CN114352886A - Airborne equipment multiplexing type mounting structure - Google Patents
Airborne equipment multiplexing type mounting structure Download PDFInfo
- Publication number
- CN114352886A CN114352886A CN202210110352.7A CN202210110352A CN114352886A CN 114352886 A CN114352886 A CN 114352886A CN 202210110352 A CN202210110352 A CN 202210110352A CN 114352886 A CN114352886 A CN 114352886A
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- Prior art keywords
- main frame
- bracket
- installation
- mounting structure
- plate
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- 230000000712 assembly Effects 0.000 claims abstract description 5
- 238000000429 assembly Methods 0.000 claims abstract description 5
- 238000005192 partition Methods 0.000 claims description 6
- 238000009434 installation Methods 0.000 abstract description 39
- 238000013461 design Methods 0.000 abstract description 16
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 238000012545 processing Methods 0.000 abstract description 3
- 238000004891 communication Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/041—Allowing quick release of the apparatus
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/24—Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
The invention discloses a multiplexing mounting structure of airborne equipment, which comprises a main frame structure and an expansion base structure, wherein the main frame structure comprises a main frame and a plurality of bracket assemblies, the bracket assemblies comprise a bracket for mounting standardized mini-enclosure equipment, the bracket is arranged on the main frame, the expanding base structure is arranged at the bottom of the main frame structure, the invention realizes the installation of equipment with the same type and the same specification of a system with the same function in different types through the whole main frame structure, the installation of the devices with difference in different machine types is realized by utilizing the expanded base structure, the design of a multiplex installation structure is realized, and the device has the characteristics of simple design, convenient disassembly and assembly and easy processing and manufacturing, and the common installation requirement and the difference compatible installation requirement of the dynamic relative positioning system in multiple models are met simultaneously.
Description
[ technical field ] A method for producing a semiconductor device
The invention belongs to the field of machinery, and particularly relates to a multiplexing type mounting structure of airborne equipment.
[ background of the invention ]
The structure multiplexing design of the airborne equipment can ensure that the product has high precision, stable performance, simple structure, strong maintainability, low cost and the like, and can be embodied in ASAAC standards, ARINC specifications and the like. However, due to the influence of factors such as the complicated installation environment and the strict installation requirement of the airborne equipment, in electronic equipment of different models or different systems of the same model, the design of an installation structure scheme and an installation scheme of non-standard airborne equipment is often required, and different numbers of standard chassis and different numbers of non-standard chassis are installed and used together. For example, the model a only includes one communication device and two standardized chassis devices, and the model B includes one communication device, one power supply device and two standardized chassis devices. Meanwhile, the same communication equipment and one standardized case device are used in the A model and the B model, and the other standardized case device belongs to different products. Therefore, the design method of the multiplexing type mounting structure is generally suitable for the design of a mounting scheme of a multi-equipment system on multiple models, and has non-negligible economic value, and the multiplexing type mounting structure is convenient to disassemble and assemble and easy to process and manufacture, meets the common mounting requirement and the difference compatibility requirement of a multi-project same-function system, and has the characteristic of realizing the use requirement of quick disassembly and assembly aiming at the small standard case.
[ summary of the invention ]
The invention aims to provide a multiplexing type mounting structure of airborne equipment, which is used for solving the problems that the mounting structure in the prior art is complex in structure and cannot be generally applied to a multi-equipment system on a multi-machine type.
In order to achieve the above object, the reusable mounting structure for airborne equipment according to the present invention includes a main frame structure and an extended base structure, wherein the main frame structure includes a main frame and a plurality of bracket assemblies, each bracket assembly includes a bracket for mounting standardized small-sized enclosure equipment, the bracket is mounted on the main frame, and the extended base structure is mounted at the bottom of the main frame structure.
According to the main characteristics, the main frame comprises an upper transverse plate, a middle partition plate, a left side plate, a right side plate, a bottom plate assembly and a rear plate assembly, the middle partition plate is arranged between the upper transverse plate and the bottom plate assembly, the rear plate assembly comprises a rear plate and four positioning pins arranged on the rear plate, the bottom plate assembly comprises a bottom plate and two front fastening devices arranged on the bottom plate, and the bracket is positioned through the positioning pins on the rear plate and is fixed through the front fastening devices on the bottom plate.
According to the main feature, the bracket assembly further comprises a fastening hook mounted on the bracket.
According to the above main feature, the expanding base structure comprises a base plate and two bottom side plates.
Compared with the prior art, the airborne equipment multiplexing installation structure of the invention realizes the quick assembly and disassembly of the standardized small-sized equipment by utilizing the bracket assembly in the main frame structure, thereby realizing the installation of the same type and same specification equipment of the same function system in different types through the whole main frame structure, the installation of the devices with difference in different machine types is realized by utilizing the expanded base structure, the design of a multiplex installation structure is realized, and the device has the characteristics of simple design, convenient disassembly and assembly and easy processing and manufacturing, simultaneously meets the common installation requirement and the differential compatible installation requirement of the dynamic relative positioning system in multiple models, obviously reduces the design cost, improves the enterprise efficiency, the design method of the installation structure is generally suitable for the design of the installation scheme of the multi-equipment system on multiple models, and has considerable economic value.
[ description of the drawings ]
Fig. 1 is a schematic perspective view of an airborne equipment multiplexing installation structure for implementing the present invention.
Fig. 2 is a schematic view of a first embodiment of an on-board equipment multiplexed mounting structure embodying the present invention.
Fig. 3 is a schematic diagram of a second embodiment of an on-board equipment multiplexed mounting structure embodying the present invention.
[ detailed description ] embodiments
Fig. 1 is a schematic perspective view of a multiplexing-type mounting structure for airborne equipment according to the present invention. The airborne equipment multiplexing type mounting structure comprises an aluminum alloy main frame structure 1 and an aluminum alloy expanding base structure. The main frame structure comprises a main frame and a plurality of bracket assemblies arranged on the main frame, the main frame comprises an upper transverse plate 6, a middle partition plate 7, a left side plate 3, a right side plate 8, a bottom plate assembly 12 and a rear plate assembly 5, the middle partition plate 7 is arranged between the upper transverse plate 6 and the bottom plate assembly 12, so that the main frame is divided into an upper layer structure and a lower layer structure, and a plurality of accommodating spaces are formed. The bracket assembly comprises a first bracket assembly 4 and a second bracket assembly 9, four stainless steel positioning pins are mounted on the back plate assembly 5, two front fasteners 11 are mounted on a bottom plate assembly 12, and a stainless steel fastening hook 10 is mounted on each of the first bracket assembly 4 and the second bracket assembly 9. The extended base structure comprises a base panel 14, a first base side panel 13 and a second base side panel 15.
Please refer to fig. 2 and fig. 3, which are schematic diagrams illustrating a first and a second embodiments of an airborne equipment multiplexing-type mounting structure for implementing the present invention. Aiming at the common installation requirements of systems with the same functions in different machine types, the airborne equipment multiplexing installation structure provided by the invention realizes a uniform installation structure by using the main frame structure 1, and realizes the different installation requirements by using the expansion base structure 2. In the dynamic relative positioning system, both the same type or the same specification of electronic equipment, such as the communication equipment 16, the first, second, and third standardized small cabinet devices 17, 18, and 19, and different numbers and different types of electronic equipment, such as the power supply device 20, and the like, are used in different models. A unified installation structure is designed according to common installation requirements in different models, the main frame structure 1 simultaneously meets all installation requirements of the system in the model a shown in fig. 2 and most installation requirements in the model B shown in fig. 3, and the two models both use the communication equipment 16 of the same model and two small cases of the same standard. The expansion base structure 2 can be used to meet the installation requirement of the additional power supply device 20 required by the model B shown in fig. 3 according to the differential installation requirement of different models.
In addition, aiming at electronic equipment with different functions in common installation requirements of systems with the same function in different models, the airborne equipment multiplexing installation structure for implementing the invention is correspondingly provided with a quick-release installation structure which is easy to disassemble and replace, for example, a first standardized small case 17 and a second standardized small case 18 which are used in a model A and a first standardized small case 17 and a third standardized small case 19 which are used in a model B shown in figure 2 belong to the same standard small cases, aiming at the standardized small cases, the standardized small cases can be installed by adopting a mode of fixing screws on structural members, so that a first bracket assembly 4 and a second bracket assembly 9 are used for carrying the cases, the quick disassembly and assembly between the first bracket assembly 4 and the second bracket assembly 9 and the main frame structure 1 are realized by a preposed fastening device 11, the quick disassembly and assembly requirements of the standardized small cases are indirectly realized, the use convenience is improved, and the requirement of interchangeability of the mounting structure is met.
Compared with the prior art, the airborne equipment multiplexing installation structure of the invention realizes the quick assembly and disassembly of the standardized small-sized equipment by utilizing the bracket assembly in the main frame structure, thereby realizing the installation of the same type and same specification equipment of the same function system in different types through the whole main frame structure, the installation of the devices with difference in different machine types is realized by utilizing the expanded base structure, the design of a multiplex installation structure is realized, and the device has the characteristics of simple design, convenient disassembly and assembly and easy processing and manufacturing, simultaneously meets the common installation requirement and the differential compatible installation requirement of the dynamic relative positioning system in multiple models, obviously reduces the design cost, improves the enterprise efficiency, the design method of the installation structure is generally suitable for the design of the installation scheme of the multi-equipment system on multiple models, and has considerable economic value.
It should be understood that equivalents and modifications of the technical solution and inventive concept thereof may occur to those skilled in the art, and all such modifications and alterations should fall within the scope of the appended claims.
Claims (6)
1. The utility model provides a multiplexing formula mounting structure of airborne equipment which characterized in that: the multiplexing type mounting structure of the airborne equipment comprises a main frame structure and an expansion base structure, wherein the main frame structure comprises a main frame and a plurality of bracket assemblies, each bracket assembly comprises a bracket used for mounting the standardized small-sized case equipment, the bracket is mounted on the main frame, and the expansion base structure is mounted at the bottom of the main frame structure.
2. The on-board unit multiplex mounting structure of claim 1, wherein: the main frame comprises an upper transverse plate, a middle partition plate, a left side plate, a right side plate, a bottom plate assembly and a rear plate assembly, wherein the middle partition plate is arranged between the upper transverse plate and the bottom plate assembly.
3. The on-board unit multiplex mounting structure of claim 2, wherein: the back plate assembly includes a back plate and four locating pins mounted thereon.
4. The on-board unit multiplex mounting structure of claim 2, wherein: the base plate assembly includes a base plate and two leading fasteners mounted thereto.
5. The on-board unit multiplex mounting structure of claim 2, wherein: the bracket assembly also includes a fastening hook mounted to the bracket.
6. The on-board unit multiplex mounting structure of claim 2, wherein: the expanding base structure comprises a base plate and two bottom side plates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210110352.7A CN114352886A (en) | 2022-01-29 | 2022-01-29 | Airborne equipment multiplexing type mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210110352.7A CN114352886A (en) | 2022-01-29 | 2022-01-29 | Airborne equipment multiplexing type mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114352886A true CN114352886A (en) | 2022-04-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210110352.7A Pending CN114352886A (en) | 2022-01-29 | 2022-01-29 | Airborne equipment multiplexing type mounting structure |
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Citations (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4687127A (en) * | 1985-03-28 | 1987-08-18 | Barry Wright Corporation | Avionic tray gasket assembly |
| KR20050066338A (en) * | 2003-12-26 | 2005-06-30 | 엘지전자 주식회사 | Shelf for communication device |
| CN200966190Y (en) * | 2006-11-07 | 2007-10-24 | 中国船舶重工集团公司第七二二研究所 | Irregular electronic box body |
| CN101268726A (en) * | 2005-09-19 | 2008-09-17 | 空中客车德国有限公司 | Avionics equipment carrier system with quick-mount housing and quick-mount modules |
| CN201296386Y (en) * | 2008-12-02 | 2009-08-26 | 中国电子科技集团公司第十四研究所 | Composite material light colligate device machine frame |
| CN101730453A (en) * | 2009-12-11 | 2010-06-09 | 中国航空无线电电子研究所 | Open integrated liquid-cooled machine frame system |
| CN202759715U (en) * | 2012-07-25 | 2013-02-27 | 中兴通讯股份有限公司 | Chassis |
| CN104076887A (en) * | 2014-06-30 | 2014-10-01 | 中国航空无线电电子研究所 | Novel case bracket locking mechanism |
| CN204678017U (en) * | 2015-06-12 | 2015-09-30 | 陕西宝成航空仪表有限责任公司 | For the shock-absorbing type scaffold of air equipment |
| CN105874894A (en) * | 2013-12-30 | 2016-08-17 | 戴尔产品有限公司 | Modular, scalable, expandable, rack-based information handling system |
| CN205707391U (en) * | 2016-04-28 | 2016-11-23 | 沈阳兴华航空电器有限责任公司 | A kind of navigator bracket |
| CN205755225U (en) * | 2016-05-19 | 2016-11-30 | 中国航空无线电电子研究所 | A kind of double mode cooling built-in air channel cabinet |
| CN207505261U (en) * | 2017-11-30 | 2018-06-15 | 江西洪都航空工业集团有限责任公司 | A kind of integrated tilting type Avionics Equipment Bay |
| CN108238271A (en) * | 2017-12-20 | 2018-07-03 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of avionic device installs stent concentratedly |
| CN108953953A (en) * | 2018-08-28 | 2018-12-07 | 北京无线电测量研究所 | A kind of limit-type damping mounting rack of airborne electronic equipment cabinet |
| CN109561628A (en) * | 2018-12-24 | 2019-04-02 | 西安现代控制技术研究所 | A kind of modularization integrated electronic case |
| US20190342429A1 (en) * | 2018-05-04 | 2019-11-07 | The Boeing Company | Reconfigurable avionics mounting |
| CN110769638A (en) * | 2019-09-28 | 2020-02-07 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Method for light-weight integrated electronic equipment rack structure |
| CN111503497A (en) * | 2020-05-15 | 2020-08-07 | 沈阳兴华航空电器有限责任公司 | Vibration reduction and air supply mounting rack for airborne equipment |
| CN212480754U (en) * | 2020-05-15 | 2021-02-05 | 沈阳兴华航空电器有限责任公司 | Vibration reduction and air supply mounting rack for airborne equipment |
| CN213043931U (en) * | 2020-07-17 | 2021-04-23 | 中国航空无线电电子研究所 | Joggle joint structure machine case |
-
2022
- 2022-01-29 CN CN202210110352.7A patent/CN114352886A/en active Pending
Patent Citations (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4687127A (en) * | 1985-03-28 | 1987-08-18 | Barry Wright Corporation | Avionic tray gasket assembly |
| KR20050066338A (en) * | 2003-12-26 | 2005-06-30 | 엘지전자 주식회사 | Shelf for communication device |
| CN101268726A (en) * | 2005-09-19 | 2008-09-17 | 空中客车德国有限公司 | Avionics equipment carrier system with quick-mount housing and quick-mount modules |
| CN200966190Y (en) * | 2006-11-07 | 2007-10-24 | 中国船舶重工集团公司第七二二研究所 | Irregular electronic box body |
| CN201296386Y (en) * | 2008-12-02 | 2009-08-26 | 中国电子科技集团公司第十四研究所 | Composite material light colligate device machine frame |
| CN101730453A (en) * | 2009-12-11 | 2010-06-09 | 中国航空无线电电子研究所 | Open integrated liquid-cooled machine frame system |
| CN202759715U (en) * | 2012-07-25 | 2013-02-27 | 中兴通讯股份有限公司 | Chassis |
| CN105874894A (en) * | 2013-12-30 | 2016-08-17 | 戴尔产品有限公司 | Modular, scalable, expandable, rack-based information handling system |
| CN104076887A (en) * | 2014-06-30 | 2014-10-01 | 中国航空无线电电子研究所 | Novel case bracket locking mechanism |
| CN204678017U (en) * | 2015-06-12 | 2015-09-30 | 陕西宝成航空仪表有限责任公司 | For the shock-absorbing type scaffold of air equipment |
| CN205707391U (en) * | 2016-04-28 | 2016-11-23 | 沈阳兴华航空电器有限责任公司 | A kind of navigator bracket |
| CN205755225U (en) * | 2016-05-19 | 2016-11-30 | 中国航空无线电电子研究所 | A kind of double mode cooling built-in air channel cabinet |
| CN207505261U (en) * | 2017-11-30 | 2018-06-15 | 江西洪都航空工业集团有限责任公司 | A kind of integrated tilting type Avionics Equipment Bay |
| CN108238271A (en) * | 2017-12-20 | 2018-07-03 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of avionic device installs stent concentratedly |
| US20190342429A1 (en) * | 2018-05-04 | 2019-11-07 | The Boeing Company | Reconfigurable avionics mounting |
| CN108953953A (en) * | 2018-08-28 | 2018-12-07 | 北京无线电测量研究所 | A kind of limit-type damping mounting rack of airborne electronic equipment cabinet |
| CN109561628A (en) * | 2018-12-24 | 2019-04-02 | 西安现代控制技术研究所 | A kind of modularization integrated electronic case |
| CN110769638A (en) * | 2019-09-28 | 2020-02-07 | 西南电子技术研究所（中国电子科技集团公司第十研究所） | Method for light-weight integrated electronic equipment rack structure |
| CN111503497A (en) * | 2020-05-15 | 2020-08-07 | 沈阳兴华航空电器有限责任公司 | Vibration reduction and air supply mounting rack for airborne equipment |
| CN212480754U (en) * | 2020-05-15 | 2021-02-05 | 沈阳兴华航空电器有限责任公司 | Vibration reduction and air supply mounting rack for airborne equipment |
| CN213043931U (en) * | 2020-07-17 | 2021-04-23 | 中国航空无线电电子研究所 | Joggle joint structure machine case |
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