CN203727648U - Unmanned annunciator - Google Patents
Unmanned annunciator Download PDFInfo
- Publication number
- CN203727648U CN203727648U CN201320825977.8U CN201320825977U CN203727648U CN 203727648 U CN203727648 U CN 203727648U CN 201320825977 U CN201320825977 U CN 201320825977U CN 203727648 U CN203727648 U CN 203727648U
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- China
- Prior art keywords
- compartment
- annunciator
- unmanned
- signal according
- unmanned signal
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Abstract
The utility model discloses an unmanned annunciator, which comprises an annunciator body, wings, and a spoiler, wherein the wings are connected with the annunciator through first bolts, the spoiler is connected with the annunciator body through a second bolt, the annunciator sequentially comprises an equipment compartment, a battery compartment, fuel compartment, a parachute compartment and a power compartment from front to back, a load compartment is further arranged below the parachute compartment, and relay equipment is arranged in the load compartment. The unmanned annunciator has the characteristics of being convenient to carry, simple to maintain and use, low in cost, capable of being repeatedly used, long in high altitude long endurance and the like, has stronger advantages on the aspect of a signal communication relay, is large in effective load, can hang high-end signal relay equipment and realize the relay function of overhead signals, and also has stronger advantages on the aspect of testing down-hung type task load experiment carrying equipment, thus being easy to popularize and apply.
Description
Technical field
The utility model relates to a kind of unmanned signal.
Background technology
Traditional signal is generally by manually manipulating.The structure of the signal of manual control is comparatively complicated, carries comparatively difficulty, and productive costs is high, short when boat.
Utility model content
The purpose of this utility model is to provide a kind of unmanned signal, with one or more in addressing the above problem.
The utility model discloses a kind of unmanned signal, it comprises fuselage, is connected to the wing on described fuselage and is connected to the empennage on described fuselage by the second latch by the first latch, described fuselage comprises equipment compartment, battery flat, fuel oil tank, umbrella cabin and piggyback pod from front to back successively, the below in described umbrella cabin is also provided with load cabin, and described load is provided with trunking in cabin.
Preferably, in described equipment compartment, be provided with autopilot.
Preferably, in described battery flat, be provided with the battery for electric power is provided.
Preferably, in described umbrella cabin, be provided with parachute.
Preferably, in described piggyback pod, be provided with driving engine.
Preferably, described trunking is relay.
Preferably, described empennage comprises shoe, is vertically connected at the vertical fin of described shoe and is vertically connected at the horizontal tail of described vertical fin.
Preferably, the front end of described equipment compartment is provided with pitot.
Preferably, in described fuel oil tank, store fuel.
The utlity model has easy to carry, safeguard use simple, cost is low, reusable, the feature such as when long boat, aspect signal and communication relaying, there is stronger advantage, this unmanned signal capacity weight is large, can carry high-side signal trunking, realize aerial signal relay function, lower hanging mission payload experiment carrying equipment test aspect has stronger advantage, is easy to apply.
Brief description of the drawings
Fig. 1 shows unmanned signal of the present utility model.
In accompanying drawing: 1, pitot; 2, equipment compartment; 3, battery flat; 4, fuel oil tank; 5, umbrella cabin; 6, piggyback pod; 7, shoe; 8, vertical fin; 9, horizontal tail; 10, load cabin; 11, wheel; 12, alighting gear; 13, wing.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, thereby so that advantage of the present utility model and feature can be easier to be those skilled in the art will recognize that, protection domain of the present utility model is made to more explicit defining.
In the first embodiment of the present utility model, shown in Fig. 1, unmanned signal, comprises fuselage, is connected to the wing 13 on described fuselage and is connected to the empennage on described fuselage by the second latch by the first latch.Empennage can comprise shoe 7, be vertically connected at the vertical fin 8 of described shoe 7 and be vertically connected at the horizontal tail 9 of described vertical fin 8.After wing 13 or empennage and fuselage are separated, the size of this unmanned signal is reduced to minimum, thereby unmanned signal is now easy to carry.Whole unmanned signal adopts modular design, and interface is type quick detaching, and more exchange device is very convenient.
Fuselage comprises equipment compartment 2, battery flat 3, fuel oil tank 4, umbrella cabin 5 and piggyback pod 6 from front to back successively, and the below in described umbrella cabin 5 is also provided with load cabin 10, in described load cabin 10, is provided with trunking.Trunking is the middle instrument and equipment adding in the time that the isomorphism network segment with same-interface and same media access-control protocol is interconnected, and it can amplify and can retransmit the signal of transmission.Thereby can avoid because of the long signal attenuation producing of network segment cable line, and then effectively improve the reliability of transmission.In the present embodiment, trunking can be relay.In the time that the isomorphism network segment with same-interface and same media access-control protocol is interconnected, the instrument and equipment that centre adds, it can amplify and can retransmit the signal of transmission.Thereby can avoid because of the long signal attenuation producing of network segment cable line, and then effectively improve the reliability of transmission.
In equipment compartment 2, be provided with autopilot.In battery flat 3, be provided with the battery for electric power is provided.This battery can improve the cruise duration of unmanned signal.In umbrella cabin 5, be provided with parachute.Complete machine intensity is high, has parachute buffering, has guaranteed aircraft safety landing, so can repeated usage.In piggyback pod 6, be provided with driving engine, for providing power to this unmanned signal.In fuel oil tank 4, store fuel, for providing power to driving engine.
Front end at equipment compartment 2 can also be provided with pitot 1, and pitot 1 can reduce the resistance of unmanned signal in flight course.
On fuselage, can also be provided with alighting gear 12 and wheel 11 to facilitate landing.The utlity model has easy to carry, safeguard use simple, cost is low, reusable, the feature such as when long boat, aspect signal and communication relaying, there is stronger advantage, this unmanned signal capacity weight is large, can carry high-side signal trunking, realize aerial signal relay function, lower hanging mission payload experiment carrying equipment test aspect has stronger advantage, is easy to apply.
Each embodiment in this specification sheets all adopts the mode of going forward one by one to describe, and what each embodiment stressed is and the difference of other embodiment, between each embodiment identical similar part mutually referring to.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (9)
1. a unmanned signal, it is characterized in that: it comprises fuselage, is connected to the wing on described fuselage and is connected to the empennage on described fuselage by the second latch by the first latch, described fuselage comprises equipment compartment, battery flat, fuel oil tank, umbrella cabin and piggyback pod from front to back successively, the below in described umbrella cabin is also provided with load cabin, and described load is provided with trunking in cabin.
2. unmanned signal according to claim 1, is characterized in that: in described equipment compartment, be provided with autopilot.
3. unmanned signal according to claim 1, is characterized in that: in described battery flat, be provided with the battery for electric power is provided.
4. unmanned signal according to claim 1, is characterized in that: described umbrella is provided with parachute in cabin.
5. unmanned signal according to claim 1, is characterized in that: in described piggyback pod, be provided with driving engine.
6. unmanned signal according to claim 1, is characterized in that: described trunking is relay.
7. unmanned signal according to claim 1, is characterized in that: described empennage comprises shoe, be vertically connected at the vertical fin of described shoe and be vertically connected at the horizontal tail of described vertical fin.
8. unmanned signal according to claim 1, is characterized in that: the front end of described equipment compartment is provided with pitot.
9. unmanned signal according to claim 1, is characterized in that: in described fuel oil tank, store fuel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320825977.8U CN203727648U (en) | 2013-12-13 | 2013-12-13 | Unmanned annunciator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320825977.8U CN203727648U (en) | 2013-12-13 | 2013-12-13 | Unmanned annunciator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203727648U true CN203727648U (en) | 2014-07-23 |
Family
ID=51197740
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320825977.8U Expired - Fee Related CN203727648U (en) | 2013-12-13 | 2013-12-13 | Unmanned annunciator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203727648U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106685510A (en) * | 2015-11-09 | 2017-05-17 | 中国移动通信集团公司 | Relay system of wireless signal coverage and communication method |
| CN108860601A (en) * | 2017-05-11 | 2018-11-23 | 厦门市汉飞鹰航空科技有限公司 | A kind of device and method of small-sized fixed-wing unmanned plane modularization load cabin |
-
2013
- 2013-12-13 CN CN201320825977.8U patent/CN203727648U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106685510A (en) * | 2015-11-09 | 2017-05-17 | 中国移动通信集团公司 | Relay system of wireless signal coverage and communication method |
| CN108860601A (en) * | 2017-05-11 | 2018-11-23 | 厦门市汉飞鹰航空科技有限公司 | A kind of device and method of small-sized fixed-wing unmanned plane modularization load cabin |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Airfoil for unmanned annunciator and unmanned annunciator adopting same Effective date of registration: 20150209 Granted publication date: 20140723 Pledgee: Hunchun Jilin rural commercial bank Limited by Share Ltd Pledgor: HUNCHUN GUOYAOBOCHENG TECHNOLOGY CO., LTD. Registration number: 2015990000120 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140723 Termination date: 20201213 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |