CN203507533U - Detachable aircraft protective cage - Google Patents
Detachable aircraft protective cage Download PDFInfo
- Publication number
- CN203507533U CN203507533U CN201320624938.1U CN201320624938U CN203507533U CN 203507533 U CN203507533 U CN 203507533U CN 201320624938 U CN201320624938 U CN 201320624938U CN 203507533 U CN203507533 U CN 203507533U
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- aircraft
- detachable
- cover bodies
- circle body
- cover
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Abstract
The utility model discloses a detachable aircraft protective cage. The detachable aircraft protective cage comprises a detachable installing rod, two cover bodies and a plurality of connecting rods. The two cover bodies are oppositely arranged at intervals, the detachable installing rod is located between the two cover bodies and detachably connected with the two cover bodies, and the connecting rods are evenly distributed between the two cover bodies and detachably connected with the two cover bodies. The detachable aircraft protective cage is ingenious and reasonable in structural design, an aircraft can be effectively prevented from dropping and being broken, when the aircraft flies under remote control, screw propellers in a high speed revolution state can be effectively prevented from being damaged, and people or objects can be effectively prevented from being hurt by the screw propellers, and therefore the safety performance is high; the aircraft can crawl on a ceiling and walls, more pleasure is provided for players, and interestingness and playability are greatly improved; in addition, due to the fact that detachable structure connection is adopted, assembly is more easily and more conveniently conducted, the playing requirements of beginners are met, when the beginners are familiar with the aircraft, the protective cage can be detached, and therefore different playing requirements are met, and the application range is wide.
Description
Technical field
The utility model relates to toy technique field, is specifically related to a kind of detachable aircraft protection cage.
Background technology
Toy aircraft is a kind of toy that children and numerous airplane hobbyists like, by wireless control system, aircraft is sent to instruction to realize the landing of aircraft, acceleration and deceleration and direction control etc.
At present; in many toy aircraft due to safety guard not being set; make the screw of toy aircraft High Rotation Speed when shaking control flight often hurt people; also be prone to and damage screw or break toy aircraft phenomenon; when serious, even cause casualty accident; cause its poor stability, recreational low, also lack corresponding enjoyment.
Utility model content
For above-mentioned deficiency, the purpose of this utility model is, provides a kind of structural design ingenious, reasonable, and security is good, can effectively not protect aircraft and its screw damaged and avoid occurring that screw hurts the detachable aircraft protection cage of people or thing.
For achieving the above object, technical scheme provided by the utility model is:
A kind of detachable aircraft protection cage; it comprises that one is used for arranging detachable mounting rod, two cover bodies and some connecting rods of aircraft; two cover body intervals are oppositely arranged; detachable mounting rod is located between two cover bodies; and two ends are plugged on respectively on the center of cover body of nearly one side; described connecting rod is evenly distributed between two cover bodies according to the periphery trend of cover body, and the two ends of this connecting rod removably connect with the marginal position of the cover body of nearly one side respectively.
As a kind of improvement of the present utility model, described cover body comprises large circle body and little circle body, this little circle body and described large circle body concentric arrange, and be positioned at a side position of this large circle body, the outer wall of this little circle body is evenly provided with many greatly radially linking arms that are connected with described large circle body, the home position of described little circle body is provided with an installation portion, the outer wall of this installation portion is evenly provided with many paths that are connected with described little circle body to linking arm, and this installation portion is provided with the inserting hole suitable with described detachable mounting rod.
As a kind of improvement of the present utility model, the described large radially quantity of linking arm is six, and it is the center of circle and is arranged on symmetrically and evenly on described little circle body.
As a kind of improvement of the present utility model, described path is six to the quantity of linking arm, and it is the center of circle and is arranged on symmetrically and evenly on described installation portion.
As a kind of improvement of the present utility model, described connecting rod quantity is six.
As a kind of improvement of the present utility model, the two ends of described connecting rod are provided with an elastic force claw, and are provided with the hole clipping suitable with this elastic force claw at the marginal position of described cover body.
As a kind of improvement of the present utility model, described aircraft is quadrotor, and this quadrotor comprises a fuselage and four rotor arms that are arranged on this fuselage, and described fuselage is arranged on described detachable mounting rod.
The beneficial effects of the utility model are: the utility model structural design is ingenious, rationally, two cover bodies and connecting rod removably connect, forming one can be by the protection cage of the cage body shape completely aircraft being covered, aircraft is arranged in this protection cage by detachable mounting rod, can effectively prevent that aircraft from being broken and making aircraft not damaged and avoid occurring that screw hurts the phenomenon of people or thing at the screw that shakes when flight control High Rotation Speed, security performance is high, allow player damage aircraft or its screw and to hurt people or thing without considering, greatly enriched playing method, can on ceiling and wall, creep, for player provides more enjoyment, interest and playability have greatly been strengthened, avoid player to produce sensation dry as dust, overall structure is simple in addition, compact, parts are few, employing demountable structure connects, make assembling more simple and convenient, fit on, meet beginner's the demand of playing, when playing certain familiarity, the utility model can be unloaded, meet the different demands of playing, applied widely, be beneficial to extensive popularization.
Below in conjunction with accompanying drawing and embodiment, the utility model is further illustrated.
Accompanying drawing explanation
Fig. 1 is perspective view of the present utility model.
Fig. 2 is the decomposition texture schematic diagram of Fig. 1.
Fig. 3 is the structure enlarged diagram of local A in Fig. 2.
Structural representation when Fig. 4 is assembling of the present utility model.
Structural representation when Fig. 5 is the utility model use.
The specific embodiment
Referring to Fig. 1 to Fig. 5; a kind of detachable aircraft protection cage that the present embodiment provides; it comprises that one is used for arranging detachable mounting rod 1, two cover bodies 2 and some connecting rods 3 of aircraft 4; two cover body 2 intervals are oppositely arranged; detachable mounting rod 1 is located between two cover bodies 2; and two ends are plugged on respectively on the center of cover body 2 of nearly one side; described connecting rod 3 is evenly distributed between two cover bodies 2 according to the periphery trend of cover body 2, and the two ends of this connecting rod 3 removably connect with the marginal position of the cover body 2 of nearly one side respectively.
Described cover body 2 comprises large circle body 21 and ringlet body 22, this ringlet body 22 and described large circle body 21 concentric settings, and be positioned at a side position of this large circle body 21, the outer wall of this ringlet body 22 is evenly provided with many greatly radially linking arms 23 that are connected with described large circle body 21, the home position of described ringlet body 22 is provided with an installation portion 24, the outer wall of this installation portion 24 is evenly provided with many paths that are connected with described ringlet body 22 to linking arm 25, and this installation portion 24 is provided with the inserting hole 26 suitable with described detachable mounting rod 1.
In the present embodiment, the described large radially quantity of linking arm 23 is preferably six, and it is the center of circle and is arranged on symmetrically and evenly on described ringlet body 22.Described path is preferably six to the quantity of linking arm 25, and it is the center of circle and is arranged on symmetrically and evenly on described installation portion 24.Described connecting rod 3 quantity are preferably six.Guaranteeing enough to protect on the basis of intensity, reduce material cost, and handsome in appearance.In other embodiment, can come the large radially linking arm 23 of respective settings, path to the quantity of linking arm 25 and connecting rod 3 according to required protection intensity effect or modeling effect, as four, five, eight etc.
Referring to Fig. 2 and Fig. 3, the two ends of described connecting rod 3 are provided with an elastic force claw 31, and are provided with the hole clipping 27 suitable with this elastic force claw 31 at the marginal position of described cover body 2.Elastic force claw 31 is directly inserted to the assembling that hole clipping 27 can complete connecting rod 3 and cover body 2, be connected firmly, structural stability is good, effectively promotes impact resistance, and easy accessibility, quick.
In the present embodiment, described aircraft 4 is preferably quadrotor, and this quadrotor comprises a fuselage 41 and four rotor arms 42 that are arranged on this fuselage 41, and described fuselage 41 is arranged on described detachable mounting rod 1.In other embodiment, described in this, aircraft 4 can be also toy helicopter, and this toy helicopter comprises fuselage and is arranged on the rotor on this fuselage, then this fuselage is arranged on to described detachable mounting rod 1.
While needing to use, referring to Fig. 4, in advance detachable mounting rod 1 is arranged on the fuselage 41 of aircraft 4, then one end of detachable mounting rod 1 is plugged in the inserting hole 26 of installation portion 24 of cover body 2 on right side, then one by one the elastic force claw 31 on connecting rod 3 one end is connect and put in the hole clipping 27 of the cover body 2 on right side, then the inserting hole 26 on the cover body 2 on the left of making is aimed at the other end of detachable mounting rod 1 and the elastic force claw 31 that hole clipping 27 is aimed on connecting rod 3 other ends, and make corresponding insertion assembling, realize whole assembling process.
While playing, referring to Fig. 5, owing to removably connecting with connecting rod 3 by two cover bodies 2, forming one can be by the protection cage of the cage body shape completely aircraft 4 being covered, aircraft 4 is arranged in this protection cage by detachable mounting rod 1, can effectively prevent that aircraft 4 from being broken and making aircraft 4 not damaged and avoid occurring that screw hurts the phenomenon of people or thing at the screw that shakes when flight control High Rotation Speed, security performance is high, allow player damage aircraft 4 or its screw and to hurt people or thing without considering, greatly enriched playing method, can on ceiling and wall, creep, for player provides more enjoyment, interest and playability have greatly been strengthened, avoid player to produce sensation dry as dust.
In addition, owing to adopting demountable structure to connect, make assembling more simple and convenient.When player is played certain familiarity, also two cover bodies 2 can be pulled open, two cover bodies 2 and detachable mounting rod 1, connecting rod 3 are separated, there is detachable function, meet the different demands of playing, be also easy to carry and store.
The announcement of book and instruction according to the above description, the utility model those skilled in the art can also change and revise above-mentioned embodiment.Therefore, the utility model is not limited to the specific embodiment disclosed and described above, to modifications and changes more of the present utility model, also should fall in the protection domain of claim of the present utility model.In addition,, although used some specific terms in this description, these terms just for convenience of description, do not form any restriction to the utility model.As described in the utility model above-described embodiment, adopt structure same or analogous with it and other protective device of obtaining, all in the utility model protection domain.
Claims (7)
1. a detachable aircraft is protected cage; it is characterized in that; it comprises that one is used for arranging detachable mounting rod, two cover bodies and some connecting rods of aircraft; two cover body intervals are oppositely arranged; detachable mounting rod is located between two cover bodies; and two ends are plugged on respectively on the center of cover body of nearly one side, described connecting rod is evenly distributed between two cover bodies according to the periphery trend of cover body, and the two ends of this connecting rod removably connect with the marginal position of the cover body of nearly one side respectively.
2. detachable aircraft according to claim 1 is protected cage; it is characterized in that: described cover body comprises large circle body and little circle body; this little circle body and described large circle body concentric arrange; and be positioned at a side position of this large circle body; the outer wall of this little circle body is evenly provided with many greatly radially linking arms that are connected with described large circle body; the home position of described little circle body is provided with an installation portion; the outer wall of this installation portion is evenly provided with many paths that are connected with described little circle body to linking arm, and this installation portion is provided with the inserting hole suitable with described detachable mounting rod.
3. detachable aircraft protection cage according to claim 2, is characterized in that: the described large radially quantity of linking arm is six, and it is the center of circle and is arranged on symmetrically and evenly on described little circle body.
4. detachable aircraft protection cage according to claim 2, is characterized in that: described path is six to the quantity of linking arm, and it is the center of circle and is arranged on symmetrically and evenly on described installation portion.
5. detachable aircraft protection cage according to claim 2, is characterized in that: described connecting rod quantity is six.
6. detachable aircraft protection cage according to claim 1, is characterized in that: the two ends of described connecting rod are provided with an elastic force claw, and is provided with the hole clipping suitable with this elastic force claw at the marginal position of described cover body.
7. detachable aircraft according to claim 1 is protected cage; it is characterized in that: described aircraft is quadrotor; this quadrotor comprises a fuselage and four rotor arms that are arranged on this fuselage, and described fuselage is arranged on described detachable mounting rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320624938.1U CN203507533U (en) | 2013-10-11 | 2013-10-11 | Detachable aircraft protective cage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320624938.1U CN203507533U (en) | 2013-10-11 | 2013-10-11 | Detachable aircraft protective cage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203507533U true CN203507533U (en) | 2014-04-02 |
Family
ID=50366519
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320624938.1U Expired - Fee Related CN203507533U (en) | 2013-10-11 | 2013-10-11 | Detachable aircraft protective cage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203507533U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN104787325A (en) * | 2015-04-21 | 2015-07-22 | 中国科学院合肥物质科学研究院 | Supporting and protection mechanism of four-rotor robot |
| CN105599911A (en) * | 2016-02-03 | 2016-05-25 | 深圳市哈博森科技有限公司 | Minitype four-axis protection wheel of unmanned aerial vehicle |
| JP2017039334A (en) * | 2015-08-17 | 2017-02-23 | 富士通株式会社 | Frame structure for flying machine, flying machine and method for using flying machine |
| FR3069447A1 (en) * | 2017-07-25 | 2019-02-01 | Eric Liegeois | DEVICE FOR RETURNING TO THE POSITION OF TAKING A DRONE AFTER CRASH WITHOUT EXTERNAL INTERVENTION. |
-
2013
- 2013-10-11 CN CN201320624938.1U patent/CN203507533U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN104787325A (en) * | 2015-04-21 | 2015-07-22 | 中国科学院合肥物质科学研究院 | Supporting and protection mechanism of four-rotor robot |
| JP2017039334A (en) * | 2015-08-17 | 2017-02-23 | 富士通株式会社 | Frame structure for flying machine, flying machine and method for using flying machine |
| CN105599911A (en) * | 2016-02-03 | 2016-05-25 | 深圳市哈博森科技有限公司 | Minitype four-axis protection wheel of unmanned aerial vehicle |
| FR3069447A1 (en) * | 2017-07-25 | 2019-02-01 | Eric Liegeois | DEVICE FOR RETURNING TO THE POSITION OF TAKING A DRONE AFTER CRASH WITHOUT EXTERNAL INTERVENTION. |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: Chen Zeguang Document name: Notification to Pay the Fees |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140402 Termination date: 20161011 |