CN103818554A - Helicopter smoke generator mounting support - Google Patents
Helicopter smoke generator mounting support Download PDFInfo
- Publication number
- CN103818554A CN103818554A CN201210464343.4A CN201210464343A CN103818554A CN 103818554 A CN103818554 A CN 103818554A CN 201210464343 A CN201210464343 A CN 201210464343A CN 103818554 A CN103818554 A CN 103818554A
- Authority
- CN
- China
- Prior art keywords
- hanger
- helicopter
- bolt
- attachment angle
- ejecting device
- 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.)
- Granted
Links
Images
Landscapes
- Catching Or Destruction (AREA)
- Toys (AREA)
Abstract
The invention belongs to the technical field of helicopter structural components, and particularly relates to a smoke generator mounting support comprising connecting angles (1), two transverse beams (2), a longitudinal beam (3), baffling members (4), long bolts (5) and ordinary bolts (6). A smoke generator (7) is connected to the longitudinal beam (3) through the long bolts (5), the longitudinal beam (3) is connected to the transverse beams (2) through the ordinary bolts (6), the transverse beams (2) and the connecting angles (1) are connected through the ordinary bolts (6), and each component is designed in a rigid manner; the connecting angles (1) are connected with a weapon hanger in a clamped manner and extend to form two flanges clamped on beams of the weapon hanger along the shape of the hanger, the hanger moves longitudinally and is limited through the baffling members (4), and the baffling members (4) are connected to the connecting angles (1) through the ordinary bolts (6), are provided with two flanges for each and are clamped in the reinforcing ribs in the front of the beams of the weapon hanger.
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 is installed 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 on certain type tactical reconnaissance helicopter, install smog ejecting device additional at home first.
Summary of the invention
The technical problem to be solved in the present invention:
The object of the invention is to design a kind of smog ejecting device mounting bracket of the Z9 of being suitable for series helicopter, for later Z9 family machine is performed and provided support in exhibition or activity.
Technical scheme of the present invention:
A kind of helicopter smog ejecting device mounting bracket, comprises that attachment angle 1, crossbeam 2, longeron 3, block piece 4, overbolt 5 and plain bolt 6 form, and are all connected by bolt.
Rubber pad is all equipped with in all junctions.
Beneficial effect of the present invention:
By the design of smog ejecting device mounting bracket, the installation of smog ejecting device on helicopter is reliable and stable, meets performance mission requirements.
Accompanying drawing explanation
Fig. 1 is birds-eye view of the present invention, and wherein, 1 is that attachment angle, 2 is that crossbeam, 3 is that longeron, 4 is that block piece, 5 is that overbolt, 6 is plain bolt.
Fig. 2 is back view of the present invention, and wherein, 7 is smog ejecting device.
The specific embodiment
A kind of helicopter smog ejecting device mounting bracket, comprises that attachment angle 1, crossbeam 2, longeron 3, block piece 4, overbolt 5 and plain bolt 6 form, and for guaranteeing ability to dismantle, is all connected by bolt.
Because weapon carrier does not allow to carry out secondary processing, therefore attachment angle 1 is connected the connection of employing clamping hoop type with hanger, attachment angle 1 stretches two flange along weapon carrier profile and is stuck on the beam of weapon carrier, can limit like this smog ejecting device hanger up-and-down movement, 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 use plain bolt 6, and block piece 4 also has two flange, is stuck on the reinforced rib before weapon carrier beam, and the constraint of smog ejecting device 7 all completes thus.
For increasing shake-proof ability, easy to assembly and prevent weapon carrier to cause wearing and tearing, rubber pad is all equipped with in all junctions.
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.Firing control line on guided missile hanger is introduced in driving compartment, and be connected with the percussion lock being arranged on chaufeur cycle bar, chaufeur is by the work of percussion lock control aerosol bomb.Percussion lock is arranged on operating console, has two percussion locks, and what can complete a 50s by next percussion lock draws cigarette process, and once lift-off can complete and draw cigarette twice.Draw cigarette process Once you begin, can not manually remove, need complete after drawing cigarette and 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 comprises attachment angle (1), crossbeam (2), longeron (3), block piece (4), overbolt (5) and plain bolt (6) composition, wherein,
It is upper that smog ejecting device (7) is connected to longeron (3) by bolt (5), and it is upper that longeron (3) is connected to two crossbeams (2) by bolt (6), and crossbeam (2) is connected by bolt (6) with attachment angle (1), and each part all adopts rigidity Design;
Attachment angle (1) is connected employing clamping hoop type and connects with hanger, 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 bolt (6) with attachment angle (1), block piece (4) also has two flange, is stuck on the reinforced rib before weapon carrier beam.
2. a kind of helicopter smog ejecting device mounting bracket as claimed in claim 1, is characterized in that, rubber pad is all equipped with in all junctions.
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 true CN103818554A (en) | 2014-05-28 |
| CN103818554B 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) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104384920A (en) * | 2014-08-26 | 2015-03-04 | 中国直升机设计研究所 | Assembly device and method of light helicopter structural part |
| 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 |
| CN105217039A (en) * | 2015-10-08 | 2016-01-06 | 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 (8)
| 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 |
| KR20120052480A (en) * | 2010-11-16 | 2012-05-24 | 대한민국(농촌진흥청장) | Seeding apparatus for unmaned helicopter |
| US20120193476A1 (en) * | 2011-01-27 | 2012-08-02 | Eurocopter | Removable fastener device equipped with attachment means for attaching an external load and with fastener means for fastening said attachment means to an aircraft, an associated aircraft, and an associated method |
-
2012
- 2012-11-16 CN CN201210464343.4A patent/CN103818554B/en not_active Expired - Fee Related
Patent Citations (8)
| 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 |
| KR20120052480A (en) * | 2010-11-16 | 2012-05-24 | 대한민국(농촌진흥청장) | Seeding apparatus for unmaned helicopter |
| US20120193476A1 (en) * | 2011-01-27 | 2012-08-02 | Eurocopter | Removable fastener device equipped with attachment means for attaching an external load and with fastener means for fastening said attachment means to an aircraft, an associated aircraft, and an associated method |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104384920A (en) * | 2014-08-26 | 2015-03-04 | 中国直升机设计研究所 | Assembly device and method of light helicopter structural part |
| 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 |
| CN105217039A (en) * | 2015-10-08 | 2016-01-06 | 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103818554B (en) | 2016-08-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103818554A (en) | Helicopter smoke generator mounting support | |
| CN105799811B (en) | A kind of hood harness and the installation method using the harness | |
| CN105298503B (en) | Small space shield machine separate launching construction method | |
| WO2017095493A3 (en) | Systems and methods for generating safe trajectories for multi-vehicle teams | |
| CN105492302A (en) | Instrument panel crossmember for a vehicle and vehicle with such an instrument panel crossmember | |
| BR112013032732A2 (en) | flight vehicle fairing that has vibration damping blankets | |
| CN207737186U (en) | A kind of unmanned aerial vehicle transportation system | |
| CN205075762U (en) | ESC electrohydraulic control unit fixed bolster | |
| CN202967152U (en) | Universal transport frame for transporting diesel engine with V-shaped hitching leg | |
| CN109795677A (en) | A kind of unmanned plane fast assembling-disassembling landing gear structure | |
| CN204279976U (en) | Transport, mount integrated ammunition carrier | |
| CN204641869U (en) | A kind of power steering oil can fixed sturcture | |
| CN203268167U (en) | Cab rear suspension system | |
| CN202705528U (en) | Skid for automobile coating | |
| CN204099778U (en) | A kind of gas exhaust tube flange structure and automobile | |
| CN203049647U (en) | Bulldozer | |
| CN204981036U (en) | Antedisplacement formula overhead guard for fork truck | |
| CN203666381U (en) | Gas cylinder fixing mechanism for natural gas truck | |
| CN204109793U (en) | A kind of novel C NG gas cylinder installation bracket | |
| CN205325145U (en) | Over -and -under type internal -combustion engine roll -over stand | |
| CN204586521U (en) | A kind of Das Gaspedal mounting bracket | |
| CN204055985U (en) | A kind of verifying model of automobile ceiling framework structure | |
| CN204367875U (en) | A kind of air filter bracket assembly | |
| CN204527293U (en) | A kind of electric powered steering controller mounting bracket | |
| CN203332228U (en) | Instrument board cross beam and automobile |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 |
Granted publication date: 20160824 Termination date: 20171116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |