CN112078810A - Platform of photoelectric observation system in cabin and installation method thereof - Google Patents
Platform of photoelectric observation system in cabin and installation method thereof Download PDFInfo
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- CN112078810A CN112078810A CN202010846325.7A CN202010846325A CN112078810A CN 112078810 A CN112078810 A CN 112078810A CN 202010846325 A CN202010846325 A CN 202010846325A CN 112078810 A CN112078810 A CN 112078810A
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- cabin
- helicopter
- observation system
- workbench
- photoelectric observation
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- 238000000034 method Methods 0.000 title claims abstract description 10
- 238000009434 installation Methods 0.000 title abstract description 9
- 239000000956 alloy Substances 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 230000005693 optoelectronics Effects 0.000 claims 5
- 230000004308 accommodation Effects 0.000 claims 2
- 108010066057 cabin-1 Proteins 0.000 description 21
- 238000007689 inspection Methods 0.000 description 6
- 230000006378 damage Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 208000019462 Occupational injury Diseases 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 206010016256 fatigue Diseases 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000011514 reflex Effects 0.000 description 1
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Classifications
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- 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
- B64D47/00—Equipment not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention relates to the technical field of helicopter airborne platforms, in particular to a cabin interior photoelectric observation system platform and an installation method thereof. A photoelectric observation system platform in a cabin is arranged in a helicopter cabin, four hanging points are arranged in the helicopter cabin, a workbench base is arranged between the four hanging points, and a photoelectric observation system workbench is fixed on the workbench base. In the invention, the workbench base is arranged in the space between the four hanging points in the helicopter cabin, and the photoelectric observation system work ticket is fixed on the workbench base, so that the photoelectric observation system work table can be prevented from being arranged on a seat of the helicopter cabin, and then the photoelectric observation system work table is prevented from occupying two helicopter guest seats, so that the photoelectric observation system work table can not occupy the overlarge space of the helicopter cabin, the problem that the photoelectric observation system work table in the helicopter cabin occupies too much space in the prior art is solved, the working environment of an inspector is improved, and the working efficiency of the inspector is improved.
Description
Technical Field
The invention relates to the technical field of helicopter airborne workbenches, in particular to a cabin interior photoelectric observation system platform and an installation method thereof.
Background
The less cabin space of helicopter organism is comparatively compel, and current photoelectric observation system workstation is because of lacking the position of placing and the support of specialty, when carrying out the operation, generally places the workstation on the cabin seat, has occupied two helicopter guest seats for originally narrow and small cabin is more crowded, influences the helicopter even and patrols the normal work of line person.
Meanwhile, because the workbench is directly placed on a seat in the cabin, data lines in the cabin of the helicopter are relatively messy. Especially infrared inspector because data line is more mixed and disorderly in the cabin, its station environment is relatively poor, makes infrared inspector keep the operation posture for a long time, and the health receives fatigue injury easily, if meet helicopter special circumstances, infrared inspector appears easily can be because of the setting of station environment difference and equipment position, is difficult to the dangerous condition of breaking away from fast.
Disclosure of Invention
The invention aims to: the invention provides a photoelectric observation system platform in a cabin and an installation method thereof, aiming at solving the problem that the photoelectric observation system workbench in the cabin occupies too much cabin space in the prior art.
In order to solve the problems in the prior art, the invention adopts the following technical scheme:
the utility model provides an in-cabin photoelectric observation system workstation, sets up in the helicopter cabin, be provided with four in the helicopter cabin and hang the point, be provided with the workstation base between four hanging the point, the photoelectric observation system workstation is fixed on the workstation base.
As an improvement of the technical scheme of the workbench of the photoelectric observation system in the cabin, the four hanging points are arranged on the lower part of the cabin of the helicopter cabin, and the workbench base is made of aviation-grade alloy materials and detachably connected to the helicopter cabin through bolts or buckles.
As an improvement of the technical scheme of the photoelectric observation system workbench in the engine room, the photoelectric observation system workbench comprises a pod cabinet, and the pod cabinet is arranged on a workbench base.
As an improvement of the technical scheme of the workbench of the photoelectric observation system in the nacelle, the workbench base is also provided with a support made of an aviation-grade alloy material, the support is fixed on the workbench base, and the nacelle cabinet is fixed on the support.
The improvement of the technical scheme of the workbench of the photoelectric observation system in the cabin is characterized in that an accommodating space is formed between the four hanging points, and the accommodating space is arranged between the front seat of the helicopter and the rear seat of the helicopter.
As an improvement of the technical scheme of the workbench of the photoelectric observation system in the cabin, the workbench base comprises a bottom plate, and the front end of the bottom plate is provided with at least two connecting parts connected with a front seat of the helicopter; the rear end of the bottom plate is fixed below the helicopter rear seat through a buckle.
The method for installing the workbench of the photoelectric observation system in the cabin comprises the following steps:
measuring the distance between four hanging points in a helicopter cabin, and calculating the space size between the four hanging points;
manufacturing a workbench base based on the space size;
fixing the workbench base in the helicopter cabin through bolts or buckles;
and installing a photoelectric observation system workbench on the workbench base.
The invention has the beneficial effects that:
in the invention, the workbench base is arranged in the space between the four hanging points in the helicopter cabin, and the photoelectric observation system work ticket is fixed on the workbench base, so that the photoelectric observation system work table can be prevented from being arranged on a seat of the helicopter cabin, and then the photoelectric observation system work table is prevented from occupying two helicopter guest seats, so that the photoelectric observation system work table can not occupy the overlarge space of the helicopter cabin, the problem that the photoelectric observation system work table in the helicopter cabin occupies too much space in the prior art is solved, the working environment of an inspector is improved, and the working efficiency of the inspector is improved.
Drawings
FIG. 1 is a schematic illustration of the structure within a nacelle of the present invention;
FIG. 2 is a schematic structural view of a base of the workbench according to the present invention;
fig. 3 is an installation flow chart of the installation method of the platform of the photoelectric observation system in the cabin of the invention.
Description of reference numerals: 1-a helicopter nacelle; 2-a table base; 3-pod cabinets; 4-a scaffold; 5-a helicopter front seat; 6-helicopter rear seats; 7-a bottom plate; 8-a connecting part; 9-buckling.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of embodiments of the present invention, and not all embodiments.
In the present invention, a helicopter model AS350B3 is taken AS an example. The AS350B3 helicopter is usually used AS a passenger plane, corresponding operation hanging points are not fully arranged in a cabin, and related modification of the helicopter is strictly controlled by the national civil aviation administration, helicopter manufacturers and helicopter operators, so that modification of the helicopter for line patrol businesses of a company is impossible.
The AS350B3 model helicopter cabin comprises a passenger cabin, wherein the passenger cabin comprises a front helicopter seat 5 and a rear helicopter seat 6, and four hanging points are arranged on the lower part of the helicopter cabin 1. The photoelectric observation system workbench comprises a photoelectric observation system, the photoelectric observation system integrates infrared inspection equipment for operation and control, data lines are regular, and inspection tools such as a single lens reflex, a telescope and/or a range finder are stored and other safety guarantee facilities are arranged.
As shown in figure 1, the photoelectric observation system workbench in the cabin is arranged in a helicopter cabin 1, four hanging points are arranged in the helicopter cabin 1, a workbench base 2 is arranged between the four hanging points, and the photoelectric observation system workbench is fixed on the workbench base 2.
Furthermore, an accommodating space is formed between the four hanging points and is arranged between the front helicopter seat 5 and the rear helicopter seat 6.
Because four hanging points are arranged on the lower part of the helicopter cabin 1, and the accommodating space is arranged between the front helicopter seat 5 and the rear helicopter seat 6, the photoelectric observation system workbench can be prevented from being arranged on the seat of the helicopter cabin 1, and then the photoelectric observation system workbench is prevented from occupying two helicopter passenger seats, so that the photoelectric observation system workbench cannot occupy the overlarge space of the helicopter cabin 1, the problem that the photoelectric observation system workbench in the helicopter cabin occupies too much cabin space in the prior art is solved, the working environment of an inspector is improved, and the working efficiency of the inspector is improved.
Furthermore, four hanging points are arranged on the lower part of a cabin of the helicopter cabin 1, the workbench base 2 is made of an aviation-grade alloy material, and the workbench base 2 is detachably connected to the helicopter cabin 1 through bolts or buckles 9. The workbench base 2 can be connected with the helicopter cabin 1 through a conventional connection mode, as an implementation mode of the invention, the invention is detachably connected on the helicopter cabin 1 through a bolt or a buckle 9, so that the effect of detachably arranging on the helicopter cabin 1 can be realized, an inspector can conveniently and selectively install the workbench base 2 and the photoelectric observation system workbench on the helicopter cabin 1 according to whether the inspection is needed, and the disassembly and assembly time can be reduced and the inspection efficiency can be improved due to the connection through the bolt or the buckle 9 during the disassembly or the installation.
The photoelectric observation system workbench comprises a pod cabinet 3, the pod cabinet 3 is arranged on a workbench base 2, the pod cabinet 3 is fixed through the workbench base 2, the occupied space of the photoelectric observation system workbench can be increased upwards, too much space of a helicopter cabin 1 does not need to be occupied, and the photoelectric observation system workbench is convenient to disassemble or assemble integrally. Preferably, a bracket 4 made of an aviation-grade alloy material is further arranged on the workbench base 2, the bracket 4 is fixed on the workbench base 2, and the pod cabinet 3 is fixed on the bracket 4. Prop up nacelle rack 3 through support 4, make the below of nacelle rack 3 leave empty, the extension of the especially foot of the personnel's health of being convenient for patroller, make the personnel of patrolling and examining keep comfortable operation posture at the in-process of patrolling and examining, when dangerous appearing, the personnel of patrolling and examining also can leave fast, break away from danger as soon as possible. Meanwhile, the bracket 4 is made of an aviation-grade alloy material, so that the weight of the bracket 4 can be reduced, the weight of the helicopter is reduced, and the safety of flight can be ensured. Preferably, the support 4 is a telescopic support 4, and the horizontal height of the nacelle cabinet 3 is adjusted through the support 4, so that a patroller can conveniently perform patrol and data information acquisition.
As shown in fig. 2, as an embodiment of the present invention, the workbench base 2 comprises a bottom plate 7, at least two connecting parts 8 connected with the front seat 5 of the helicopter are arranged on the front end of the bottom plate 7, and the rear end of the bottom plate 7 is fixed under the helicopter seat through a buckle 9. When in use, the workbench base 2 is connected with the front helicopter seat 5 through the connecting part 8, so that the front end of the workbench base 2 is fixed at the front helicopter seat 5. The rear end of the workbench base 2 is fixed in the helicopter cabin 1 through a conventional connection mode, in the invention, for example, the buckle 9 is connected, the rear end of the workbench base 2 is fixed on the ground of the helicopter cabin 1 through the buckle 9, and the ground is arranged below a workbench rear seat, namely, the rear end of the workbench base 2 is fixed through the buckle 9, and the fixed position is arranged below the helicopter rear seat 6, so that the space of the helicopter cabin 1 is optimized.
In the invention, the helicopter electric power line patrol service integrally adopts the helicopter as a flight workbench to carry out work, so that the helicopter flight is the core work of the helicopter electric power line patrol service, the helicopter flight has important requirements on the takeoff weight, and the takeoff weight directly influences important flight indexes such as takeoff safety, cruise time and the like. Therefore, the whole weight of the workbench of the photoelectric observation system in the helicopter cabin is also restricted, and in order to ensure the structural strength of the workbench of the photoelectric observation system, the workbench of the photoelectric observation system in the helicopter cabin 1 is integrally made of aviation-grade alloy main materials which have the characteristics of high strength, light weight, easy cutting and processing and the like. The photoelectric observation system workbench in the helicopter cabin is an independently designed product, each part and each connecting piece of the workbench are required to be independently designed and modeled, and part of structural connecting pieces are required to be connected with the helicopter and are subjected to special treatment, so that fine grinding is carried out, and mutual influence or mutual damage of the parts and the helicopter is avoided.
As shown in fig. 3, the present invention further provides a method for installing a workbench of an indoor photoelectric observation system, including the following steps:
measuring the distance between four hanging points in the helicopter cabin 1;
calculating the space size of the accommodating space based on the distance;
manufacturing the table base 2 based on the size of the space;
the workbench base 2 is fixed in the accommodating space through a bolt or a buckle 9;
and installing a photoelectric observation system workbench on the workbench base 2.
In the present invention, the size and available space of the main part of the cabin of the helicopter model AS350B3 are first measured using four hanging points in the cabin 1 of the helicopter model AS350B 3. Through the combination of the alloy material component of aviation level, utilize four hanging points in the cabin to build workstation base 2, adjust the bottom of nacelle rack 3, adopt bolt or buckle 9's connected mode to install the photoelectric observation system workstation on workstation base 2, thus, the space of helicopter cabin 1 of AS350B3 type helicopter has been integrated, the installation of helicopter inspection equipment has been standardized, the space utilization of AS350B3 type helicopter cabin 1 has been improved, more reasonable for the inspector provides, more comfortable operational environment, the risk of the occupational injury that narrow and small space probably caused the inspector has been reduced, the work efficiency of helicopter inspection is improved.
All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present invention without making any creative effort, shall fall within the protection scope of the present invention.
Claims (7)
1. The utility model provides an in-cabin photoelectric observation system workstation, sets up in the helicopter cabin, be provided with four in the helicopter cabin and hang the point, its characterized in that, be provided with the workstation base between four hanging the point, the photoelectric observation system workstation is fixed on the workstation base.
2. The under-cabin optoelectronic observation system workbench according to claim 1, wherein the four hanging points are disposed on the lower part of the cabin of the helicopter cabin, and the workbench base is made of an aviation-grade alloy material and detachably connected to the helicopter cabin by bolts or fasteners.
3. The under-cabin optoelectronic observation system workbench according to claim 2, wherein the optoelectronic observation system workbench comprises a pod cabinet, and the pod cabinet is disposed on the workbench base.
4. The under-cabin optoelectronic observation system workbench according to claim 3, wherein a support made of an aviation-grade alloy material is further disposed on the workbench base, the support is fixed on the workbench base, and the pod cabinet is fixed on the support.
5. The under-cabin optoelectronic observation system workbench according to any one of claims 1 to 4, wherein an accommodation space is formed between the four hanging points, and the accommodation space is disposed between the front seat of the helicopter and the rear seat of the helicopter.
6. The under-cabin photoelectric observation system workbench according to claim 5, wherein the workbench base comprises a bottom plate, and at least two connecting parts connected with a front seat of the helicopter are arranged on the front end of the bottom plate; the rear end of the bottom plate is fixed below the helicopter rear seat through a buckle.
7. A method of installing a workstation of an electro-optical surveillance system in a nacelle according to any of claims 1 to 6, comprising the steps of:
measuring the distance between four hanging points in a helicopter cabin, and calculating the space size between the four hanging points;
manufacturing a workbench base based on the space size;
fixing the workbench base in the helicopter cabin through bolts or buckles;
and installing a photoelectric observation system workbench on the workbench base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010846325.7A CN112078810A (en) | 2020-08-20 | 2020-08-20 | Platform of photoelectric observation system in cabin and installation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010846325.7A CN112078810A (en) | 2020-08-20 | 2020-08-20 | Platform of photoelectric observation system in cabin and installation method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112078810A true CN112078810A (en) | 2020-12-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010846325.7A Pending CN112078810A (en) | 2020-08-20 | 2020-08-20 | Platform of photoelectric observation system in cabin and installation method thereof |
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| Country | Link |
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| CN (1) | CN112078810A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201439383U (en) * | 2009-07-14 | 2010-04-21 | 华北电网有限公司北京超高压公司 | Support frame for pod of helicopter |
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| US20120217345A1 (en) * | 2011-02-28 | 2012-08-30 | Marenco Swisshelicopter AG Engineering & Consulting | Observation port and a helicopter cabin |
| CN204391601U (en) * | 2014-08-01 | 2015-06-10 | 南方电网科学研究院有限责任公司 | Photoelectric pod universal system for helicopter inspection |
| CN205221129U (en) * | 2015-10-29 | 2016-05-11 | 重庆通用航空产业集团有限公司 | Helicopter is used and is not surveyd optoelectronic system to ground |
| US20160214702A1 (en) * | 2015-01-28 | 2016-07-28 | Marenco Swisshelicopter Ag | Helicopter cabin |
| CN106603967A (en) * | 2016-08-31 | 2017-04-26 | 广州科易光电技术有限公司 | Electric power inspection system |
| CN206155803U (en) * | 2016-08-31 | 2017-05-10 | 广州科易光电技术有限公司 | Rack of helicopter rack base and applied this base |
| CN107685869A (en) * | 2017-08-23 | 2018-02-13 | 天津津航技术物理研究所 | A kind of large photoelectric gondola installing mechanism |
-
2020
- 2020-08-20 CN CN202010846325.7A patent/CN112078810A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201439383U (en) * | 2009-07-14 | 2010-04-21 | 华北电网有限公司北京超高压公司 | Support frame for pod of helicopter |
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| US20120217345A1 (en) * | 2011-02-28 | 2012-08-30 | Marenco Swisshelicopter AG Engineering & Consulting | Observation port and a helicopter cabin |
| CN204391601U (en) * | 2014-08-01 | 2015-06-10 | 南方电网科学研究院有限责任公司 | Photoelectric pod universal system for helicopter inspection |
| US20160214702A1 (en) * | 2015-01-28 | 2016-07-28 | Marenco Swisshelicopter Ag | Helicopter cabin |
| CN205221129U (en) * | 2015-10-29 | 2016-05-11 | 重庆通用航空产业集团有限公司 | Helicopter is used and is not surveyd optoelectronic system to ground |
| CN106603967A (en) * | 2016-08-31 | 2017-04-26 | 广州科易光电技术有限公司 | Electric power inspection system |
| CN206155803U (en) * | 2016-08-31 | 2017-05-10 | 广州科易光电技术有限公司 | Rack of helicopter rack base and applied this base |
| CN107685869A (en) * | 2017-08-23 | 2018-02-13 | 天津津航技术物理研究所 | A kind of large photoelectric gondola installing mechanism |
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Application publication date: 20201215 |