CN110937111B - Small-size cluster unmanned aerial vehicle dispensing system of gliding style - Google Patents
Small-size cluster unmanned aerial vehicle dispensing system of gliding style Download PDFInfo
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- CN110937111B CN110937111B CN201911196917.2A CN201911196917A CN110937111B CN 110937111 B CN110937111 B CN 110937111B CN 201911196917 A CN201911196917 A CN 201911196917A CN 110937111 B CN110937111 B CN 110937111B
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- unmanned aerial
- aerial vehicle
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/10—Stowage arrangements for the devices in aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
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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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- 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
Abstract
The invention discloses a gliding small-sized cluster unmanned aerial vehicle launching device, which consists of a gliding pod, a folding main wing, a folding tail wing, a locking and releasing mechanism, a control subsystem and a small-sized unmanned aerial vehicle, wherein the gliding pod is arranged on the upper portion of the small-sized cluster unmanned aerial vehicle; the gliding nacelle is connected to the wings of the carrier by means of a wing pylon. The main wing surface and the tail wing surface are respectively arranged in the middle and the tail of the gliding nacelle of the small unmanned aerial vehicle in a folding mode. The locking and releasing mechanism of the small unmanned aerial vehicle is of an electromagnetic lock hook structure and is positioned in the belly of the gliding nacelle; when loading unmanned aerial vehicle, the electromagnetism latch hook pins two hangers around with unmanned aerial vehicle, realizes unmanned aerial vehicle's locking. The onboard battery and flight control subsystem are located in front of the drone glide pod. The onboard battery provides power for the unlocking and releasing mechanism and the flight control subsystem; and an explosion bolt for fastening a cabin door of the gliding nacelle is opened, and the small unmanned aerial vehicle locking and releasing mechanism is sequentially unlocked and released. The flight control of the gliding pod and the launching of the small unmanned aerial vehicle are realized.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a small-sized cluster unmanned aerial vehicle rapid delivery system adopting an externally hung gliding pod.
Background
The unmanned aerial vehicle 'bee colony' tactics integrates the technical advantages of the unmanned aerial vehicle and the system group advantages, and the suppression is carried out on the enemy while the fighting capacity of the unmanned aerial vehicle is kept. The swarm unmanned aerial vehicle consists of a plurality of small unmanned aerial vehicles, and can form a number of advantages on enemies in a local combat area. Especially in high-rejection operational environments, the loss of a single drone does not affect the operational performance of the entire cluster. Therefore, various countries in the world have developed researches on the unmanned aerial vehicle clustering technology. The launching mode of the small swarm unmanned aerial vehicle mainly comprises three modes of ground box type launching, air medium and large mother machine loading launching and gun launching. The ground box type transmitting mode is limited by the range and the time of flight of the small unmanned aerial vehicle, and in order to reach a designated combat area, the ground transmitting unit must be close to an enemy threat area, so that long-distance launching cannot be realized. The gun is penetrated the transmission and is owing to receive bore size restriction, and structure integrated level is higher, and the thermal shock and the dynamic load that unmanned aerial vehicle bore in the bore born during the transmission are great, have more restrictions to unmanned aerial vehicle's structural strength and overall arrangement form, and this transmission mode is still in theoretical stage. The aerial large and medium-sized mother machines can be loaded by a man-machine or a large-sized unmanned aerial vehicle to load a cluster unmanned aerial vehicle to fly above a combat area for aerial delivery and emission, and the mode can realize the remote delivery of the small swarm unmanned aerial vehicle. However, the launching mode still needs the aerial carrier to have man-machine or unmanned aerial vehicle flying to the sky above the enemy area, and the aerial carrier is inevitably threatened by air or ground firepower from the enemy in the launching process. This type of launch is not suitable for the launch of small bee colony unmanned aerial vehicles in the strong rejection environment.
Disclosure of Invention
In order to avoid the defects in the prior art, the invention provides a gliding type small-sized cluster unmanned aerial vehicle launching system; this dispensing system can protect the carrier safety, realizes launching small-size bee colony unmanned aerial vehicle fast outside keeping away from enemy firepower threat radius. The feeding system has the characteristics of simple structure, light weight and low cost.
The invention solves the technical problem by adopting the technical scheme that the gliding pod comprises a gliding pod, a folding main wing, a folding tail wing, a locking and releasing mechanism, an abdominal throwing type cabin door, an airborne battery, a control subsystem and a small unmanned aerial vehicle, and is characterized in that the gliding pod is connected to the wings of a medium-sized unmanned aerial vehicle through a main aircraft wing hanging frame; the folding main wing surface and the folding tail wing root are connected with torsion springs, and the main wing surface and the tail wing surface are respectively installed in the middle and the tail of the gliding nacelle in a folding mode;
the locking and releasing mechanism is of an electromagnetic lock hook structure, the locking and releasing mechanism is positioned in the belly of the gliding pod of the small unmanned aerial vehicle, and when the small unmanned aerial vehicle is loaded, the electromagnetic lock hook locks the front and rear two lugs of the small unmanned aerial vehicle so as to realize locking of the small unmanned aerial vehicle; the airborne battery and the control subsystem are positioned at the front part of the small unmanned aerial vehicle gliding nacelle, and the airborne battery provides electric power for the unlocking and releasing mechanism and the flight control subsystem so as to realize the flight control of the gliding nacelle and the launching of the small unmanned aerial vehicle;
when the small unmanned aerial vehicle is thrown, the folding main wing surface cutter and the folding tail wing surface cutter respectively cut off the main wing surface binding rope and the tail wing surface binding rope, and the folding main wing and the folding tail wing of the small unmanned aerial vehicle gliding nacelle are unfolded under the action of the torsion spring;
the flight control subsystem of the gliding pod is powered up to control the gliding pod, an explosion bolt connected with the disposable cabin door of the gliding pod is unlocked, the disposable cabin door of the gliding pod is opened under the action of gravity and aerodynamic force, and the small unmanned aerial vehicle locking and releasing mechanism sequentially unlocks and releases the small unmanned aerial vehicle; and the small-sized cluster unmanned aerial vehicle is delivered in a near mode.
The gliding pod is symmetrically arranged according to the body of the unmanned aerial vehicle, and is of a streamline structure.
Advantageous effects
The invention provides a gliding type small-sized cluster unmanned aerial vehicle launching device which comprises a gliding pod, a folding main wing, a folding tail wing, a locking and releasing mechanism, a control subsystem and a small-sized unmanned aerial vehicle, wherein the gliding pod is arranged on the upper portion of the gliding pod; the gliding nacelle is connected to the wings of the carrier by means of a wing pylon. The main wing surface and the tail wing surface are respectively arranged in the middle and the tail of the small unmanned aerial vehicle gliding nacelle in a folding mode. The locking and releasing mechanism of the small unmanned aerial vehicle is of an electromagnetic lock hook structure and is positioned in the belly of the gliding nacelle; when loading unmanned aerial vehicle, the electromagnetism latch hook pins two hangers around with unmanned aerial vehicle, realizes unmanned aerial vehicle's locking. The onboard battery and flight control subsystem are located in front of the drone glide pod. The onboard battery provides power for the unlocking and releasing mechanism and the flight control subsystem; and an explosion bolt for fastening a cabin door of the gliding nacelle is opened, and the small unmanned aerial vehicle locking and releasing mechanism is sequentially unlocked and released. The flight control of the gliding pod and the launching of the small unmanned aerial vehicle are realized.
The gliding type small cluster unmanned aerial vehicle launching device can realize aerial launching in an area far away from enemy fire threat, and the safety of the aerial carrier is high; a plurality of gliding nacelle can put in small-size bee colony unmanned aerial vehicle simultaneously, and the input time is short.
The gliding small-sized cluster unmanned aerial vehicle throwing device avoids the continuous emission of the small-sized swarm unmanned aerial vehicle near the carrier, and eliminates the risk of collision between the small-sized swarm unmanned aerial vehicle and the carrier; the aircraft can carry a plurality of gliding throwing nacelle, and the gliding throwing nacelle can fly to different combat areas under the effect of the flight control system, and the throwing area is large and flexible.
Drawings
The following describes a gliding small-sized cluster unmanned aerial vehicle launching system in further detail with reference to the accompanying drawings and embodiments.
Fig. 1 is a schematic diagram of a launching process of a gliding type small cluster unmanned aerial vehicle launching system.
Fig. 2 is a schematic view of a gliding pod of the gliding type small-cluster unmanned aerial vehicle delivery system of the invention.
In the figure:
1. gliding pod 2, folding main wing 3, folding tail wing 4, belly throwing type cabin door 5, airborne battery 6, control subsystem 7, locking and releasing mechanism 8, small unmanned aerial vehicle
Detailed Description
The embodiment is a small-size cluster unmanned aerial vehicle delivery system of gliding style.
Referring to fig. 1 and fig. 2, the gliding type small cluster unmanned aerial vehicle launching system of the embodiment is composed of a gliding pod 1, a folding main wing 2, a folding tail wing 3, a locking and releasing mechanism 7, an abdomen throwing type cabin door 4, an airborne battery 5, a control subsystem 6 and a small unmanned aerial vehicle 8; the gliding nacelle 1 is connected to the wings of the medium-sized unmanned aerial vehicle through a parent aircraft wing hanging rack; the folding main wing surface and the folding tail wing root are connected with torsion springs, and the main wing surface and the tail wing surface are respectively installed in the middle and the tail of the small unmanned aerial vehicle gliding nacelle 1 in a folding mode. The locking and releasing mechanism 7 is of an electromagnetic latch hook structure, and the locking and releasing mechanism 7 is positioned in the belly of the small unmanned aerial vehicle gliding nacelle 1; when loading unmanned aerial vehicle, two hangers pin around electromagnetic lock hook 7 with unmanned aerial vehicle, realize unmanned aerial vehicle's locking. The airborne battery 5 and the control subsystem 6 are located in the front of the small unmanned aerial vehicle gliding nacelle 1, and the airborne battery 5 provides power for the unlocking and releasing mechanism 7 and the flight control subsystem 6, so that the flight control of the gliding nacelle and the launching of the small unmanned aerial vehicle are realized.
When the small unmanned aerial vehicle is thrown in, the folding main wing surface cutter and the folding tail wing surface cutter respectively cut off and connect the main wing surface strapping ropes and the tail wing surface strapping ropes, and the folding main wing 2 and the folding tail wing 3 of the small unmanned aerial vehicle gliding nacelle 1 are unfolded under the action of the torsion spring.
The flight control subsystem 6 of the gliding pod is powered on to control the gliding pod, an explosion bolt connected with the disposable cabin door 4 of the gliding pod is unlocked, the disposable cabin door 4 of the gliding pod is opened under the action of gravity and aerodynamic force, and the small unmanned aerial vehicle locking and releasing mechanism 7 sequentially unlocks and releases the small unmanned aerial vehicle; and the small-sized cluster unmanned aerial vehicle is delivered in a near mode. The gliding pod is symmetrically arranged according to the unmanned aerial vehicle, and is of a streamline structure.
In this embodiment, when the small swarm drone is launched, the medium-sized and large-sized drone aircraft flies outside the thermal radius of the enemy, and the gliding drone gliding pod is released at high altitude. The gliding pod is accelerated to leave downwards under the action of gravity. After the gliding type small unmanned aerial vehicle nacelle reaches the safety distance from the main machine, the folding main wing surface cutter and the folding tail wing surface cutter respectively cut off and connect the main wing surface binding rope and the tail wing surface binding rope, and the folding main wing and the folding tail wing of the gliding type small unmanned aerial vehicle nacelle are unfolded under the action of the torsion spring. And the gliding pod flight control subsystem is electrified to control the gliding pod to fly to the target area. When the gliding pod reaches the designated combat area, the explosion bolt connected with the disposable cabin door of the gliding pod belly is unlocked, the disposable cabin door of the gliding pod belly is opened under the action of gravity and aerodynamic force, and the small unmanned aerial vehicle locking and releasing mechanism sequentially unlocks and releases the small unmanned aerial vehicle. And the small-sized cluster unmanned aerial vehicle is delivered in a near mode.
Claims (2)
1. A gliding type small-sized cluster unmanned aerial vehicle launching system comprises a gliding pod, a folding main wing, a folding tail wing, a locking and releasing mechanism, an abdominal throwing type cabin door, an airborne battery, a control subsystem and a small-sized unmanned aerial vehicle, and is characterized in that the gliding pod is connected to the wings of a medium-sized unmanned aerial vehicle through a main aircraft wing hanging rack; the folding main wing surface and the folding tail wing root are connected with torsion springs, and the main wing surface and the tail wing surface are respectively installed in the middle and the tail of the gliding nacelle in a folding mode;
the locking and releasing mechanism is of an electromagnetic lock hook structure, the locking and releasing mechanism is positioned in the belly of the gliding pod of the small unmanned aerial vehicle, and when the small unmanned aerial vehicle is loaded, the electromagnetic lock hook locks the front and rear hangers of the small unmanned aerial vehicle so as to lock the small unmanned aerial vehicle; the airborne battery and the control subsystem are positioned at the front part of the gliding pod of the small unmanned aerial vehicle, and the airborne battery provides power for the unlocking and releasing mechanism and the flight control subsystem so as to realize the flight control of the gliding pod and the launching of the small unmanned aerial vehicle;
when the small unmanned aerial vehicle is thrown, the folding main wing surface cutter and the folding tail wing surface cutter respectively cut off the main wing surface binding rope and the tail wing surface binding rope, and the folding main wing and the folding tail wing of the small unmanned aerial vehicle gliding nacelle are unfolded under the action of the torsion spring;
the flight control subsystem of the gliding pod is powered up to control the gliding pod, an explosion bolt connected with the disposable cabin door of the gliding pod is unlocked, the disposable cabin door of the gliding pod is opened under the action of gravity and aerodynamic force, and the small unmanned aerial vehicle locking and releasing mechanism sequentially unlocks and releases the small unmanned aerial vehicle; and the small-sized cluster unmanned aerial vehicle is delivered in a near mode.
2. The gliding type small cluster unmanned aerial vehicle launching system as claimed in claim 1, is characterized in that the gliding pod is symmetrically arranged according to the unmanned aerial vehicle body, and the gliding pod is of a streamline structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911196917.2A CN110937111B (en) | 2019-11-29 | 2019-11-29 | Small-size cluster unmanned aerial vehicle dispensing system of gliding style |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201911196917.2A CN110937111B (en) | 2019-11-29 | 2019-11-29 | Small-size cluster unmanned aerial vehicle dispensing system of gliding style |
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| CN110937111A CN110937111A (en) | 2020-03-31 |
| CN110937111B true CN110937111B (en) | 2022-09-02 |
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Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824386B (en) * | 2020-06-22 | 2023-01-10 | 中国科学院空天信息创新研究院 | Aircraft launching device and method |
| CN112224432A (en) * | 2020-09-22 | 2021-01-15 | 南京航空航天大学 | Interference bomb suitable for mixed marshalling aircraft is empty base transmission in batches |
| CN112249333A (en) * | 2020-09-23 | 2021-01-22 | 北京特种机械研究所 | Microminiature aerial scattering type unmanned aerial vehicle system |
| CN112607031B (en) * | 2020-12-22 | 2022-02-22 | 西安羚控电子科技有限公司 | Modular unmanned aerial vehicle cluster aerial rapid delivery system |
| CN113200146A (en) * | 2021-05-18 | 2021-08-03 | 重庆交通大学 | Missile type folding cluster unmanned aerial vehicle control method, system, medium and unmanned aerial vehicle |
| CN113492992B (en) * | 2021-07-21 | 2022-10-28 | 中国电子科技集团公司电子科学研究院 | Throwing device and throwing method of folding wing unmanned aerial vehicle |
| CN113815861B (en) * | 2021-10-27 | 2024-04-02 | 江西洪都航空工业股份有限公司 | Gliding type remote accurate air drop device |
| CN114476074B (en) * | 2022-03-09 | 2023-11-10 | 四川傲势科技有限公司 | Unmanned aerial vehicle throwing feedback and actuating device and method |
| CN117048849B (en) * | 2023-10-13 | 2024-01-23 | 四川腾盾科技有限公司 | Flight test method for propeller-driven unmanned aerial vehicle delivering wing-hanging nacelle |
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| CN106882387A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | The landing mode and its device of a kind of aircraft |
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| CN109018349A (en) * | 2018-08-10 | 2018-12-18 | 侯志强 | A kind of multi-rotor unmanned aerial vehicle system suitable for stablizing dispensing under the conditions of high-speed flight |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020066825A1 (en) * | 2000-04-13 | 2002-06-06 | Miralles Carlos T. | Payload delivery system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101988813A (en) * | 2009-07-31 | 2011-03-23 | 三菱重工业株式会社 | Launching system and launching apparatus |
| CN106882387A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | The landing mode and its device of a kind of aircraft |
| CN106915444A (en) * | 2017-03-10 | 2017-07-04 | 佛山市神风航空科技有限公司 | A kind of combined type aircraft lifting gear and mode |
| CN109018349A (en) * | 2018-08-10 | 2018-12-18 | 侯志强 | A kind of multi-rotor unmanned aerial vehicle system suitable for stablizing dispensing under the conditions of high-speed flight |
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| CN110937111A (en) | 2020-03-31 |
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