CN103818554B - A kind of helicopter smog ejecting device mounting bracket - Google Patents
A kind of helicopter smog ejecting device mounting bracket Download PDFInfo
- Publication number
- CN103818554B CN103818554B CN201210464343.4A CN201210464343A CN103818554B CN 103818554 B CN103818554 B CN 103818554B CN 201210464343 A CN201210464343 A CN 201210464343A CN 103818554 B CN103818554 B CN 103818554B
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- Prior art keywords
- bolt
- attachment angle
- ejecting device
- block piece
- mounting bracket
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Abstract
The invention belongs to helicopter structure part technical field, particularly relate to a kind of smog ejecting device mounting bracket.This mounting bracket includes attachment angle (1), crossbeam (2), longeron (3), block piece (4), stay bolt (5) and plain bolt (6) composition, wherein, smog ejecting device (7) is connected on longeron (3) by bolt (5), longeron (3) is connected on two crossbeams (2) by bolt (6), crossbeam (2) and attachment angle (1) are connected by bolt (6), and each part all uses rigidity Design；Attachment angle (1) is connected by clamping hoop type with hanger and is connected, attachment angle (1) stretches two flange along weapon carrier profile and is stuck on the beam of weapon carrier, the restriction that hanger seesaws is completed by block piece (4), block piece (4) is connected with attachment angle (1) bolt (6), block piece (4) also has two flange, is stuck on the reinforcement before weapon carrier beam.
Description
Technical field
The invention belongs to helicopter structure part technical field, particularly relate to a kind of smog ejecting device mounting bracket.
Background technology
Helicopter installs smog ejecting device for carrying out demonstration flight in all kinds of air shows or large-scale celebration activity.Smog ejecting device has different installation sites and installation form in different type of machines, and this is designed as installing smog ejecting device additional on certain type tactical reconnaissance helicopter the most at home.
Summary of the invention
The technical problem to be solved in the present invention:
It is an object of the invention to design a kind of smog ejecting device mounting bracket being suitable for Z9 series helicopter, provide for the performance in exhibition or activity of later Z9 series machine and support.
Technical scheme:
A kind of helicopter smog ejecting device mounting bracket, forms including attachment angle 1, crossbeam 2, longeron 3, block piece 4, stay bolt 5 and plain bolt 6, is all connected by bolt.
Smog ejecting device 7 is connected on longeron 3 by bolt 5, and longeron 3 is connected on two crossbeams 2 by bolt 6, and crossbeam 2 and attachment angle 1 are connected by bolt 6, and each part all uses rigidity Design.
Attachment angle 1 is connected by clamping hoop type with hanger and is connected, attachment angle 1 stretches two flange along weapon carrier profile and is stuck on the beam of weapon carrier, the restriction that hanger seesaws is completed by block piece 4, block piece 4 is connected with attachment angle 1 bolt 6, block piece 4 also has two flange, is stuck on the reinforcement before weapon carrier beam.
All junctions are respectively arranged with rubber blanket.
Beneficial effects of the present invention:
By the design of smog ejecting device mounting bracket, smog ejecting device installation on helicopter is reliable and stable, meets performance mission requirements.
Accompanying drawing explanation
Fig. 1 is the top view of the present invention, wherein, 1 be attachment angle, 2 be crossbeam, 3 be longeron, 4 be block piece, 5 be stay bolt, 6 for plain bolt.
Fig. 2 is the rearview of the present invention, and wherein, 7 is smog ejecting device.
Detailed description of the invention
A kind of helicopter smog ejecting device mounting bracket, forms including attachment angle 1, crossbeam 2, longeron 3, block piece 4, stay bolt 5 and plain bolt 6, for ensureing detachability, is all connected by bolt.
Smog ejecting device 7 is connected on longeron 3 by three stay bolts 5, and longeron 3 is connected on two crossbeams 2 by four plain bolts 6, and crossbeam 2 and attachment angle 1 are connected by 12 plain bolts 6, and for preventing deformation minimum, each part all uses rigidity Design.As shown in Figure 1.
Do not allow due to weapon carrier to carry out secondary operations, therefore attachment angle 1 is connected by clamping hoop type with hanger and is connected, attachment angle 1 stretches two flange along weapon carrier profile and is stuck on the beam of weapon carrier, so can limit smog ejecting device hanger and move up and down, as shown in Figure 2.And the restriction that hanger seesaws is completed by block piece 4, block piece 4 is connected with attachment angle 1 plain bolt 6, and block piece 4 also has two flange, is stuck on the reinforcement before weapon carrier beam, and thus the constraint of smog ejecting device 7 is fully completed.
For increasing shake-proof ability, easy to assembly and prevent from weapon carrier causes abrasion, all junctions are respectively arranged with rubber blanket.
According to the feature of certain type tactical reconnaissance helicopter, plan colored smog ejecting device and be arranged on below missile launcher, then hanger is suspended on the weapon camber beam of helicopter left and right.Being introduced in driving cabin by firing control line on guided missile hanger, and be connected with the percussion lock being arranged on driver's cycle bar, driver controls the work of aerosol bomb by percussion lock.Percussion lock is arranged on bench board, has two percussion locks, draws cigarette process by what next percussion lock can complete a 50s, and once lift-off can complete twice to draw cigarette.Draw cigarette process once, it is impossible to enough manually release, after need to completing to draw cigarette, could again implement to draw cigarette next time.
Claims (2)
1. a helicopter smog ejecting device mounting bracket, is characterized in that, this mounting bracket include attachment angle (1), crossbeam (2),
Longeron (3), block piece (4), stay bolt (5) and plain bolt (6) composition, wherein,
Smog ejecting device (7) is connected on longeron (3) by stay bolt (5), and longeron (3) is connected to by plain bolt (6)
On two crossbeams (2), crossbeam (2) and attachment angle (1) are connected by plain bolt (6), and each part all uses rigidity
Design；
Attachment angle (1) is connected by clamping hoop type with hanger and is connected, and attachment angle (1) stretches two along weapon carrier profile and turns over
Checkpost is on the beam of weapon carrier, and the restriction that hanger seesaws is completed by block piece (4), block piece (4) and attachment angle (1)
Connecting with plain bolt (6), block piece (4) also has two flange, is stuck on the reinforcement before weapon carrier beam.
2. a kind of helicopter smog ejecting device mounting bracket as claimed in claim 1, is characterized in that, all of junction is respectively arranged with
Rubber blanket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210464343.4A CN103818554B (en) | 2012-11-16 | 2012-11-16 | A kind of helicopter smog ejecting device mounting bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210464343.4A CN103818554B (en) | 2012-11-16 | 2012-11-16 | A kind of helicopter smog ejecting device mounting bracket |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103818554A CN103818554A (en) | 2014-05-28 |
| CN103818554B true CN103818554B (en) | 2016-08-24 |
Family
ID=50753914
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210464343.4A Expired - Fee Related CN103818554B (en) | 2012-11-16 | 2012-11-16 | A kind of helicopter smog ejecting device mounting bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103818554B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104384920B (en) * | 2014-08-26 | 2018-10-02 | 中国直升机设计研究所 | A kind of light helicopter structural member assembly devices and methods therefor |
| CN104456023A (en) * | 2014-12-04 | 2015-03-25 | 石家庄飞机工业有限责任公司 | Mounting bracket for display in small general-purpose aircraft cabin |
| CN105217039B (en) * | 2015-10-08 | 2017-10-27 | 谢飞 | A kind of smog ejecting device |
| CN110294127A (en) * | 2019-08-02 | 2019-10-01 | 北京通用航空江西直升机有限公司 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4138078A (en) * | 1977-05-31 | 1979-02-06 | Textron Inc. | Helicopter cargo hook apparatus |
| US5045649A (en) * | 1989-10-03 | 1991-09-03 | Bell Helicopter Textron Inc. | Self-adjusting slide assembly for weight on gear switch |
| US6176167B1 (en) * | 1999-03-31 | 2001-01-23 | Paul H. Sanderson | Helicopter underside armament mounting apparatus and associated methods |
| CN2863643Y (en) * | 2005-12-07 | 2007-01-31 | 上海子锦电子科技有限公司 | Smog ejecting device |
| CN101758922A (en) * | 2008-12-23 | 2010-06-30 | 江西洪都航空工业集团有限责任公司 | Retractable captive flight support for external hanging equipment |
| CN102431647A (en) * | 2010-09-29 | 2012-05-02 | 成都飞机工业（集团）有限责任公司 | Aircraft smoke plume system |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20120052480A (en) * | 2010-11-16 | 2012-05-24 | 대한민국(농촌진흥청장) | Seeding apparatus for unmaned helicopter |
| FR2970944B1 (en) * | 2011-01-27 | 2013-02-08 | Eurocopter France | REMOVABLE FIXING DEVICE WITH A MEANS FOR HANGING AN EXTERNAL LOAD AND A MEANS FOR FASTENING SAID MEANS OF ATTACHING TO AN AIRCRAFT, AIRCRAFT AND ASSOCIATED METHOD |
-
2012
- 2012-11-16 CN CN201210464343.4A patent/CN103818554B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4138078A (en) * | 1977-05-31 | 1979-02-06 | Textron Inc. | Helicopter cargo hook apparatus |
| US5045649A (en) * | 1989-10-03 | 1991-09-03 | Bell Helicopter Textron Inc. | Self-adjusting slide assembly for weight on gear switch |
| US6176167B1 (en) * | 1999-03-31 | 2001-01-23 | Paul H. Sanderson | Helicopter underside armament mounting apparatus and associated methods |
| CN2863643Y (en) * | 2005-12-07 | 2007-01-31 | 上海子锦电子科技有限公司 | Smog ejecting device |
| CN101758922A (en) * | 2008-12-23 | 2010-06-30 | 江西洪都航空工业集团有限责任公司 | Retractable captive flight support for external hanging equipment |
| CN102431647A (en) * | 2010-09-29 | 2012-05-02 | 成都飞机工业（集团）有限责任公司 | Aircraft smoke plume system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103818554A (en) | 2014-05-28 |
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Legal Events
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160824 Termination date: 20171116 |