CN204279947U - The unmanned prior-warning plane of a kind of novel long-range - Google Patents
The unmanned prior-warning plane of a kind of novel long-range Download PDFInfo
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- CN204279947U CN204279947U CN201420667247.4U CN201420667247U CN204279947U CN 204279947 U CN204279947 U CN 204279947U CN 201420667247 U CN201420667247 U CN 201420667247U CN 204279947 U CN204279947 U CN 204279947U
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- fuselage
- unmanned
- empennage
- wing
- early warning
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Abstract
The utility model discloses the unmanned prior-warning plane of a kind of novel long-range, comprise fuselage, air refueling probe, take-off and landing device, wing, driving engine, empennage, early warning radar fairing, described wing is positioned at the both sides of described fuselage; Described driving engine is positioned at the below of described wing; The fairing of described early warning radar is positioned at before the top of described fuselage, described empennage; Described air refueling probe is positioned at the front end of described fuselage; Described front fuselage is provided with described air refueling probe, tail end is provided with described empennage, the utility model is when work, can be flown out in different spatial domain required speed, due to can air refuelling be carried out, can continue a journey for unmanned plane, reach farther destination, ensure unmanned function in different spatial domain, different distance can finish the work smoothly.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is specifically related to a kind of novel high speed long-range unmanned early warning investigation aircraft.
Background technology
Robot airplane, is called for short unmanned plane (UAV), is a kind ofly to be in the equipment of the new concept weapon in developing rapidly, its have maneuverability, reaction fast, unmanned flight, advantage that operation requirements is low.Unmanned plane, by carrying multiclass sensor, can realize image real-time Transmission, high-risk areas detecting function, is that satellite remote sensing and the strong of traditional air remote sensing supplement.At present, the range of use of unmanned plane has widened military affairs, scientific research, civilian three large fields, specifically in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the application of public security anti-terrorism field be very wide.Large-scale unmanned early warning investigation aircraft due to take-off weight large, the speed of a ship or plane and voyage are all subject to certain restriction, there is shortcoming when practical operation, can not meet friction speed, distance be have requirement.Four driving engines are equipped with in the present invention, and can meet the requirement to friction speed, front fuselage is provided with air refueling probe, and can implement air refuelling increases voyage.The feature of the common unmanned early warning investigation aircraft of the utility model, also has the different speed of a ship or plane and longer voyage simultaneously, can meet the user demand of various condition, have more superior performance.
Summary of the invention
In order to solve above-mentioned Problems existing, the utility model is equipped with four dynamic driving engines, can meet multiple speed rank, and can carry out air refuelling, is the continuation of the journey of early warning and reconnaissance aircraft.
The utility model is achieved through the following technical solutions:
The unmanned prior-warning plane of a kind of novel long-range, comprise fuselage, air refueling probe, take-off and landing device, wing, driving engine, empennage, early warning radar fairing, described wing is positioned at the both sides of described fuselage; Described driving engine is positioned at the below of described wing; The fairing of described early warning radar is positioned at before the top of described fuselage, described empennage; Described air refueling probe is positioned at the front end of described fuselage; Described front fuselage is provided with described air refueling probe, and tail end is provided with described empennage.
As further prioritization scheme of the present utility model, described empennage is positioned at above the end of fuselage.
As further prioritization scheme of the present utility model, ventral is provided with described take-off and landing device, and both sides are provided with described wing, and top is provided with the fairing of described early warning radar.
Compared with prior art, the beneficial effects of the utility model are: the utility model can meet unmanned early warning investigation aircraft to the demand of friction speed rank, air refuelling can be carried out, the speed of unmanned plane can be ensured, the voyage of unmanned plane can be ensured again, the operating needs of various different environment can be adapted to.
Accompanying drawing explanation
Fig. 1 is elevational schematic view of the present utility model;
Fig. 2 is that axle of the present utility model measures intention;
Fig. 3 is front view of the present utility model;
Fig. 4 is right elevation of the present utility model.
In figure: 1, fuselage; 2, air refueling probe; 3, take-off and landing device; 4, wing; 5, driving engine; 6, empennage; 7, early warning radar fairing.
Detailed description of the invention
Below in conjunction with accompanying drawing and detailed description of the invention, the utility model is described in further detail:
As shown in Figure 1, Figure 2, shown in Fig. 3 and Fig. 4, the unmanned prior-warning plane of a kind of novel long-range, comprise fuselage 1, air refueling probe 2, take-off and landing device 3, wing 4, driving engine 5, empennage 6, early warning radar fairing 7, described wing 4 is positioned at the both sides of described fuselage 1; Described driving engine 5 is positioned at the below of described wing 4, and described driving engine 5 is four, can meet the requirement of friction speed; Described early warning radar fairing 7 is positioned at the top of described fuselage 1, and before described empennage 6, described early warning radar fairing 7 adopts stream line pattern, can meet the operating needs of radar, also can meet the aerodynamic demands of aircraft flight; Described air refueling probe 2 is positioned at the front end of described fuselage 1, can carry out air refuelling when long-distance flight, extends voyage and to achieve the goal spatial domain; Described empennage 6 is positioned at above the end of fuselage 1; Described fuselage 1 front end is provided with described air refueling probe 2, and tail end is provided with described empennage 6, and ventral is provided with described take-off and landing device 3, and both sides are provided with described wing 4, and top is provided with described early warning radar fairing 7.
The utility model is when work, and described driving engine 5 can meet the speed of unmanned plane needed for the condition of different spatial domains, and described early warning radar fairing 7 can meet the operating needs of radar, also can meet the aerodynamic demands of aircraft flight; Described air refueling probe 2 can be continued a journey for unmanned plane, reaches farther destination, ensure unmanned function in different spatial domain, different distance can finish the work smoothly.
More than show and describe groundwork of the present utility model, principal character and advantage.The technical personnel of the industry should be understood; the utility model is not restricted to the described embodiments; what describe in above-described embodiment and specification sheets just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and effect thing thereof.
Claims (3)
1. the unmanned prior-warning plane of novel long-range, is characterized in that: comprise fuselage, air refueling probe, take-off and landing device, wing, driving engine, empennage, early warning radar fairing, and described wing is positioned at the both sides of described fuselage; Described driving engine is positioned at the below of described wing; The fairing of described early warning radar is positioned at before the top of described fuselage, described empennage; Described air refueling probe is positioned at the front end of described fuselage; Described front fuselage is provided with described air refueling probe, and tail end is provided with described empennage.
2. the unmanned prior-warning plane of the novel long-range of one according to claim 1, is characterized in that: described empennage is positioned at above the end of fuselage.
3. the unmanned prior-warning plane of the novel long-range of one according to claim 1, it is characterized in that: ventral is provided with described take-off and landing device, both sides are provided with described wing, and top is provided with the fairing of described early warning radar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420667247.4U CN204279947U (en) | 2014-11-10 | 2014-11-10 | The unmanned prior-warning plane of a kind of novel long-range |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420667247.4U CN204279947U (en) | 2014-11-10 | 2014-11-10 | The unmanned prior-warning plane of a kind of novel long-range |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204279947U true CN204279947U (en) | 2015-04-22 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420667247.4U Expired - Fee Related CN204279947U (en) | 2014-11-10 | 2014-11-10 | The unmanned prior-warning plane of a kind of novel long-range |
Country Status (1)
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105000193A (en) * | 2015-06-23 | 2015-10-28 | 中国航空工业集团公司西安飞机设计研究所 | Follow-up radome bracket and follow-up radar with same as well as aircraft |
| CN105302158A (en) * | 2015-10-23 | 2016-02-03 | 南京航空航天大学 | Unmanned aerial vehicle aerial refueling shortest time meeting method based on Dubins path |
| CN105947174A (en) * | 2016-05-12 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | Airplane |
| CN106379510A (en) * | 2016-09-29 | 2017-02-08 | 华东电子工程研究所（中国电子科技集团公司第三十八研究所） | Load structure integrated sensor flight vehicle |
| CN111369833A (en) * | 2020-03-09 | 2020-07-03 | 沈观清 | Early warning and countermeasure system based on long-endurance large-height small unmanned aerial vehicle |
-
2014
- 2014-11-10 CN CN201420667247.4U patent/CN204279947U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105000193A (en) * | 2015-06-23 | 2015-10-28 | 中国航空工业集团公司西安飞机设计研究所 | Follow-up radome bracket and follow-up radar with same as well as aircraft |
| CN105302158A (en) * | 2015-10-23 | 2016-02-03 | 南京航空航天大学 | Unmanned aerial vehicle aerial refueling shortest time meeting method based on Dubins path |
| CN105302158B (en) * | 2015-10-23 | 2018-05-22 | 南京航空航天大学 | Unmanned plane air refuelling shortest time congregation method based on Dubins paths |
| CN105947174A (en) * | 2016-05-12 | 2016-09-21 | 中国航空工业集团公司西安飞机设计研究所 | Airplane |
| CN106379510A (en) * | 2016-09-29 | 2017-02-08 | 华东电子工程研究所（中国电子科技集团公司第三十八研究所） | Load structure integrated sensor flight vehicle |
| CN111369833A (en) * | 2020-03-09 | 2020-07-03 | 沈观清 | Early warning and countermeasure system based on long-endurance large-height small unmanned aerial vehicle |
| CN111369833B (en) * | 2020-03-09 | 2021-06-08 | 沈观清 | Early warning and countermeasure system based on long-endurance large-height small unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150422 Termination date: 20151110 |
|
| EXPY | Termination of patent right or utility model |