CN205034350U - A mounted frame for on multiaxis aircraft - Google Patents
A mounted frame for on multiaxis aircraft Download PDFInfo
- Publication number
- CN205034350U CN205034350U CN201520818414.5U CN201520818414U CN205034350U CN 205034350 U CN205034350 U CN 205034350U CN 201520818414 U CN201520818414 U CN 201520818414U CN 205034350 U CN205034350 U CN 205034350U
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- CN
- China
- Prior art keywords
- suspension arm
- hanger bracket
- shaped groove
- bar shaped
- utility
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- Expired - Fee Related
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Abstract
The utility model relates to a multiaxis aircraft part, concretely relates to a mounted frame for on multiaxis aircraft, including horizontal bracket, the horizontal bracket below is equipped with two and connects the foot, connects sole portion and is equipped with the installation screw, horizontal bracket's both ends are equipped with a tilt up respectively and hang the arm to what extended in the outside, and the inclination who hangs the arm be 30 -75, hang the arm upper end and are equipped with a C shape and grab the clamp, and double -layered opening is grabbed towards the setting of the both sides of mounted frame to C shape. The utility model discloses a mounted frame simple structure, light in weight can bear the function equipment fixing of certain weight, the utility model discloses a mounted frame can a plurality ofly be used together, and the installation is dismantled also very conveniently, is applicable to the installation of multiple equipment on the multiaxis aircraft.
Description
Technical field
The utility model relates to a kind of Multi-axis aircraft parts, is specifically related to a kind of hanger bracket on Multi-axis aircraft.
Background technology
Multi-axis aircraft has that volume is little, lightweight, expense is low, flexible operation and safety high, can be widely used in taking photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural.In order to realize these functions, Multi-axis aircraft often needs to carry some equipment bottom frame, as parts such as pick up cameras, these parts are all more difficult after being mounted to the frame of Multi-axis aircraft to be disassembled, install and also extremely bother, extremely bother when needing repairing or needing just to seem when changing, and the hanger bracket be suspended on by these equipment in frame is all generally special, a Multi-axis aircraft hanger bracket can not be shared, so in general can only carry a kind of specialized equipment by a hanger bracket between distinct device.
Summary of the invention
The utility model removes and installs the drawback of inconvenience for the hanger bracket of Multi-axis aircraft in prior art, a kind of hanger bracket on Multi-axis aircraft is provided, the C shape that this hanger bracket comprises on horizontal connecting plate, two, left and right suspension arm and suspension arm grabs folder, use the utility model only need install two round bars parallel to each other in advance on Multi-axis aircraft, then this hanger bracket is by two C shape bluff piece pawls on two round bars, and installing/dismounting is very convenient.
Goal of the invention of the present utility model is achieved through the following technical solutions: a kind of hanger bracket on Multi-axis aircraft, comprises horizontal connecting plate, is provided with two connecting pins, is provided with installation screw bottom connecting pin below horizontal connecting plate; The two ends of horizontal connecting plate are respectively equipped with one and are inclined upwardly and the suspension arm extended laterally, and the angle of inclination of suspension arm is 30-75 °, and suspension arm upper end is provided with a C shape and grabs folder, and the opening that C shape grabs folder is arranged towards the both sides of hanger bracket.
When using the utility model, needs first arrange two round bars parallel to each other in advance bottom the frame of Multi-axis aircraft, round bar external diameter and C shape grab that to press from both sides internal diameter identical, distance between two round bars is equal with the distance that two C shapes are grabbed between folder, this hanger bracket grabs the direct pawl of folder on two round bars by two C shapes, install very convenient, and first-class function device of making a video recording is arranged on hanger bracket by installation screw, different function devices can be connected by installation screw, as these function devices can first be arranged on one block of plate, then this block plate is connected with installation screw, so just different function devices can be installed.
As preferably, described suspension arm is provided with the bar shaped groove running through suspension arm both sides, and the direction of bar shaped groove is consistent with the direction of suspension arm.Suspension arm arranges bar shaped groove, what decrease manufacture suspension arm uses material, the weight of integral hanging frame can be alleviated, and by the consistent setting in the direction of bar shaped groove and the direction of suspension arm, the Impact direction of i.e. suspension arm also has stressed structure, the setting of bar shaped groove, does not affect again its stress performance while alleviating hanger bracket weight, it is very reasonable to design.
As preferably, described installation screw is communicated with bar shaped groove.
As preferably, described suspension arm is also provided with through hole, and through hole is positioned at directly over installation screw, and through hole is communicated with bar shaped groove.Installation screw is used to the function devices such as installation pick up camera, and these equipment are bolted on hanger bracket, when selected bolt is long, bolt top is just likely pushed up on the cell wall of bar shaped groove, thus these function devices are installed built on the sand, and this is unallowable, and the through hole arranged well avoids this problem, the long part of bolt can insert through hole, ensure that bolt can screw, thus it is firm that function device is installed.
Compared with prior art, the utility model has following beneficial effect: hanging scaffold structure of the present utility model is simple, lightweight, the function device that can bear constant weight is installed, hanger bracket of the present utility model can multiplely use together, installing/dismounting is also very convenient, and Multi-axis aircraft is applicable to the installation of plurality of devices.
Accompanying drawing explanation
Fig. 1 is the utility model front view;
Fig. 2 is the utility model upward view;
Fig. 3 is the utility model block diagram;
Fig. 4 is the utility model using state figure;
Mark in figure: 1, horizontal connecting plate, 2, connecting pin, 3, installation screw, 4, suspension arm, 5, C shape grabs folder, 6, bar shaped groove, 7, through hole, 8, round bar, 9, function device.
Detailed description of the invention
Below in conjunction with the embodiment represented by accompanying drawing 1-4, the utility model is further described:
Embodiment 1
As Figure 1-4, a kind of hanger bracket on Multi-axis aircraft, comprises horizontal connecting plate 1, is provided with two connecting pins 2, is provided with installation screw 3 bottom connecting pin 2 below horizontal connecting plate 1; The two ends of horizontal connecting plate 1 are respectively equipped with one and are inclined upwardly and the suspension arm 4 extended laterally, and the angle of inclination of suspension arm 4 is 60 °, and suspension arm 4 upper end is provided with a C shape and grabs opening that folder 5, C shape grabs folder 5 and arrange towards the both sides of hanger bracket.Described suspension arm 4 is also provided with and runs through suspension arm 4 both sides and the bar shaped groove 6 of horizontally set, the direction of bar shaped groove 6 is consistent with the direction of suspension arm 4.Suspension arm 4 arranges bar shaped groove 6, what decrease manufacture suspension arm 4 uses material, the weight of integral hanging frame can be alleviated, and by setting consistent with the direction of suspension arm 4 for the direction of bar shaped groove 6, the Impact direction of i.e. suspension arm 4 also has stressed structure, the setting of bar shaped groove 6, does not affect again its stress performance while alleviating hanger bracket weight, it is very reasonable to design; Described installation screw 3 is communicated with bar shaped groove 6; Described suspension arm 4 is also vertically provided with through hole 7, and through hole 7 is positioned at directly over installation screw 3, and through hole 7 is communicated with bar shaped groove 6.Installation screw 3 is used to the equipment such as installation pick up camera, and these equipment are bolted on hanger bracket, when selected bolt is long, bolt top is just likely pushed up on the cell wall of bar shaped groove 6, thus these equipment is installed built on the sand, and this is unallowable, and the through hole 7 arranged well avoids this problem, the long part of bolt can insert through hole 7, ensure that bolt can screw, thus it is firm that equipment is installed.
As shown in Figure 4, when using the utility model, needs first arrange two round bars 8 parallel to each other in advance bottom the frame of Multi-axis aircraft, it is identical that round bar 8 external diameter and C shape grab folder 5 internal diameter, distance between two round bars 8 is equal with the distance that two C shapes are grabbed between folder 5, this hanger bracket grabs the direct pawl of folder 5 on two round bars 8 by two C shapes, install very convenient, and the function devices such as pick up camera 9 are arranged on two hanger brackets by installation screw 3, different function devices can be connected by installation screw 3, as these function devices can first be arranged on one block of plate, then this block plate is connected with installation screw 3, so just different function devices can be installed.
Specific embodiment described in literary composition is only to the explanation for example of the utility model spirit.The utility model person of ordinary skill in the field can make various amendment or supplements or adopt similar mode to substitute to described specific embodiment, but can't depart from spirit of the present utility model or surmount the scope that appended claims defines.
Claims (4)
1. the hanger bracket on Multi-axis aircraft, comprises horizontal connecting plate (1), is provided with two connecting pins (2), is provided with installation screw (3) bottom connecting pin below horizontal connecting plate; The two ends of horizontal connecting plate are respectively equipped with one and are inclined upwardly and the suspension arm (4) extended laterally, and the angle of inclination of suspension arm is 30-75 °, and suspension arm upper end is provided with a C shape and grabs folder (5), and the opening that C shape grabs folder is arranged towards the both sides of hanger bracket.
2. a kind of hanger bracket on Multi-axis aircraft according to claim 1, is characterized in that, described suspension arm is provided with the bar shaped groove (6) running through suspension arm both sides, and the direction of bar shaped groove is consistent with the direction of suspension arm.
3. a kind of hanger bracket on Multi-axis aircraft according to claim 2, it is characterized in that, described installation screw is communicated with bar shaped groove.
4. a kind of hanger bracket on Multi-axis aircraft according to claim 3, is characterized in that, described suspension arm is also provided with through hole (7), through hole is positioned at directly over installation screw, and through hole is communicated with bar shaped groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520818414.5U CN205034350U (en) | 2015-10-22 | 2015-10-22 | A mounted frame for on multiaxis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520818414.5U CN205034350U (en) | 2015-10-22 | 2015-10-22 | A mounted frame for on multiaxis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205034350U true CN205034350U (en) | 2016-02-17 |
Family
ID=55293269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520818414.5U Expired - Fee Related CN205034350U (en) | 2015-10-22 | 2015-10-22 | A mounted frame for on multiaxis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205034350U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622389A (en) * | 2017-03-25 | 2018-10-09 | 周良勇 | A kind of multi-rotor unmanned aerial vehicle |
| CN113998131A (en) * | 2021-11-26 | 2022-02-01 | 昌河飞机工业（集团）有限责任公司 | Universal hanging rack for helicopter ventral |
-
2015
- 2015-10-22 CN CN201520818414.5U patent/CN205034350U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108622389A (en) * | 2017-03-25 | 2018-10-09 | 周良勇 | A kind of multi-rotor unmanned aerial vehicle |
| CN113998131A (en) * | 2021-11-26 | 2022-02-01 | 昌河飞机工业（集团）有限责任公司 | Universal hanging rack for helicopter ventral |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201125 Address after: No.29, Fuhou Road, Funan Economic Development Zone, Fuyang City, Anhui Province Patentee after: Anhui Zhitian Intelligent Technology Co.,Ltd. Address before: 321000, south wing, room 520, building 1111, Li Yu East Road, Jindong District, Zhejiang, Jinhua Patentee before: ZHEJIANG ZHITIAN TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160217 Termination date: 20211022 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |