CN106379546A - Helicopter horn installation rack - Google Patents
Helicopter horn installation rack Download PDFInfo
- Publication number
- CN106379546A CN106379546A CN201510454594.8A CN201510454594A CN106379546A CN 106379546 A CN106379546 A CN 106379546A CN 201510454594 A CN201510454594 A CN 201510454594A CN 106379546 A CN106379546 A CN 106379546A
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- CN
- China
- Prior art keywords
- web
- rack
- helicopter
- support
- bracket
- 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
- 238000009434 installation Methods 0.000 title abstract description 11
- 238000004378 air conditioning Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
Description
技术领域technical field
本发明属于直升机结构件技术领域,特别是涉及一种直升机喇叭的安装支架。The invention belongs to the technical field of helicopter structural parts, in particular to a mounting bracket for a helicopter horn.
背景技术Background technique
直升机由于执行多种任务的需要,经常配备空中广播系统,以用于直升机驾驶员或机组成员向地面喊话。然而由于直升机机体安装位置和空间的限制,空中广播系统中的喇叭一直安装在行李舱地板下外蒙皮上,这个安装位置同时也是空调系统和多普勒雷达的安装位置,造成三项选装任务设备不能同时安装的困局。Due to the needs of performing various tasks, helicopters are often equipped with an air broadcast system for the helicopter pilot or crew members to shout to the ground. However, due to the limitation of the installation position and space of the helicopter body, the loudspeaker in the air broadcasting system has been installed on the outer skin under the floor of the luggage compartment. This installation position is also the installation position of the air conditioning system and Doppler radar, resulting in three options. The dilemma that mission equipment cannot be installed at the same time.
发明内容Contents of the invention
本发明要解决的技术问题:The technical problem to be solved in the present invention:
通过设计一种直升机喇叭的安装支架,将喇叭安装在直升机机身右侧外蒙皮上,解决喇叭与空调系统和多普勒雷达系统干涉问题,同时考虑喇叭使用、安装、拆卸和维护等特性。本发明的技术方案:By designing a mounting bracket for the helicopter horn, the horn is installed on the outer skin of the right side of the helicopter fuselage to solve the problem of interference between the horn and the air conditioning system and Doppler radar system, while considering the characteristics of the horn use, installation, disassembly and maintenance . Technical scheme of the present invention:
一种直升机喇叭的安装支架,包括支架后腹板5、支架下腹板6、支架前腹板7,支架后腹板5和支架下腹板6通过铆钉铆接,支架下腹板6和支架前腹板7通过铆钉铆接,所述支架后腹板5和支架前腹板7上有支架安装孔3,用于固定喇叭1,所述支架后腹板5和支架前腹板7通过肋上的支架装配孔4使用螺钉螺接在机身蒙皮上,机身蒙皮内预置有嵌入件,各个零件均采用刚度设计。A mounting bracket for a helicopter horn, comprising a bracket rear web 5, a bracket lower web 6, a bracket front web 7, the bracket rear web 5 and the bracket lower web 6 are riveted by rivets, the bracket lower web 6 and the bracket front web 7 Through rivet riveting, there are bracket installation holes 3 on the rear web 5 of the bracket and the front web 7 of the bracket, which are used to fix the horn 1, and the rear web 5 of the bracket and the front web 7 of the bracket pass through the bracket assembly holes on the ribs 4. Use screws to connect to the skin of the fuselage. Inserts are preset in the skin of the fuselage, and each part is designed with rigidity.
支架安装孔3和支架装配孔4处安装有橡胶垫片。Rubber gaskets are installed at the bracket mounting hole 3 and the bracket mounting hole 4.
本发明的有益效果:Beneficial effects of the present invention:
通过新设计支架,将喇叭安装在直升机尾段机身右侧外部蒙皮上,即解决设备间的干涉问题,同时解决空中广播系统安装使用,并考虑喇叭的快速拆卸更换方便。Through the newly designed bracket, the horn is installed on the outer skin on the right side of the tail section of the helicopter, which solves the problem of interference between equipment, and at the same time solves the installation and use of the air broadcast system, and considers the quick disassembly and replacement of the horn.
附图说明Description of drawings
图1为本发明的零件分解图,其中,5为支架后腹板、6为支架下腹板、7为支架前腹板。Fig. 1 is an exploded view of parts of the present invention, wherein, 5 is the rear web of the bracket, 6 is the lower web of the bracket, and 7 is the front web of the bracket.
图2为本发明的组件图。Figure 2 is a component diagram of the present invention.
图3为本发明在直升机上的安装位置示意图。Fig. 3 is a schematic diagram of the installation position of the present invention on a helicopter.
具体实施方式detailed description
一种直升机喇叭的安装支架,包括支架后腹板5、支架下腹板6、支架前腹板7组成。A mounting bracket for a helicopter horn, comprising a rear web 5 of the bracket, a lower web 6 of the bracket, and a front web 7 of the bracket.
支架后腹板5和支架下腹板6通过铆钉铆接,支架下腹板6和支架前腹板7通过铆钉铆接,支架后腹板5和支架前腹板7上有支架安装孔3,用于固定喇叭1。The rear web 5 of the bracket and the lower web 6 of the bracket are riveted by rivets, the lower web 6 of the bracket and the front web 7 of the bracket are riveted by rivets, and there are bracket installation holes 3 on the rear web 5 of the bracket and the front web 7 of the bracket, which are used to fix the horn 1.
支架后腹板5和支架前腹板7通过肋上的支架装配孔4使用螺钉螺接在机身蒙皮上,机身蒙皮内预置有嵌入件,各个零件均采用刚度设计。The rear web 5 of the bracket and the front web 7 of the bracket are screwed to the fuselage skin through the bracket assembly hole 4 on the rib. Inserts are preset in the fuselage skin, and each part adopts rigidity design.
为增加防震能力、装配方便以及防止对机身蒙皮造成磨损,螺栓连接处装有橡胶垫片。In order to increase the shock resistance, facilitate assembly and prevent abrasion to the skin of the fuselage, rubber gaskets are installed at the bolt joints.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510454594.8A CN106379546A (en) | 2015-07-29 | 2015-07-29 | Helicopter horn installation rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510454594.8A CN106379546A (en) | 2015-07-29 | 2015-07-29 | Helicopter horn installation rack |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106379546A true CN106379546A (en) | 2017-02-08 |
Family
ID=57916153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510454594.8A Pending CN106379546A (en) | 2015-07-29 | 2015-07-29 | Helicopter horn installation rack |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106379546A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2694154A1 (en) * | 1992-07-24 | 1994-01-28 | Vibrachoc Sa | Support for aircraft electrical equipment box. |
| CN2410712Y (en) * | 1999-12-28 | 2000-12-13 | 钟大地 | Helicopter type audiovisual device |
| WO2003024175A1 (en) * | 2001-09-13 | 2003-03-20 | The Boeing Company | Method to install equipment racks in aircraft |
| CN102098610A (en) * | 2011-03-11 | 2011-06-15 | 湖南继善高科技有限公司 | Loudspeaker unit, loudspeaking device and orientated sound wave bird driving device |
| CN202686770U (en) * | 2012-07-13 | 2013-01-23 | 哈尔滨飞机工业集团有限责任公司 | Installation structure of air loudspeaker |
-
2015
- 2015-07-29 CN CN201510454594.8A patent/CN106379546A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2694154A1 (en) * | 1992-07-24 | 1994-01-28 | Vibrachoc Sa | Support for aircraft electrical equipment box. |
| CN2410712Y (en) * | 1999-12-28 | 2000-12-13 | 钟大地 | Helicopter type audiovisual device |
| WO2003024175A1 (en) * | 2001-09-13 | 2003-03-20 | The Boeing Company | Method to install equipment racks in aircraft |
| CN102098610A (en) * | 2011-03-11 | 2011-06-15 | 湖南继善高科技有限公司 | Loudspeaker unit, loudspeaking device and orientated sound wave bird driving device |
| CN202686770U (en) * | 2012-07-13 | 2013-01-23 | 哈尔滨飞机工业集团有限责任公司 | Installation structure of air loudspeaker |
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| PB01 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170208 |
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| WD01 | Invention patent application deemed withdrawn after publication |