CN103274046A - Modularized pilotless helicopter for task loads - Google Patents
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- CN103274046A CN103274046A CN 201310154144 CN201310154144A CN103274046A CN 103274046 A CN103274046 A CN 103274046A CN 201310154144 CN201310154144 CN 201310154144 CN 201310154144 A CN201310154144 A CN 201310154144A CN 103274046 A CN103274046 A CN 103274046A
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Abstract
The invention relates to the field of pilotless helicopters, especially to a modularized pilotless helicopter for task loads. The total design of the pilotless helicopter is carried out by taking task loads as a constituent part of the pilotless helicopter. The pilotless helicopter is divided into an upper part flight platform module (1) and a lower part task load module (2); wherein the flight platform module (1) comprises regular basic components of a pilotless helicopter, the regular basic components consisting of a fuselage (101), a rotor system (102), a flight control system (103), a power system (104), a electric power system (105), cables and interfaces (106); the task load module (2) mainly consists of a load cabin (201); and the two modules are rigorous in anastomosis and firm in connection and form an integral pilotless helicopter. The problems that a conventional pilotless helicopter with a limit capacity in a singularity shape cannot be suitable for various kinds of load devices in various sizes and shapes is solved by the modularized pilotless helicopter for task loads of the invention, and the flexibility of the task load integrated usage and the multitask execution capability of the pilotless helicopter are both improved.
Description
Technical field
The present invention relates to the unmanned plane field, particularly a kind of modularization depopulated helicopter of oriented mission load.
Background technology
In recent years, along with improving constantly of state-of-art, the unmanned plane technology constantly develops.Unmanned plane can be divided into fixed-wing and rotor two big classes, and the former is the present main flow of unmanned plane in the world, and the latter is because its technology content is higher, and the design and fabrication technology of unmanned plane has been proposed bigger challenge.The important difference of unmanned plane and model plane is: the latter only pays close attention to its airworthiness, belongs to motion and amusing products; What the former then paid close attention to is the load that can carry, and finishes the task of appointment, is a kind of task and job platform.Functions such as depopulated helicopter has vertical takeoff and landing, hovers, low speed and close-target flight have wide application potential at civil area.
For the general design of depopulated helicopter, people's thinking comes from both direction usually: the one, and the air equipment builder of specialty mostly is the design concept that is replaced the aviator by flight control system; The 2nd, model plane design and fan trend towards model amplification and integration more.These two kinds of design concepts all are primarily focused on the airworthiness aspect, and the practical application purpose of depopulated helicopter is ignored to some extent.Depopulated helicopter is as a task platform, and except airworthiness, most important function is to carry different mission payloads to carry out operation.In existing depopulated helicopter design, mission payload and aircraft do not have direct correlation, usually hang to realize that by the outside mission payload carries.Because mission payload size, size, shape and vary in weight, and when unmanned helicopter flight, need consider corresponding center of gravity counterweight problem, so it is comparatively loaded down with trivial details that existing this outer hanging method makes task implement, the probability of makeing mistakes is higher, also causes the infringement of equipment easily.
Summary of the invention
The technical problem to be solved in the present invention is existing depopulated helicopter load cabin shape and finite capacity, can't be suitable for the loading device of various variety classeses, different size and shape, simultaneously, the outside hanging method of mission payload is implemented complexity, complex operation, error rate height, equipment rapid wear.
The present invention is that the technical scheme that solves the problems of the technologies described above is: the general design that mission payload is carried out depopulated helicopter as the component part of depopulated helicopter, depopulated helicopter is divided into top flying platform module 1 and bottom mission payload module 2, comprise in the flying platform module 1 by fuselage 101, rotor system 102, flight control system 103, power system 104, electric system 105, the conventional basic module of depopulated helicopter that cable and interface 106 are formed, mission payload module 2 mainly is made up of a load cabin 201, two modules are tightly coincide, firmly connect, form whole depopulated helicopter.
One cover is installed in mission payload module 2 or is overlapped mission payload equipment or system, additional fuel tank 202 or emergency battery 203, mass 204 more, mission payload module 2 is carried out independent design and counterweight according to shape, size, weight and the application characteristic of load.By mission requirements, additional fuel tank 202 and emergency battery 203 can be used for improving the flying power of depopulated helicopter.Mass 204 is used for regulating the body nodal point counterweight, increases the flight stability of depopulated helicopter.
A kind of flying platform module 1 can be used with multiple difform mission payload module 2.A kind of mission payload module 2 also can be used with the flying platform module 1 of multiple different performance.
The modularization depopulated helicopter of a kind of oriented mission load of the present invention also comprises an alighting gear 4, and alighting gear 4 can be installed on the framework of flying platform module 1, also can be installed on the framework of mission payload module 2.Described alighting gear 4 is standing height or adopts the adjustable-height structure.
The modularization depopulated helicopter of a kind of oriented mission load of the present invention, described flight control system 103 and electric system 105 will provide unified standard interface, be connected with corresponding mission payload, realize power supply and data between the two, instruction transmission.
Beneficial effect of the present invention comprises:
(1) the modularization depopulated helicopter of a kind of oriented mission load of the present invention, mission payload is considered as the component part of depopulated helicopter is in addition whole, be divided into flying platform module 1 with depopulated helicopter conventional structure and towards the mission payload module 2 of loading device, when depopulated helicopter is carried out different task, can be by changing the demand that mission payload module 2 satisfies different task.
(2) the modularization depopulated helicopter of a kind of oriented mission load of the present invention, be devoted to the independent design of unmanned helicopter flight console module 1 and mission payload module 2, globality after pursuing it and integrating has improved comprehensive alerting ability and the popularity of using of mission payload, and has been convenient to install.
(3) the modularization depopulated helicopter of a kind of oriented mission load of the present invention, a kind of flying platform module 1 can be used with multiple-task load module 2, conversely, a kind of mission payload module 2 can be used with multiple flying platform module 1 again, thereby realized that a tractor serves several purposes of depopulated helicopter and multimachine are used in combination, improved the multitask executive capability of depopulated helicopter, made that the application of depopulated helicopter is more economical.
(4) the modularization depopulated helicopter of a kind of oriented mission load of the present invention; mission payload module 2 is component parts of depopulated helicopter; and sealing also provides standard interface; can effectively protect mission payload equipment thus; and the normal operation of support equipment; be convenient to realize the center of gravity counterweight, in the hope of reaching flight optimization efficient.
(5) the modularization depopulated helicopter of a kind of oriented mission load of the present invention is realized the depopulated helicopter structural module, breaks the whole up into parts, and is convenient to carrying and transportation.
Description of drawings
Fig. 1 is the structural representation of the modularization depopulated helicopter of a kind of oriented mission load of the present invention.
Fig. 2 is the depopulated helicopter overall schematic of embodiments of the invention one and embodiment two.
Fig. 3 is embodiments of the invention one decomposition module scheme drawings.
Fig. 4 is embodiments of the invention two decomposition module scheme drawings.
Fig. 5 is embodiments of the invention three decomposition module scheme drawings.
Fig. 6 is the depopulated helicopter overall schematic of embodiments of the invention three.
Fig. 7 is interchangeable flying platform module 1 scheme drawing.
The specific embodiment
The modularization depopulated helicopter of a kind of oriented mission load of the present invention is divided into flying platform module 1 and mission payload module 2 two parts, as shown in Figure 1, flying platform module 1 comprises the conventional element of depopulated helicopters such as fuselage 101, rotor system 102, flight control system 103, power system 104, electric system 105, cable and interface 106.Mission payload module 2 mainly is made up of a load cabin 201, is used for carrying a cover or overlaps mission payload equipment or system more; One or more additional fuel tanks 202 or emergency battery 203 can also be installed as required, be used for promoting the flying power of depopulated helicopter; In case of necessity, mass 204 can also be installed and carry out center of gravity of airplane counterweight.Alighting gear 4 can be installed on the framework of flying platform module 1, also can be installed on the framework of mission payload module 2.Flying platform module 1 can be by fixedly buckle, screw or other anchor fittings 3 tightly coincide, firmly are connected with mission payload module 2.
The modularization depopulated helicopter of a kind of oriented mission load of the present invention, the loading device situation design that the shape of mission payload module 2 and big I are carried as required.When the equipment of needs lift-launch more maybe needed to carry a plurality of equipment, mission payload module 2 can design to such an extent that the space is big; The equipment that carries when needs hour, mission payload module 2 can design to such an extent that the space is smaller.The shape of mission payload module 2 can be diversified, as semiellipsoid, cube, many curved bodies, centrum or other irregular fabricate block shapes.
Embodiment one:
The integral structure of depopulated helicopter as shown in Figure 2, flying platform module 1 adopts the rotor system 102 of the staggered form bispin wing, mission payload module 2 adopts oval section structure.Fig. 3 is the decomposition module scheme drawing, and alighting gear 4 is installed on the framework of flying platform module 1, and alighting gear 4 is the design of adjustable-height formula, according to the height of the height adjustment alighting gear 4 of mission payload module 2.
Embodiment two:
The integral structure of depopulated helicopter as shown in Figure 2, flying platform module 1 adopts the rotor system 102 of the staggered form bispin wing, mission payload module 2 adopts oval section structure.Fig. 4 is the decomposition module scheme drawing, and alighting gear 4 is installed on the framework of mission payload module 2, and alighting gear 4 is the design of adjustable-height formula, according to the height of the height adjustment alighting gear 4 of mission payload module 2.
Embodiment three:
The integral structure of depopulated helicopter as shown in Figure 6, flying platform module 1 is identical with the flying platform module 1 among the embodiment one, mission payload module 2 is changed into shape as shown in Figure 5, has further increased load capacity.Alighting gear 4 is installed on the framework of mission payload module 2, is the adjustable-height structure.
A kind of flying platform module 1 can be used with multiple different mission payload module 2, similarly, a kind of mission payload module 2 can be used with multiple different flying platform module 1, has improved the multiple task ability of depopulated helicopter thus, has widened its application category.
Though above invention has been described according to various certain embodiments, the invention is not restricted to this, those skilled in the art can carry out various modifications according to principle of the present invention.Therefore every modification of carrying out according to principle of the present invention all is construed as and is included in protection scope of the present invention.
Claims (10)
1. the modularization depopulated helicopter of an oriented mission load, it is characterized in that: constituted by the flying platform module (1) on top and the mission payload module (2) of bottom, comprise the conventional basic module of the depopulated helicopter of being formed by fuselage (101), rotor system (102), flight control system (103), power system (104), electric system (105), cable and interface (106) in the flying platform module (1), mission payload module (2) mainly is made up of a load cabin (201), two modules are tightly coincide, are firmly connected, and form whole depopulated helicopter.
2. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: a cover is installed in mission payload module (2) or is overlapped mission payload equipment or system, additional fuel tank (202) or emergency battery (203), mass (204) more, mission payload module (2) is carried out independent design and counterweight according to shape, size, weight and the application characteristic of load.
3. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: flying platform module (1) can be replaced according to the demand of task.
4. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: flying platform module (1) can be by fixedly buckle, screw or other anchor fittings (3) tightly coincide, firmly are connected with mission payload module (2).
5. according to the modularization depopulated helicopter of claim 1,2,3 or 4 described a kind of oriented mission load, it is characterized in that: a kind of flying platform module (1) can be used with multiple difform mission payload module (2).
6. according to the modularization depopulated helicopter of claim 1,2,3 or 4 described a kind of oriented mission load, it is characterized in that: a kind of mission payload module (2) can be used with the flying platform module (1) of multiple different performance.
7. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: also comprise an alighting gear (4), alighting gear (4) is installed on the framework of flying platform module (1).
8. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: also comprise an alighting gear (4), alighting gear (4) is installed on the framework of mission payload module (2).
9. according to the modularization depopulated helicopter of claim 7 or 8 described a kind of oriented mission load, it is characterized in that: described alighting gear (4) is for standing height or adopt the adjustable-height structure.
10. the modularization depopulated helicopter of a kind of oriented mission load according to claim 1, it is characterized in that: described flight control system (103) and electric system (105) will provide unified standard interface, be connected with corresponding mission payload, realize power supply and data between the two, instruction transmission.
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| CN 201310154144 CN103274046A (en) | 2013-04-28 | 2013-04-28 | Modularized pilotless helicopter for task loads |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103823380A (en) * | 2014-03-14 | 2014-05-28 | 北京航空航天大学 | Helicopter overall design method based on consideration of flying quality |
| CN104176261A (en) * | 2014-09-12 | 2014-12-03 | 深圳市创新智慧港有限公司 | Remote aerial photography device with self-control performance |
| WO2015039362A1 (en) * | 2013-09-18 | 2015-03-26 | 林日壮 | Flying toy vehicle |
| CN105882988A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Quick dismounting and mounting design scheme for load and body of small unmanned aerial vehicle |
| CN106143886A (en) * | 2015-03-25 | 2016-11-23 | 北京天翼合创科技发展有限公司 | One can be disintegrated formula multi-rotor aerocraft |
| CN107422742A (en) * | 2017-08-16 | 2017-12-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multifunctional service Towed bird system |
| CN108454878A (en) * | 2018-04-28 | 2018-08-28 | 成都致冠科技有限公司 | A kind of assembly method of Modularized unmanned helicopter |
| CN108528693A (en) * | 2018-05-25 | 2018-09-14 | 张博 | Manned equipment |
| 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 |
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
-
2013
- 2013-04-28 CN CN 201310154144 patent/CN103274046A/en active Pending
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015039362A1 (en) * | 2013-09-18 | 2015-03-26 | 林日壮 | Flying toy vehicle |
| CN103823380A (en) * | 2014-03-14 | 2014-05-28 | 北京航空航天大学 | Helicopter overall design method based on consideration of flying quality |
| CN103823380B (en) * | 2014-03-14 | 2017-01-18 | 北京航空航天大学 | Helicopter overall design method based on consideration of flying quality |
| CN104176261A (en) * | 2014-09-12 | 2014-12-03 | 深圳市创新智慧港有限公司 | Remote aerial photography device with self-control performance |
| CN105882988A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Quick dismounting and mounting design scheme for load and body of small unmanned aerial vehicle |
| CN106143886A (en) * | 2015-03-25 | 2016-11-23 | 北京天翼合创科技发展有限公司 | One can be disintegrated formula multi-rotor aerocraft |
| CN106143886B (en) * | 2015-03-25 | 2018-11-06 | 北京天翼合创科技发展有限公司 | One kind can disintegrate formula multi-rotor aerocraft |
| 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 |
| CN107422742A (en) * | 2017-08-16 | 2017-12-01 | 广东容祺智能科技有限公司 | A kind of unmanned plane multifunctional service Towed bird system |
| CN108454878A (en) * | 2018-04-28 | 2018-08-28 | 成都致冠科技有限公司 | A kind of assembly method of Modularized unmanned helicopter |
| CN108528693A (en) * | 2018-05-25 | 2018-09-14 | 张博 | Manned equipment |
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
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Application publication date: 20130904 |