CN208412095U - A kind of first radome fairing of unmanned plane - Google Patents
A kind of first radome fairing of unmanned plane Download PDFInfo
- Publication number
- CN208412095U CN208412095U CN201820642878.9U CN201820642878U CN208412095U CN 208412095 U CN208412095 U CN 208412095U CN 201820642878 U CN201820642878 U CN 201820642878U CN 208412095 U CN208412095 U CN 208412095U
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- housing
- attachment base
- chassis
- unmanned plane
- threaded rod
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Abstract
The utility model discloses a kind of the first radome fairings of unmanned plane, including housing, mounting groove, positioning column, the first fastening bolt, attachment base, notch, mounting hole, chassis, the second fastening bolt, expansion rod, threaded rod and fastening nut.The beneficial effects of the utility model are: the top of housing is arc shape, make housing that there is preferable aesthetic effect, simultaneously during unmanned plane during flying, it can be used in adjusting air-flow, have the function of lowering resistance, housing is made of aluminum alloy materials, it can be while proof strength, also guarantee that weight will not be too heavy, rubber pad is equipped between attachment base and chassis, increase the frictional force between attachment base and chassis, the two directly contact is avoided to cause to wear simultaneously, elastic washer is cased on threaded rod, make the more fastening that fastening nut is connect with threaded rod, prevent the automatic Hui Song of fastening nut.
Description
Technical field
The utility model relates to a kind of radome fairing, the first radome fairing of specially a kind of unmanned plane belongs to unmanned plane and matches
Part technical field.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, Huo Zheyou
Car-mounted computer fully or intermittently automatically operates, at present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, calamity
Hardly possible rescue, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture are romantic
Etc. field application, greatly expanded the purposes of unmanned plane itself, and radome fairing is the essential accessory of unmanned plane, it is whole
Stream cover is just installed in aircraft front end, cover on the conical objects on paddle and engine, as the term suggests be for adjusting air-flow, can
To lower resistance, the equipment for protecting the inside also functions to beautiful effect, and existing radome fairing is carbon fiber or nylon material mostly,
It is economical and practical, it is at low cost, it is easy to reequip, but intensity difference, is easily damaged, and assembling is more troublesome, and is unfavorable for carrying out replacement group
Dress, two ends for connecting blade are arranged on the outside of radome fairing, during unmanned plane during flying, are easy to bring biggish resistance.
Utility model content
The purpose of this utility model is that solve the above-mentioned problems and provides a kind of the first radome fairing of unmanned plane.
The utility model achieves the above object through the following technical schemes: a kind of the first radome fairing of unmanned plane, packet
Include housing, mounting groove, positioning column, the first fastening bolt, attachment base, notch, mounting hole, chassis, the second fastening bolt, expansion
Bar, threaded rod and fastening nut；The housing is located at the upper end of the radome fairing, and the housing is in coniform, the side of the housing
Side is equipped with mounting groove, and the mounting groove is located at the two sides of housing, and one end of the positioning column is connected on chassis, described fixed
The other end of position column is located at the lower section of mounting groove, the positioning column and mounting groove in one-to-one correspondence placement, the first fastening spiral shell
Bolt is connected between mounting groove and positioning column, and first fastening bolt is located at the two sides of housing, the attachment base setting
In housing, the attachment base is placed in chassis upper surface, and the both ends of the attachment base offer notch, in the attachment base
Mounting hole is offered at the heart, the chassis is fixed together by the second fastening bolt with attachment base, second fastening bolt
It being made of expansion rod and threaded rod, the expansion rod is located at the lower end of threaded rod, and the expansion rod is arranged at the center on chassis,
The mounting hole that the threaded rod passes through attachment base is attached with fastening nut.
Preferably, in order to be used to adjust air-flow, have the function of lowering resistance, the top of the housing is arc
Shape.
Preferably, in order to while proof strength, also guarantee that weight will not be too heavy, the housing uses aluminium alloy material
Material is made.
Preferably, in order to increase the frictional force between attachment base and chassis, rubber is equipped between the attachment base and chassis
Pad.
Preferably, the automatic Hui Song of fastening nut in order to prevent is cased with elastic washer on the threaded rod.
The beneficial effects of the utility model are: the first cowling design of the unmanned plane is reasonable, the top of housing is arc
Shape makes housing have preferable aesthetic effect, while during unmanned plane during flying, can be used in adjusting air-flow, has and subtract
The effect of lower resistance, housing are made of aluminum alloy materials, can also guarantee that weight will not be too heavy, even while proof strength
It is equipped with rubber pad between joint chair and chassis, increases the frictional force between attachment base and chassis, while the two directly contact being avoided to make
At abrasion, it is cased with elastic washer on threaded rod, the more fastening for connecting fastening nut with threaded rod prevents fastening nut automatic
Hui Song.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model structure mounting base schematic diagram；
Fig. 3 is the second fastening bolt of the utility model structure schematic diagram；
In figure: 1, housing, 2, mounting groove, 3, positioning column, the 4, first fastening bolt, 5, attachment base, 6, notch, 7, installation
Hole, 8, chassis, the 9, second fastening bolt, 10, expansion rod, 11, threaded rod and 12, fastening nut.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1~3, a kind of first radome fairing of unmanned plane, including housing 1, mounting groove 2, positioning column 3, first
Fastening bolt 4, attachment base 5, notch 6, mounting hole 7, chassis 8, the second fastening bolt 9, expansion rod 10, threaded rod 11 and fastening spiral shell
Mother 12；The housing 1 is located at the upper end of the radome fairing, and for the housing 1 in coniform, the side of the housing 1 is equipped with mounting groove
2, the mounting groove 2 is located at the two sides of housing 1, and one end of the positioning column 3 is connected on chassis 8, the positioning column 3
The other end is located at the lower section of mounting groove 2, and the positioning column 3 is with mounting groove 2 in one-to-one correspondence placement, first fastening bolt 4
It is connected between mounting groove 2 and positioning column 3, first fastening bolt 4 is located at the two sides of housing 1, and the attachment base 5 is set
It sets in housing 1, the attachment base 5 is placed in 8 upper surface of chassis, and the both ends of the attachment base 5 offer notch 6, the company
Mounting hole 7 is offered at the center of joint chair 5, the chassis 8 is fixed together by the second fastening bolt 9 with attachment base 5, described
Second fastening bolt 9 is made of expansion rod 10 and threaded rod 11, and the expansion rod 10 is located at the lower end of threaded rod 11, the expansion
Bar 10 is arranged at the center on chassis 8, and the mounting hole 7 that the threaded rod 11 passes through attachment base 5 is attached with fastening nut 12,
The top of the housing 1 is arc shape, so that housing 1 is had preferable aesthetic effect, while during unmanned plane during flying, can
For adjusting air-flow, have the function of lowering resistance, the housing 1 is made of aluminum alloy materials, can be in the same of proof strength
When, also guarantee that weight will not be too heavy, is equipped with rubber pad between the attachment base 5 and chassis 8, increases between attachment base 5 and chassis 8
Frictional force, while directly contact both being avoided to cause to wear, is cased with elastic washer on the threaded rod 11, makes fastening nut 12
The more fastening connecting with threaded rod 11 prevents the automatic Hui Song of fastening nut 12.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of the first radome fairing of unmanned plane, it is characterised in that: including housing (1), mounting groove (2), positioning column (3),
One fastening bolt (4), attachment base (5), notch (6), mounting hole (7), chassis (8), the second fastening bolt (9), expansion rod (10),
Threaded rod (11) and fastening nut (12)；The housing (1) is located at the upper end of the radome fairing, and the housing (1) is in coniform, institute
The side for stating housing (1) is equipped with mounting groove (2), and the mounting groove (2) is located at the two sides of housing (1), the positioning column (3)
One end be connected on chassis (8), the other end of the positioning column (3) is located at the lower section of mounting groove (2), the positioning column (3)
It is connected between mounting groove (2) and positioning column (3) with mounting groove (2) in placement, first fastening bolt (4) is corresponded,
First fastening bolt (4) is located at the two sides of housing (1), and attachment base (5) setting is in housing (1), the company
Joint chair (5) is placed in chassis (8) upper surface, and the both ends of the attachment base (5) offer notch (6), in the attachment base (5)
It is offered at the heart mounting hole (7), the chassis (8) is fixed together by the second fastening bolt (9) with attachment base (5), described
Second fastening bolt (9) is made of expansion rod (10) and threaded rod (11), and the expansion rod (10) is located under threaded rod (11)
End, the expansion rod (10) are arranged at the center of chassis (8), and the threaded rod (11) passes through the mounting hole (7) of attachment base (5)
It is attached with fastening nut (12).
2. a kind of the first radome fairing of unmanned plane according to claim 1, it is characterised in that: the top of the housing (1)
End is arc shape.
3. a kind of the first radome fairing of unmanned plane according to claim 1, it is characterised in that: the housing (1) uses
Aluminum alloy materials are made.
4. a kind of the first radome fairing of unmanned plane according to claim 1, it is characterised in that: the attachment base (5) with
Rubber pad is equipped between chassis (8).
5. a kind of the first radome fairing of unmanned plane according to claim 1, it is characterised in that: on the threaded rod (11)
It is cased with elastic cushion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820642878.9U CN208412095U (en) | 2018-05-02 | 2018-05-02 | A kind of first radome fairing of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820642878.9U CN208412095U (en) | 2018-05-02 | 2018-05-02 | A kind of first radome fairing of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208412095U true CN208412095U (en) | 2019-01-22 |
Family
ID=65117691
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820642878.9U Expired - Fee Related CN208412095U (en) | 2018-05-02 | 2018-05-02 | A kind of first radome fairing of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208412095U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110676799A (en) * | 2019-08-27 | 2020-01-10 | 江西洪都航空工业集团有限责任公司 | Sealing structure of cabin section cable fairing |
| CN112415612A (en) * | 2020-10-30 | 2021-02-26 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetic probe rod |
| CN114516271A (en) * | 2022-02-22 | 2022-05-20 | 黑龙江工程学院 | New energy automobile power electronic converter high-voltage control case |
-
2018
- 2018-05-02 CN CN201820642878.9U patent/CN208412095U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110676799A (en) * | 2019-08-27 | 2020-01-10 | 江西洪都航空工业集团有限责任公司 | Sealing structure of cabin section cable fairing |
| CN112415612A (en) * | 2020-10-30 | 2021-02-26 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetic probe rod |
| CN112415612B (en) * | 2020-10-30 | 2024-05-24 | 哈尔滨飞机工业集团有限责任公司 | Helicopter cantilever magnetism probe rod |
| CN114516271A (en) * | 2022-02-22 | 2022-05-20 | 黑龙江工程学院 | New energy automobile power electronic converter high-voltage control case |
| CN114516271B (en) * | 2022-02-22 | 2023-11-28 | 黑龙江工程学院 | High-voltage control box of new energy automobile power electronic converter |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190122 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |