CN113895620A - A military child-mother unmanned aerial vehicle system - Google Patents
A military child-mother unmanned aerial vehicle system Download PDFInfo
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- CN113895620A CN113895620A CN202111178855.XA CN202111178855A CN113895620A CN 113895620 A CN113895620 A CN 113895620A CN 202111178855 A CN202111178855 A CN 202111178855A CN 113895620 A CN113895620 A CN 113895620A
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- aerial vehicle
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
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Abstract
The invention belongs to the technical field of electronic power unmanned aerial vehicles, and particularly relates to a military primary-secondary unmanned aerial vehicle system which comprises a primary machine system, a secondary machine system and a ground station, wherein the ground station controls the primary machine, the primary machine arrives at a use place by carrying a secondary machine, the secondary machine is released, the secondary machine is used for executing tasks by consuming loads once, the secondary machine can carry detonators, laser guides, electronic disturbers and the like, one primary machine can carry the secondary machines with the same or different functions to execute tasks in a battlefield, the use is very flexible, and the cost is low.
Description
Technical Field
The invention belongs to the technical field of electronic power unmanned aerial vehicles, and particularly relates to a military primary-secondary unmanned aerial vehicle system.
Background
The military unmanned aerial vehicle has the characteristics of 0 casualty, less use limitation, good concealment, high efficiency-cost ratio and the like, the status and the action of the military unmanned aerial vehicle in modern war are gradually highlighted, and the number, the types, the frequency and the like of the military unmanned aerial vehicle in recent local war are in a rapid growth trend, so that the rapid development of the unmanned aerial vehicle becomes a common recognition of military, strong country and military.
In recent years, each country has seen a development plan of each unmanned aerial vehicle, and the investment is increased, so that the development of military unmanned aerial vehicles shows no prior heat tide, and can meet the situation that the unmanned aerial vehicles will play a very important role in future war with the unique advantages of the unmanned aerial vehicles.
Disclosure of Invention
The invention provides a military primary-secondary unmanned aerial vehicle system with an independent power supply and a power system, wherein a primary machine can effectively carry a plurality of even several teamed secondary machines, the secondary machines can be used for carrying blasting detonators, laser guides, electronic disturbers and the like to support a battlefield, and the military primary-secondary unmanned aerial vehicle system is flexible and variable in tactics and low in cost.
The military primary-secondary unmanned aerial vehicle system is characterized by comprising a ground station (1), a primary system (2) and a secondary system (3).
A military primary-secondary unmanned aerial vehicle system according to claim 1, wherein the primary system (2) comprises a primary wireless signal transceiver (4), a primary cradle head (5), a primary image transmission (6), a primary flight control system (10), a primary power supply system (14) and a primary engine system (15).
A military primary-secondary unmanned aerial vehicle system according to claim 1, wherein the secondary aircraft system (3) comprises a secondary aircraft wireless signal transceiver (7), a secondary aircraft cradle head (8), a secondary aircraft image transmission (9), a secondary aircraft release device (11), a secondary aircraft flight control system (12), a secondary aircraft payload operating system (13), a secondary aircraft power supply system (16) and a secondary aircraft engine system (17).
A military primary-secondary unmanned aerial vehicle system as claimed in claim 1, wherein the ground station (1) controls the primary aircraft system (2) to operate the primary aircraft to fly to a use site, the ground station (1) controls the secondary aircraft system (3) to enable the secondary aircraft to be separated from the primary aircraft, and the secondary aircraft performs tasks.
The military primary-secondary drone system of claim 1 wherein the secondary drone performs as a disposable consumable.
A military primary and secondary drone system according to claim 1 wherein items operated by the secondary payload operating system (13) include but are not limited to blasting detonators, laser guides, electronic disturbers.
The military primary-secondary unmanned aerial vehicle system of claim 1, wherein the number of slaves carried by a master includes but is not limited to 2.
The technology of the invention has the following advantages:
(1) in the military primary-secondary unmanned aerial vehicle system provided by the invention, the secondary machines are low in cost, the primary machines can return to the air and be recycled after the task of the primary machine is finished, and the secondary machines can be scrapped after being used as disposable consumables to execute the task.
(2) Tactical consumables carried by the submachine are various in types, but the submachine has the characteristics of small volume, light weight and low cost, can independently execute tasks and can form a team to execute the tasks, and the submachine is high in flexibility and suitable for complex and variable battlefields.
Drawings
FIG. 1 is a structural framework diagram of a military primary-secondary unmanned aerial vehicle system of the present invention
Detailed Description
The technical solutions in the patent cases of the present invention will be described below with reference to the drawings and the specific design solutions, the described cases are only a part of the cases of the present invention, and all other cases obtained by those skilled in the art without any creative efforts based on the cases in the patent cases belong to the protection scope of the present patent.
Case 1
As shown in figure 1, the whole system is divided into a ground station (1), a master machine system (2) and a slave machine system (3).
The master system (2) comprises a master wireless signal transceiver (4), a master holder (5), a master image transmission (6), a master flight control system (10), a master power system (14) and a master engine system (15).
The slave unit system (3) comprises a slave unit wireless signal transceiver (7), a slave unit cradle head (8), a slave unit image transmission (9), a slave unit release device (11), a slave unit flight control system (12), a slave unit payload operation system (13), a slave unit power supply system (16) and a slave unit engine system (17).
The ground station (1) sends a signal to the master wireless signal transceiver (4) to operate the master flight control system (10), the master carries out master image transmission (6) through the master cradle head (5) and the camera and feeds back the image to the ground station (1), and meanwhile, the master flight control system (10) controls the master power system (14) and the master engine system (15) to be started.
When the mother aircraft flies to a battlefield to execute a task, the ground station sends a signal to the wireless signal transceiver (7) of the son aircraft to operate the flight control system (12) of the son aircraft, and the mother aircraft carries out mother aircraft image transmission (9) through the camera of the cradle head (8) of the mother aircraft and feeds back the mother aircraft image transmission to the ground station (1).
The ground station (1) controls a submachine flight control system (12) to start a submachine release device (11), and the submachine is separated from the master machine independently to continue a task. When the submachine is separated, the submachine flight control system (12) controls the submachine power supply system (16) and the submachine engine system (17) to be started synchronously, so that the submachine cannot fall down when being separated from the master machine.
The slave unit flies to a designated place as a disposable consumable product to execute a task, and a slave unit flight control system (12) starts a slave unit payload operation system (13).
Targets operated by the handset payload operating system (13) include, but are not limited to, blasting detonators, laser guides, and electronic disruptors.
It will be appreciated by persons skilled in the art that while the present invention has been described in terms of the foregoing embodiments, any use of the concepts of the present invention is within the scope of the appended claims.
Claims (7)
1. The military primary-secondary unmanned aerial vehicle system is characterized by comprising a ground station (1), a primary system (2) and a secondary system (3).
2. A military primary-secondary unmanned aerial vehicle system according to claim 1, wherein the primary system (2) comprises a primary wireless signal transceiver (4), a primary cradle head (5), a primary image transmission (6), a primary flight control system (10), a primary power supply system (14) and a primary engine system (15).
3. A military primary-secondary unmanned aerial vehicle system according to claim 1, wherein the secondary aircraft system (3) comprises a secondary aircraft wireless signal transceiver (7), a secondary aircraft cradle head (8), a secondary aircraft image transmission (9), a secondary aircraft release device (11), a secondary aircraft flight control system (12), a secondary aircraft payload operating system (13), a secondary aircraft power supply system (16) and a secondary aircraft engine system (17).
4. A military primary-secondary unmanned aerial vehicle system as claimed in claim 1, wherein the ground station (1) controls the primary aircraft system (2) to operate the primary aircraft to fly to a use site, the ground station (1) controls the secondary aircraft system (3) to enable the secondary aircraft to be separated from the primary aircraft, and the secondary aircraft performs tasks.
5. The military primary-secondary drone system of claim 1 wherein the secondary drone performs as a disposable consumable.
6. A military primary and secondary drone system according to claim 1 wherein items operated by the secondary payload operating system (13) include but are not limited to blasting detonators, laser guides, electronic disturbers.
7. The military primary-secondary unmanned aerial vehicle system of claim 1, wherein the number of slaves carried by a master includes but is not limited to 2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111178855.XA CN113895620A (en) | 2021-10-09 | 2021-10-09 | A military child-mother unmanned aerial vehicle system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111178855.XA CN113895620A (en) | 2021-10-09 | 2021-10-09 | A military child-mother unmanned aerial vehicle system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113895620A true CN113895620A (en) | 2022-01-07 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111178855.XA Pending CN113895620A (en) | 2021-10-09 | 2021-10-09 | A military child-mother unmanned aerial vehicle system |
Country Status (1)
| Country | Link |
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| CN (1) | CN113895620A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105303899A (en) * | 2015-11-12 | 2016-02-03 | 范云生 | Child-mother type robot cooperation system of combination of unmanned surface vessel and unmanned aerial vehicle |
| US20160214717A1 (en) * | 2013-10-08 | 2016-07-28 | Shelton Gamini De Silva | Combination of unmanned aerial vehicles and the method and system to engage in multiple applications |
| CN106005410A (en) * | 2016-07-05 | 2016-10-12 | 国网浙江省电力公司衢州供电公司 | Novel son and mother unmanned aerial vehicle system |
| CN107272739A (en) * | 2017-07-24 | 2017-10-20 | 湘潭大学 | A kind of pesticide spraying system and method based on primary and secondary system |
| CN108216621A (en) * | 2017-12-13 | 2018-06-29 | 中国航空工业集团公司成都飞机设计研究所 | A kind of wing tip connection composite lights aircraft in parallel |
| CN111645835A (en) * | 2019-12-10 | 2020-09-11 | 河北汉光重工有限责任公司 | Unmanned primary and secondary underwater vehicle with multiple underwater belts |
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2021
- 2021-10-09 CN CN202111178855.XA patent/CN113895620A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160214717A1 (en) * | 2013-10-08 | 2016-07-28 | Shelton Gamini De Silva | Combination of unmanned aerial vehicles and the method and system to engage in multiple applications |
| CN105303899A (en) * | 2015-11-12 | 2016-02-03 | 范云生 | Child-mother type robot cooperation system of combination of unmanned surface vessel and unmanned aerial vehicle |
| CN106005410A (en) * | 2016-07-05 | 2016-10-12 | 国网浙江省电力公司衢州供电公司 | Novel son and mother unmanned aerial vehicle system |
| CN107272739A (en) * | 2017-07-24 | 2017-10-20 | 湘潭大学 | A kind of pesticide spraying system and method based on primary and secondary system |
| CN108216621A (en) * | 2017-12-13 | 2018-06-29 | 中国航空工业集团公司成都飞机设计研究所 | A kind of wing tip connection composite lights aircraft in parallel |
| CN111645835A (en) * | 2019-12-10 | 2020-09-11 | 河北汉光重工有限责任公司 | Unmanned primary and secondary underwater vehicle with multiple underwater belts |
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Application publication date: 20220107 |
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