CN203806143U - Installation platform assembly of aerophotography platform - Google Patents
Installation platform assembly of aerophotography platform Download PDFInfo
- Publication number
- CN203806143U CN203806143U CN201420184712.9U CN201420184712U CN203806143U CN 203806143 U CN203806143 U CN 203806143U CN 201420184712 U CN201420184712 U CN 201420184712U CN 203806143 U CN203806143 U CN 203806143U
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- China
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- platform
- photograph
- taken
- cantilever beam
- erecting stage
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Abstract
The utility model provides an installation platform assembly of an aerophotography platform. The assembly comprises an installation plate and a bearing rod assembly. The bearing rod assembly comprises an installation beam and a cantilever, and the installation plate and the installation beam are arranged at the two ends of the cantilever respectively; the installation beam is provided with machine body connectors connected with a machine body; the cantilever is provided with a concave area, the installation plate is arranged on the concave area, the cantilever is provided with multiple reinforcing foot materials, the installation plate is provided with installation foot materials corresponding to the reinforcing foot materials, and the installation foot materials are connected with the reinforcing foot materials through the connectors. After a camera is arranged on the installation platform assembly of the structure, a whole aerophotography system can be arranged on an airplane through the installation platform assembly, refit of the airplane is omitted, and the aerophotography system can be directly detached from the airplane after working.
Description
Technical field
The utility model relates to Hang She field, high-altitude, and particularly a kind of boat is taken the photograph platform and be fixed on the assembly of erecting stage.
Background technology
It is the system that finger device is photographed to ground on aircraft or other aircraft that boat is taken the photograph system.Boat is taken the photograph system can be for carrying out the occasions such as terrain map of survey and drawing, disaster monitoring, makes mapping serve better the development of the national economy.First the application that boat is taken the photograph system needs to be stably arranged on aircraft.When existing aerial surveying camera is installed, need first aircraft to be reequiped, so that aerial surveying camera is arranged on aircraft and carries out operation according to Its Relevant Technology Standards, the mode of repacking is to output ground photographic window mouth in aircraft cabin bottom, to settle aerial surveying camera and relevant devices.Just need to use dissimilar aircraft when carrying out different tasks, after boat is taken the photograph task and finished, aerial surveying camera is just dismantled from aircraft, still but aircraft can not be restored to the original state.Like this overall performance of aircraft is had to adverse influence, and also increased the use cost of aerial surveying camera.
Utility model content
The utility model object is to need aboard the problem of first aircraft being reequiped, the erecting stage assembly that provides a kind of boat to take the photograph platform in order to overcome existing aerial surveying camera installation.
In order to achieve the above object, the utility model is by the following technical solutions:
Boat is taken the photograph an erecting stage assembly for platform, comprises adapter plate and carrier bar assembly; Described carrier bar assembly comprises mounting rail and cantilever beam, and described adapter plate and mounting rail are separately positioned on first end and the second end of described cantilever beam; Described mounting rail is provided with some fuselage attaching partss that are connected with fuselage; Described cantilever beam is provided with depressed area, described adapter plate is installed on depressed area, the lateral wall of described cantilever beam is provided with some reinforcement pin materials, the marginal portion of the downside of described adapter plate is provided with installation foot material corresponding to some and described reinforcement pin material, and described installation foot material is connected by attaching parts with described reinforcement pin material.
As preferably, described cantilever beam comprises two beam bodies, between two beam bodies, is mutually permanently connected by pipe link; In the depressed area of the first end of described cantilever beam, be provided with the first perforate, adapter plate is provided with the second perforate, and the first perforate communicates with the second perforate.
As preferably, also comprise some groups of adjustable rod assemblies, described adjustable rod assembly comprises head rod, transiting rod and the second pipe link; Transiting rod is provided with the inner core of open at both ends; The first end of described head rod is articulated with the second end of described cantilever beam, the first end thread connection of the second end of described head rod and the inner core of described transiting rod; The second end thread connection of the first end of described the second pipe link and the inner core of described transiting rod.
As preferably, described adjustable lever assembly includes two groups.
As preferably, the second end of described cantilever beam is provided with U-shaped connector, and the first end of described head rod and described U-shaped connector are hinged.
As preferably, the second end of described head rod is by the first inner core that is threadedly connected to described transiting rod; The first end of described the second pipe link is by rotation direction second inner core that be threadedly connected to described transiting rod contrary with described the first screw thread.
As preferably, described head rod is connected by left and right hand thread with the inner core of transiting rod respectively with the second pipe link.
As preferably, the second end of described cantilever beam is provided with some fail safety joints.
As preferably, described fail safety joint arranges four.
As preferably, described fail safety joint is that vertical section is the attachment hardware of L-type, is provided with some connecting bores on described attachment hardware, and two edges of said attachment hardware are across being provided with a reinforced rib.
Compared with prior art, the utlity model has following beneficial effect:
Photographic apparatus is arranged on after the erecting stage assembly of said structure composition, and whole boat is taken the photograph system and can be installed aboard by erecting stage assembly, has exempted the repacking to aircraft; Boat is taken the photograph after system job, can directly disassemble from aircraft.Adapter plate is further fixedly connected with by strengthening pin material and installation foot material with cantilever beam, has improved the fastness of erecting stage assembly, has improved the convenience that dismounting is safeguarded.Adjustable rod assembly is connected with the original mounting interface of fuselage together with mounting rail and fuselage attaching parts thereof, and by the load of erecting stage assembly, for example aerodynamic loading and overloading load, transmit and diffuse to fuselage reinforcing frame.In adjustable rod assembly, by turn head rod and/or the second pipe link or excessive bar, can regulate easily the length of adjustable rod assembly, thereby strengthen the assembly process process of erecting stage assembly and fuselage.Fail safety joint has increased the quantity of erection space and attaching screw, has not only divided equally well the basic load of hazardous location, and the Redundancy Design of erection joint place is also provided, and has greatly improved the safety factor of erecting stage assembly.
Brief description of the drawings
Fig. 1 is application schematic diagram of the present utility model;
Fig. 2 is the enlarged drawing of the A portion of Fig. 1;
Fig. 3 is the enlarged drawing of the B portion of Fig. 1.
In figure:
1-adapter plate; 11-installation foot material; The 12-the second perforate; 21-cantilever beam; 211-reinforcement pin material; The 212-the first perforate; 213-fail safety joint; 2131-attachment hardware; 2132-reinforced rib; 214-beam body; 215-pipe link; 216-U-shaped connector; 22-mounting rail; 221-beam body; 222-pipe link; 3-adjustable rod assembly; 31-head rod; 32-transiting rod; The 33-the second pipe link.
Now the utility model is described in further detail with specific embodiment by reference to the accompanying drawings.
Detailed description of the invention
As shown in Figure 1 to Figure 3, take the photograph the erecting stage assembly of platform for a kind of boat described in the utility model, it mainly comprises adapter plate 1 and carrier bar assembly.
Carrier bar assembly comprises mounting rail 22 and cantilever beam 21.As shown in Figure 3, the structure of mounting rail 22 is: comprise between 221, two beam bodies 221 of two beam bodies and being mutually permanently connected by pipe link 222; Mounting rail 22 is provided with for the mounting hole being connected with fuselage.As shown in Figure 2, the structure of cantilever beam 21 is: comprise between 214, two beam bodies 214 of two beam bodies and being mutually permanently connected by pipe link 215.
Adapter plate 1 and mounting rail 22 are separately positioned on first end and the second end of cantilever beam 21.The first end of cantilever beam 21 is provided with depressed area, is provided with the first perforate 212 in depressed area, and adapter plate 1 is installed on depressed area, and adapter plate 1 is provided with the second perforate 12, the first perforates 212 and communicates with the second perforate 12; As shown in Figure 2, the lateral wall of cantilever beam 21 is provided with some reinforcement pin materials 211, and the marginal portion of the downside of adapter plate 1 is provided with some installation foot materials 11 corresponding with strengthening pin material 211, and installation foot material 11 is connected by screw with reinforcement pin material 211.Mounting rail 22 is provided with some fuselage attaching partss that are connected with fuselage, and fuselage attaching parts is provided with for the mounting hole being connected with fuselage.The second end of cantilever beam 21 is provided with some fail safety joints 213, and as preferred embodiment, fail safety joint 213 arranges four; As shown in Figure 3, the attachment hardware 2131 that fail safety joint 213 is L-type for vertical section, is provided with some connecting bores on attachment hardware 2131, and two edges of attachment hardware 2131 are across being provided with a reinforced rib 2132; Fail safety joint 213 is connected with mounting rail 22.
As shown in Figure 2, strengthen pin material 211 for being arranged on the attaching parts of cantilever beam 21 lateral walls, installation foot material 11 is for being vertically set on the plate-like attaching parts of adapter plate 1 downside.
Also comprise some groups of adjustable rod assemblies 3, as preferred embodiment, adjustable lever assembly is provided with two groups.Adjustable rod assembly 3 comprises head rod 31, transiting rod 32 and the second pipe link 33; Transiting rod 32 is provided with the inner core of open at both ends.The first end of head rod 31 is articulated with the second end of cantilever beam 21, and the second end of head rod 31 is by the first first end that is threadedly connected to the inner core of transiting rod 32; The first end of the second pipe link 33 is by rotation direction second second end that be threadedly connected to the inner core of transiting rod 32 contrary with the first screw thread.The second end of cantilever beam 21 is provided with U-shaped connector 216, and the first end of head rod 31 and U-shaped connector 216 are hinged.As a preferred embodiment, head rod 31 is connected by left and right hand thread with transiting rod 32 respectively with the second pipe link 33.The end of the second end of the second pipe link is set to Gua Hook part, and the end of the second end links directly on the original mounting interface of aircraft.
Application of the present utility model:
First photographic apparatus is arranged on adapter plate 1, the camera of photographic apparatus is in the first perforate 212 and the second perforate 12.
Fuselage attaching parts on mounting rail 22, mounting rail 22 is fixedly connected with by the original mounting interface of screw and fuselage; The end of the second end of the second pipe link 33 of adjustable rod assembly 3 links directly on the original mounting interface of fuselage, can be by whole erecting stage assembly installation aboard.
The effect of the utility model part-structure:
Adapter plate 1 is further fixedly connected with by strengthening pin material 211 and installation foot material 11 with cantilever beam 21, has improved the fastness of erecting stage assembly, strengthens pin material 211 and installation foot material 11 and is connected by screw, and has improved the convenience that dismounting is safeguarded.
Adjustable rod assembly 3 is connected with the original mounting interface of fuselage together with mounting rail 22 and fuselage attaching parts thereof, and by the load of erecting stage assembly, for example aerodynamic loading and overloading load, transmit and diffuse to fuselage reinforcing frame.
In adjustable rod assembly 3, by turn head rod 31 and/or the second pipe link 33 or excessive bar, can regulate easily the length of adjustable rod assembly 3, thereby strengthen the assembly process process of erecting stage assembly and fuselage.
Fail safety joint 213 is connected with mounting rail 22, increase the quantity of erection space and attaching screw, not only divide equally well the basic load of hazardous location, the Redundancy Design of erection joint place is also provided, greatly improved the safety factor of erecting stage assembly.
Head rod 31 and the second pipe link 33 adopt contrary being threaded of rotation direction with the connection of transiting rod 32, when work, and transiting rod 32 parts in the middle of can only rotating, adjustable two pipe links is flexible, i.e. the length of adjustable whole adjustable rod assembly 3.
To sum up, after photographic apparatus is arranged on erecting stage assembly described in the utility model, whole boat is taken the photograph system and is installed aboard by erecting stage assembly, has exempted the repacking to aircraft; Boat is taken the photograph after system job, can directly disassemble from aircraft.
The utility model is not limited to above-mentioned embodiment, if various changes of the present utility model or modification are not departed to spirit and scope of the present utility model, if within these changes and modification belong to claim of the present utility model and equivalent technologies scope, the utility model is also intended to comprise these changes and variation.
Claims (10)
1. boat is taken the photograph an erecting stage assembly for platform, it is characterized in that, comprises adapter plate and carrier bar assembly; Described carrier bar assembly comprises mounting rail and cantilever beam, and described adapter plate and mounting rail are separately positioned on first end and the second end of described cantilever beam; Described mounting rail is provided with some fuselage attaching partss that are connected with fuselage; Described cantilever beam is provided with depressed area, described adapter plate is installed on depressed area, the lateral wall of described cantilever beam is provided with some reinforcement pin materials, the marginal portion of the downside of described adapter plate is provided with installation foot material corresponding to some and described reinforcement pin material, and described installation foot material is connected by attaching parts with described reinforcement pin material.
2. boat according to claim 1 is taken the photograph the erecting stage assembly of platform, it is characterized in that, described cantilever beam comprises two beam bodies, between two beam bodies, is mutually permanently connected by pipe link; In the depressed area of the first end of described cantilever beam, be provided with the first perforate, adapter plate is provided with the second perforate, and the first perforate communicates with the second perforate.
3. boat according to claim 1 and 2 is taken the photograph the erecting stage assembly of platform, it is characterized in that, also comprises some groups of adjustable rod assemblies, and described adjustable rod assembly comprises head rod, transiting rod and the second pipe link; Transiting rod is provided with the inner core of open at both ends; The first end of described head rod is articulated with the second end of described cantilever beam, the first end thread connection of the second end of described head rod and the inner core of described transiting rod; The second end thread connection of the first end of described the second pipe link and the inner core of described transiting rod.
4. boat according to claim 3 is taken the photograph the erecting stage assembly of platform, it is characterized in that, described adjustable lever assembly includes two groups.
5. boat according to claim 3 is taken the photograph the erecting stage assembly of platform, it is characterized in that, the second end of described cantilever beam is provided with U-shaped connector, and the first end of described head rod and described U-shaped connector are hinged.
6. boat according to claim 3 is taken the photograph the erecting stage assembly of platform, it is characterized in that, the second end of described head rod is by the first inner core that is threadedly connected to described transiting rod; The first end of described the second pipe link is by rotation direction second inner core that be threadedly connected to described transiting rod contrary with described the first screw thread.
7. boat according to claim 6 is taken the photograph the erecting stage assembly of platform, it is characterized in that, described head rod is connected by left and right hand thread with the inner core of transiting rod respectively with the second pipe link.
8. boat according to claim 1 is taken the photograph the erecting stage assembly of platform, it is characterized in that, the second end of described cantilever beam is provided with some fail safety joints.
9. boat according to claim 8 is taken the photograph the erecting stage assembly of platform, it is characterized in that, described fail safety joint arranges four.
10. boat according to claim 8 is taken the photograph the erecting stage assembly of platform, it is characterized in that, described fail safety joint is that vertical section is the attachment hardware of L-type, is provided with some connecting bores on described attachment hardware, and two edges of said attachment hardware are across being provided with a reinforced rib.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420184712.9U CN203806143U (en) | 2014-04-16 | 2014-04-16 | Installation platform assembly of aerophotography platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420184712.9U CN203806143U (en) | 2014-04-16 | 2014-04-16 | Installation platform assembly of aerophotography platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203806143U true CN203806143U (en) | 2014-09-03 |
Family
ID=51444936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420184712.9U Expired - Fee Related CN203806143U (en) | 2014-04-16 | 2014-04-16 | Installation platform assembly of aerophotography platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203806143U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882989A (en) * | 2016-01-21 | 2016-08-24 | 西北工业大学 | Installation platform for bilateral hanging detection system of helicopter with three-dimensional static stability |
-
2014
- 2014-04-16 CN CN201420184712.9U patent/CN203806143U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882989A (en) * | 2016-01-21 | 2016-08-24 | 西北工业大学 | Installation platform for bilateral hanging detection system of helicopter with three-dimensional static stability |
| CN105882989B (en) * | 2016-01-21 | 2018-07-06 | 西北工业大学 | Helicopter bilateral hanging detection system mounting platform with three-dimensional static stability |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160622 Address after: 510036 Guangzhou Science City, Luogang District science Avenue, No. 182 innovation building C2 District, No. 101, Patentee after: Guangzhou Redbird Helicopter Remote Sensing Technology Co., Ltd. Address before: 510036, Guangdong, Luogang District Science City, science Road, 182 innovation building, C1 District, Annex 7 floor, Guangzhou Patentee before: Xu Peng |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140903 Termination date: 20210416 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |