CN112591075B - Airborne antenna folding transportation and fast-assembling locking mechanism and unmanned aerial vehicle - Google Patents
Airborne antenna folding transportation and fast-assembling locking mechanism and unmanned aerial vehicle Download PDFInfo
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- CN112591075B CN112591075B CN202110004412.2A CN202110004412A CN112591075B CN 112591075 B CN112591075 B CN 112591075B CN 202110004412 A CN202110004412 A CN 202110004412A CN 112591075 B CN112591075 B CN 112591075B
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- antenna
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The invention provides an airborne antenna folding, transporting and fast-assembling locking mechanism and an unmanned aerial vehicle, wherein the airborne antenna folding, transporting and fast-assembling locking mechanism comprises an antenna housing, an antenna tray, a fastening pin, a spring buckle and a hinge, the fastening pin is rotatably arranged on the antenna tray, the antenna is arranged in the antenna housing, the spring is arranged below the spring buckle in a cushioning mode, the spring can be slidably arranged in the fastening pin, and the antenna housing is connected with the antenna tray through the hinge.
Description
[ technical field ] A method for producing a semiconductor device
The invention relates to the technical field of unmanned aerial vehicles, in particular to a folding, transporting and fast-assembling locking mechanism for an airborne antenna and an unmanned aerial vehicle.
[ background of the invention ]
Antenna wide application in fixed wing unmanned aerial vehicle and unmanned helicopter, to relay antenna or other electron load antennas, antenna protrusion fuselage size is more, and conventional antenna and fuselage generally directly link firmly, and the dismouting is troublesome in the transportation, and this scheme has designed an antenna folding scheme, can realize the convenient dismouting of antenna no instrument, easy operation, and fixed locking is reliable.
Therefore, there is a need to develop an airborne antenna folding, transporting, and quick-assembling locking mechanism and an unmanned aerial vehicle to overcome the deficiencies of the prior art and to solve or alleviate one or more of the above problems.
[ summary of the invention ]
In view of the above, the invention provides an airborne antenna folding, transporting and fast-assembling locking mechanism and an unmanned aerial vehicle, wherein an antenna is fixed inside an antenna housing, the antenna housing and an antenna tray are connected through a hinge and locked through a fast-locking anti-loosening pin, the antenna housing can rotate around the tray, an antenna and the antenna housing can be folded in a transportation state, and the antenna housing and the antenna can be locked in a flight state.
On one hand, the folding, transporting and quickly-assembling locking mechanism for the airborne antenna comprises an antenna housing, an antenna tray, a fastening pin, a spring buckle and a hinge, wherein the fastening pin is rotatably arranged at the bottom of the antenna housing, the antenna is arranged in the antenna housing, a spring is arranged under the spring buckle in a cushioning mode, the spring is slidably arranged in the antenna tray, and the antenna housing is connected with the antenna tray through the hinge.
The above aspect and any possible implementation manner further provide an implementation manner that the antenna is fixed inside the radome, and the fixing manner of the antenna and the radome includes but is not limited to screwing.
The above aspects and any possible implementations further provide an implementation in which the fastening pins have at least three, and the fastening pins rotate 90 ° when locked in combination.
There is further provided in accordance with the above-described aspect and any one of the possible implementations, an implementation in which the spring catch is wedge-shaped.
The above aspects and any possible implementations further provide an implementation in which the antenna folding, transporting, and quick-assembly locking mechanism is not operated when in a closed, unlocked state.
The above aspects and any possible implementations further provide an implementation where the antenna folding, transporting, and quick-assembling locking mechanism is in an operating state when in a closed and locked state.
As in the aspect described above and any possible implementation manner, an unmanned aerial vehicle is further provided, which includes an antenna folding, transporting, and fast-assembling locking mechanism, a vehicle body, and a control unit, where the control unit is connected to a spring buckle, and the antenna folding, transporting, and fast-assembling locking mechanism is disposed on the vehicle body.
The above aspects and any possible implementation further provide an implementation in which the antenna housing is fixedly connected to the bottom of the machine body.
The above-described aspects and any possible implementations further provide an implementation in which the antenna folding, transporting, and fast-assembling locking mechanism is folded inside the body of the drone when in a closed, unlocked state.
As to the aspects and any possible implementation manners described above, an implementation manner is further provided, where the antenna folding transportation and fast-assembly locking mechanism is disengaged from the unmanned aerial vehicle body when in a closed and locked state.
Compared with the prior art, the invention can obtain the following technical effects: according to the mechanism, the antenna is fixed inside the antenna housing, the antenna housing and the antenna tray are connected through the hinge and locked through the quick-locking anti-loosening pin, the antenna housing can rotate around the tray, the antenna and the antenna housing can be folded in a transportation state, and the antenna housing and the antenna can be locked in a flying state.
Of course, it is not necessary for any one product in which the invention is practiced to achieve all of the above-described technical effects simultaneously.
[ description of the drawings ]
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 is an overall effect diagram of a foldable radome in a closed and unlocked state according to an embodiment of the present invention;
fig. 2 is an overall effect diagram of an open-state foldable radome provided by an embodiment of the present invention;
fig. 3 is a detailed view of a portion of a foldable radome in a closed and locked state according to an embodiment of the invention.
Wherein, antenna house 1, antenna 2, antenna tray 3, fastening pin 4, spring buckle 5, hinge 6.
[ detailed description ] A
For better understanding of the technical solutions of the present invention, the following detailed descriptions of the embodiments of the present invention are provided with reference to the accompanying drawings.
It should be understood that the described embodiments are only some embodiments of the invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The terminology used in the embodiments of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used in the examples of the present invention and the appended claims, the singular forms "a," "an," and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise.
The invention provides an airborne antenna folding, transporting and fast-assembling locking mechanism which comprises an antenna housing, an antenna tray, a fastening pin, a spring buckle and a hinge. The antenna is fixed inside the antenna housing, and the fixing mode of the antenna and the antenna housing comprises but not limited to screwing. The number of the fastening pins is at least three, and the fastening pins rotate by 90 degrees when being combined and locked. The spring buckle is a wedge-shaped body. The antenna folding, transporting and quick-assembling locking mechanism does not work when in a closed and unlocked state. The antenna folding, transporting and quick-assembling locking mechanism is in a working state when in a closed and locked state.
The utility model provides an unmanned aerial vehicle, includes folding transportation of antenna and fast-assembling locking mechanism, organism and the control unit, the control unit connects the spring buckle, folding transportation of antenna and fast-assembling locking mechanism set up on the organism. The antenna shell is fixedly connected to the bottom of the machine body. The antenna folding, transporting and quick-assembling locking mechanism is folded in the unmanned aerial vehicle body when in a closed and unlocked state. The antenna folding, transporting and quick-mounting locking mechanism is separated from the unmanned aerial vehicle body in a closed locking state.
According to the folding, transporting and fast-assembling locking mechanism for the airborne antenna, the antenna is fixed inside the antenna housing, the antenna housing and the antenna tray are connected through the hinge and locked through the fast-locking and anti-loosening pin, the antenna housing can rotate around the tray, the antenna and the antenna housing can be folded in a transportation state, and the antenna housing and the antenna can be locked in a flight state.
1. The foldable antenna housing device consists of an antenna housing 1, an antenna 2, an antenna tray 3, a fastening pin 4, a spring buckle 5 and a hinge 6;
2. the fastening pin 4 can rotate freely, and a spring is arranged below the spring buckle 5 and can slide up and down;
3. the antenna 2 can be fixed inside the antenna housing 1 in a fixing mode such as a screw joint mode, the antenna housing 1 and the antenna tray 3 are connected together through a hinge 6, the antenna housing 1 (containing the antenna 2) can rotate around the hinge 6, and the folding antenna housing in an opening state is shown in an overall effect diagram in figure 2;
4. the folding antenna housing combining and locking process comprises the following steps: the radome 1 (containing the antenna 2) rotates around the hinge 6 until the radome 1 is completely attached to the antenna tray 3 (as shown in fig. 1), at the moment, the radome rotates 3 fastening pins 4 by about 90 degrees respectively, in the process, the spring buckle 5 undergoes two processes of being pressed down and bouncing again, and finally self-locking is realized (the buckle is a wedge-shaped body), and the local details of the self-locking state are shown in fig. 3;
5. the unlocking and folding processes of the foldable antenna housing are as follows: meanwhile, the spring buckles 5 on two sides of one fastening pin 4 are pressed down, the fastening pin 4 is rotated by about 90 degrees, the fastening pin 4 is unlocked at the moment, the other two self-locking pins 4 are unlocked in the same mode, and finally the folding process of the foldable antenna housing is completed by rotating the wire housing 1.
The above folding transportation of airborne antenna and fast-assembling locking mechanism and unmanned aerial vehicle that provide to this application embodiment have carried out detailed introduction. The above description of the embodiments is only for the purpose of helping to understand the method of the present application and its core ideas; meanwhile, for a person skilled in the art, according to the idea of the present application, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present application.
As used in the specification and claims, certain terms are used to refer to particular components. As one skilled in the art will appreciate, manufacturers may refer to a component by different names. This specification and claims do not intend to distinguish between components that differ in name but not function. In the following description and in the claims, the terms "include" and "comprise" are used in an open-ended fashion, and thus should be interpreted to mean "include, but not limited to. "substantially" means within an acceptable error range, that a person skilled in the art can solve the technical problem within a certain error range to substantially achieve the technical effect. The following description is of the preferred embodiment for carrying out the present application, but is made for the purpose of illustrating the general principles of the application and is not to be taken in a limiting sense. The scope of the present application is to be construed in accordance with the substance defined by the following claims.
It is also noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a good or system that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such good or system. Without further limitation, an element defined by the phrase "comprising a … …" does not exclude the presence of another identical element in a good or system that comprises the element.
It should be understood that the term "and/or" as used herein is merely one type of association that describes an associated object, meaning that three relationships may exist, e.g., a and/or B may mean: a exists alone, A and B exist simultaneously, and B exists alone. In addition, the character "/" herein generally indicates that the former and latter related objects are in an "or" relationship.
The foregoing description shows and describes several preferred embodiments of the present application, but as aforementioned, it is to be understood that the application is not limited to the forms disclosed herein, but is not to be construed as excluding other embodiments and is capable of use in various other combinations, modifications, and environments and is capable of changes within the scope of the application as described herein, commensurate with the above teachings, or the skill or knowledge of the relevant art. And that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the application, which is to be protected by the claims appended hereto.
Claims (5)
1. The folding, transporting and quickly-assembling locking mechanism for the airborne antenna is characterized by comprising an antenna housing, an antenna tray, a fastening pin, a spring buckle and a hinge, wherein the fastening pin is rotatably arranged at the bottom of the antenna housing;
the antenna is fixed inside the antenna housing, the fixing modes of the antenna and the antenna housing include but are not limited to screw connection, at least three fastening pins are provided, and the fastening pins rotate for 90 degrees when being combined and locked; the antenna folding, transporting and quick-mounting locking mechanism is in a closed and unlocked state, and is in a working state.
2. An unmanned aerial vehicle, comprising the antenna folding, transporting and fast-assembling locking mechanism of claim 1, wherein the unmanned aerial vehicle further comprises a body and a control unit, the control unit is connected with the spring buckle, and the antenna folding, transporting and fast-assembling locking mechanism is arranged on the body.
3. The drone of claim 2, wherein the antenna housing is fixedly connected at a bottom of the airframe.
4. The drone of claim 3, wherein the antenna fold transport and quick lock mechanism is folded within the body of the drone when in a closed, unlocked state.
5. The drone of claim 4, wherein the antenna fold transport and quick lock mechanism disengages from the body of the drone when in the closed and locked state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110004412.2A CN112591075B (en) | 2021-01-04 | 2021-01-04 | Airborne antenna folding transportation and fast-assembling locking mechanism and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110004412.2A CN112591075B (en) | 2021-01-04 | 2021-01-04 | Airborne antenna folding transportation and fast-assembling locking mechanism and unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN112591075A CN112591075A (en) | 2021-04-02 |
| CN112591075B true CN112591075B (en) | 2023-03-07 |
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| CN202110004412.2A Active CN112591075B (en) | 2021-01-04 | 2021-01-04 | Airborne antenna folding transportation and fast-assembling locking mechanism and unmanned aerial vehicle |
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|---|---|---|---|---|
| CN201737105U (en) * | 2010-05-13 | 2011-02-09 | 庞明方 | Upper spanner semi-circle locking type folder |
| CN202997031U (en) * | 2012-11-05 | 2013-06-12 | 杨瑞雄 | Antenna foldable structure |
| CN105442960A (en) * | 2015-12-25 | 2016-03-30 | 海鹰航空通用装备有限责任公司 | Quick-locking device for hatch cover of unmanned aerial vehicle |
| CN206964311U (en) * | 2017-07-04 | 2018-02-06 | 衢州信辉塑料配件有限公司 | A kind of improved purse eye-splice of structure |
| CN108891618A (en) * | 2018-07-06 | 2018-11-27 | 西安爱生技术集团公司 | A kind of quick dispatch mechanism of unmanned plane antenna house |
| CN110190463A (en) * | 2019-06-18 | 2019-08-30 | 上海航天科工电器研究院有限公司 | A kind of cylindrical connector rotating quick lock in and unlock |
| CN209454978U (en) * | 2018-11-27 | 2019-10-01 | 昆山优尼电能运动科技有限公司 | A kind of unmanned plane aerial mounting structure and unmanned plane |
| CN209667027U (en) * | 2019-03-14 | 2019-11-22 | 博科丝特工业技术(江苏)有限公司 | A kind of plastic buckle for car belt limit |
| CN210576451U (en) * | 2019-12-07 | 2020-05-19 | 福州兴正达信息科技有限公司 | Mounting structure of antenna cover |
| CN210769733U (en) * | 2019-07-22 | 2020-06-16 | 青州耐威智能科技有限公司 | Quick-release lock |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3635815B1 (en) * | 2017-06-05 | 2022-06-01 | The Nordam Group LLC | Accessible radome assembly |
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2021
- 2021-01-04 CN CN202110004412.2A patent/CN112591075B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201737105U (en) * | 2010-05-13 | 2011-02-09 | 庞明方 | Upper spanner semi-circle locking type folder |
| CN202997031U (en) * | 2012-11-05 | 2013-06-12 | 杨瑞雄 | Antenna foldable structure |
| CN105442960A (en) * | 2015-12-25 | 2016-03-30 | 海鹰航空通用装备有限责任公司 | Quick-locking device for hatch cover of unmanned aerial vehicle |
| CN206964311U (en) * | 2017-07-04 | 2018-02-06 | 衢州信辉塑料配件有限公司 | A kind of improved purse eye-splice of structure |
| CN108891618A (en) * | 2018-07-06 | 2018-11-27 | 西安爱生技术集团公司 | A kind of quick dispatch mechanism of unmanned plane antenna house |
| CN209454978U (en) * | 2018-11-27 | 2019-10-01 | 昆山优尼电能运动科技有限公司 | A kind of unmanned plane aerial mounting structure and unmanned plane |
| CN209667027U (en) * | 2019-03-14 | 2019-11-22 | 博科丝特工业技术(江苏)有限公司 | A kind of plastic buckle for car belt limit |
| CN110190463A (en) * | 2019-06-18 | 2019-08-30 | 上海航天科工电器研究院有限公司 | A kind of cylindrical connector rotating quick lock in and unlock |
| CN210769733U (en) * | 2019-07-22 | 2020-06-16 | 青州耐威智能科技有限公司 | Quick-release lock |
| CN210576451U (en) * | 2019-12-07 | 2020-05-19 | 福州兴正达信息科技有限公司 | Mounting structure of antenna cover |
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| Publication number | Publication date |
|---|---|
| CN112591075A (en) | 2021-04-02 |
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