it is possible to the efficiency of fast lifting carry guided missile.
Description
Technical field
The invention belongs to airborne missile hanger field.
Background technology
Existing airborne missile hanger all uses machinery hanger, and guided missile is transported to the docking structure of aircraft hanger through bomb truck,
Hang guided missile by mechanical hook, and lock.During MISSILE LAUNCHING, the hanger of aircraft is by mechanical movement and unlocks, and is sent out by guided missile
It is shot out.Being mechanically connected owing to guided missile hanger uses, position and the interface of hanger are fixed, it is impossible to meet the guided missile of all models,
The versatility of hanger is poor.Being mechanically connected simultaneously because use, the carry of guided missile needs the cooperation of several ground staff, carry mistake
Cheng Sudu is slow, and efficiency is low.
Summary of the invention
The purpose of the present invention: propose a kind of airborne missile hanger, the shortcoming overcoming tradition guided missile hanger poor universality, meet
The carry of dissimilar guided missile and mission need, simplify carry flow process.
Technical scheme:
This airborne missile hanger, is connected to main extension including main drop in beam, right baffle-plate, right baffle plate, right baffle-plate and right baffle plate
Beam both sides, are respectively disposed with magnetic induction coil or induction machine in right baffle-plate, right baffle plate and main drop in beam.
Further, right baffle-plate, right baffle plate flexibly connect with main drop in beam respectively.
Advantages of the present invention:
The mechanical force carry guided missile that conventional hanger uses abandoned by this airborne missile hanger, and using electromagnetic force is the extension of guided missile
Carry to provide and support.It is respectively disposed with magnetic induction coil or induction machine, at hanger energising bar in left baffle and main drop in beam
Under part, hanger is opened carry pattern, magnetic induction coil or induction machine and is produced magnetic attraction, on main drop in beam, right baffle-plate, right baffle plate
Magnetic induction coil or induction machine guided missile is adsorbed firmly.Left baffle can effectively prevent guided missile from vacillating now to the left, now to the right.
This airborne missile hanger can meet the carry requirement of dissimilar guided missile, it is possible to the efficiency of fast lifting carry guided missile.Left and right
Baffle plate flexibly connects respectively with main drop in beam, it is possible to according to the difference of the diameter of hung guided missile, suitably regulate, and meets multiple type
Number general carry.
Accompanying drawing illustrates:
Fig. 1 is airborne missile hanger outline drawing of the present invention
Fig. 2 is airborne missile hanger organization chart of the present invention
Fig. 3 is airborne missile hanger carry guided missile side view of the present invention
Fig. 4 is airborne missile hanger carry guided missile top view of the present invention
1-the first magnetic induction coil or the first induction machine, 2-the second magnetic induction coil or the second induction machine, 3-
3rd magnetic induction coil or the 3rd induction machine
Detailed description of the invention:
Below in conjunction with the accompanying drawings the present invention is described in further detail.
Embodiment 1
This airborne missile hanger includes, main drop in beam, right baffle-plate, right baffle plate, and right baffle-plate and right baffle plate are connected to main extension
Beam both sides, are respectively disposed with first magnetic induction coil the 1, second magnetic induction coil 2 and in right baffle-plate, right baffle plate and main drop in beam
Three magnetic induction coils 3.
Embodiment 2
This airborne missile hanger includes, main drop in beam, right baffle-plate, right baffle plate, and right baffle-plate and right baffle plate are connected to main extension
Beam both sides, are respectively disposed with the first induction machine the 1, first induction machine 2 and the 3rd sense in right baffle-plate, right baffle plate and main drop in beam
Answer motor 3.
Right baffle-plate, right baffle plate flexibly connect with main drop in beam.
During carry, when guided missile is lifted to corresponding height and position by guided missile carry car, at airborne missile hanger energising bar
Under part, hanger is opened carry pattern, magnetic induction coil or induction machine and is produced magnetic attraction, and guided missile is at the electromagnetic attraction of hanger
Effect under, magnetic induction coil or induction machine on main drop in beam, right baffle-plate, right baffle plate adsorb guided missile firmly.Lead
The automatic carry of bullet puts in place, can complete the carry of guided missile conveniently and efficiently.Under hanger outage condition, magnetic induction coil or sense
The magnetic attraction answering motor disappears, and can carry out guided missile input.
Claims (2)
1. an airborne missile hanger, it is characterised in that include that main drop in beam, right baffle-plate, right baffle plate, right baffle-plate and right baffle plate are respectively
It is connected to main drop in beam both sides, in right baffle-plate, right baffle plate and main drop in beam, is respectively disposed with magnetic induction coil or induction machine.
2. airborne missile hanger as claimed in claim 1, it is characterised in that right baffle-plate, right baffle plate are flexible with main drop in beam respectively
Connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610607540.5A CN106184760A (en) | 2016-07-29 | 2016-07-29 | Airborne missile hanger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610607540.5A CN106184760A (en) | 2016-07-29 | 2016-07-29 | Airborne missile hanger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184760A true CN106184760A (en) | 2016-12-07 |
Family
ID=57495780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610607540.5A Pending CN106184760A (en) | 2016-07-29 | 2016-07-29 | Airborne missile hanger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184760A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112719804A (en) * | 2020-12-18 | 2021-04-30 | 湖北三江航天江北机械工程有限公司 | Processing method of air-to-air missile hanging combination for training |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3667342A (en) * | 1970-04-08 | 1972-06-06 | Us Navy | Magnetic weapon link transducer |
| US5831200A (en) * | 1996-01-09 | 1998-11-03 | Bodenseewerk Geratetechnik Gmbh | Hanger for a missile in a launcher |
| 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 |
| US20040262456A1 (en) * | 2003-03-06 | 2004-12-30 | Moates James Benjamin | Hanger assembly for aircraft |
| KR100779749B1 (en) * | 2007-04-30 | 2007-11-26 | 주식회사 태화에레마 | Multi type adjustable magnetic lifter for steel coil |
| CN103569361A (en) * | 2013-11-13 | 2014-02-12 | 中国航空工业集团公司西安飞机设计研究所 | Bomb electromagnetic mounting device |
| CN204461247U (en) * | 2014-12-09 | 2015-07-08 | 江西洪都航空工业集团有限责任公司 | The anti-sway stop device of a kind of hanger |
| CN105173086A (en) * | 2015-08-16 | 2015-12-23 | 邢永安 | Hanging rack used for modified missiles of fixed wing model airplane |
-
2016
- 2016-07-29 CN CN201610607540.5A patent/CN106184760A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3667342A (en) * | 1970-04-08 | 1972-06-06 | Us Navy | Magnetic weapon link transducer |
| US5831200A (en) * | 1996-01-09 | 1998-11-03 | Bodenseewerk Geratetechnik Gmbh | Hanger for a missile in a launcher |
| 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 |
| US20040262456A1 (en) * | 2003-03-06 | 2004-12-30 | Moates James Benjamin | Hanger assembly for aircraft |
| KR100779749B1 (en) * | 2007-04-30 | 2007-11-26 | 주식회사 태화에레마 | Multi type adjustable magnetic lifter for steel coil |
| CN103569361A (en) * | 2013-11-13 | 2014-02-12 | 中国航空工业集团公司西安飞机设计研究所 | Bomb electromagnetic mounting device |
| CN204461247U (en) * | 2014-12-09 | 2015-07-08 | 江西洪都航空工业集团有限责任公司 | The anti-sway stop device of a kind of hanger |
| CN105173086A (en) * | 2015-08-16 | 2015-12-23 | 邢永安 | Hanging rack used for modified missiles of fixed wing model airplane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112719804A (en) * | 2020-12-18 | 2021-04-30 | 湖北三江航天江北机械工程有限公司 | Processing method of air-to-air missile hanging combination for training |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |