CN206782019U - It is a kind of can VTOL the amphibious airship of air-sea - Google Patents
It is a kind of can VTOL the amphibious airship of air-sea Download PDFInfo
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- CN206782019U CN206782019U CN201720506566.0U CN201720506566U CN206782019U CN 206782019 U CN206782019 U CN 206782019U CN 201720506566 U CN201720506566 U CN 201720506566U CN 206782019 U CN206782019 U CN 206782019U
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Abstract
The utility model discloses it is a kind of can VTOL the amphibious airship of air-sea, including the hull with deck, hull both sides be symmetrically installed wing, be installed on the vertical fin and horizontal tail of hull afterbody;Rotor driver is separately installed with the wing of both sides, it includes engine nacelle and propeller, and rotor driver can make 0 90 degree of pitching around wing and vert;The propeller includes propeller hub and being uniformly distributed along the circumference and is connected in the blade on propeller hub, blade by hinge with propeller hub, and blade can 0 90 degree of around hinge folding and abut in around engine nacelle;Fold mechanism is provided with wing, the foldable connection of outer wing and interior wing is realized by fold mechanism;Propeller storage cabin is provided with below the wing of the hull both sides, for the rotor driver under folded for storage.The utility model has the dual-use function of yacht and aircraft concurrently, by the lift system that can be verted and fold realize can VTOL at any time, greatly reduce the use limitation of seaplane, economical and practical, flexibility and reliability.
Description
Technical field
The present invention relates to it is a kind of can VTOL the amphibious airship of air-sea, belong to multifunctional traffic means field.
Background technology
Due to landform and the diversity and complexity of traffic, the single vehicles of function can not meet people
Demand, the single vehicles of function also result in the serious wasting of resources, and these problems are required for new, multi-functional
The vehicles solve, seaplane also just application and give birth to, it is the aircraft that can be taken off, land and berth on the water surface, existing
Seaplane be divided to and be divided into two kinds of wing combination hull formula or wing combination float-type substantially, filled on hull or floating drum retractable
Undercarriage, receive during landing, put down by land during landing on the water.Although it solves the single vehicles to a certain extent
Limitation, but be the shortcomings that seaplane need taken off on the water surface, without VTOL at any time across the sea
Function, practicality is poor.
Therefore, need to design it is a kind of can VTOL the amphibious airship of air-sea, can be in the vast river in waters, lake, river, seawater face
Upper use, security is good, and ground auxiliary equipment is more economical;Militarily, it is possible to achieve transport goods and materials, wounded's rescue, sea in battlefield
It is upper forced landing, antisubmarine, scout, search, need not by carriers such as aircraft carriers, can carry out other aircrafts can not the work(such as special assignment
Can, scouting strategy, defence policies, strategy and tactics to future battlefield etc. produce significant innovation, have widely military, civilian etc.
Purposes.
The content of the invention
Goal of the invention:In order to overcome the deficiencies in the prior art, the present invention provide it is a kind of can VTOL air-sea
Amphibious airship, there is simple in construction, easy to use, flexibility and reliability, realized by the lift system that can be verted and fold
The VTOL at any time of hull, the use limitation of existing seaplane is substantially reduced, it is economical and practical.
Technical scheme:To achieve the above object, the technical solution adopted by the present invention is:
It is a kind of can VTOL the amphibious airship of air-sea, including the machine that the hull with deck, hull both sides are symmetrically installed
The wing, the vertical fin and horizontal tail for being installed on hull afterbody;
Wherein, rotor driver is separately installed with the wing of both sides, the rotor driver includes engine nacelle and with starting
The connected propeller of machine nacelle, and rotor driver can make the pitching of 0-90 degree around wing and vert;The propeller include propeller hub and
It is uniformly distributed along the circumference in the blade on propeller hub, and propeller hub is rotatablely connected by central rotating shaft and engine nacelle;The blade passes through
Hinge is connected with propeller hub, and blade can around hinge fold 0-90 degree and abut in around engine nacelle;
Fold mechanism is respectively arranged with the wing of both sides, wing is divided into by interior wing and outer wing by fold mechanism, and
The foldable connection of outer wing and interior wing is realized by fold mechanism;Propeller is provided with below the wing of the hull both sides to deposit
Cabin is stored up, for the rotor driver under folded for storage.
On the one hand, roomy hull provides the buoyancy that airship is docked on the water surface, and by be arranged on wing two secondary rotations
Power of the wing as advance, the rotor blade of lift system is folded in around engine nacelle when berthing, while by wing
Portion's mechanical structure makes wing-folding greatly reduce volume, on the other hand, two secondary rotors on wing can be with hair to hull interior
Motivation cockpit verts 90 degree, so as to overcome the gravity of airship and it is preceding winged when resistance, VTOL and high speed can be realized
It is preceding to fly, it is that a frame can be at any time from the water surface to aerial special airship.
Preferably, the fold mechanism includes one group of affixed side hydraulic stem being connected with interior wing, one group and outer wing phase
Folded sides hydraulic stem, one group of A-frame and the pole being fixed on interior wing outer face even, and affixed side hydraulic stem, folding
Side hydraulic stem mutually corresponds with A-frame;One summit of the A-frame is socketed on pole, its another top
Point is hinged and connected by first connecting rod with the telescopic end of corresponding affixed side hydraulic stem, its last summit by second connecting rod and
The telescopic end of corresponding folded sides hydraulic stem is hinged and connected.Simple in construction, easy to connect, control is reliable.
Preferably, fuel oil-cell hybrid power system is disposed with the hull, and covered with solar recharging on hull
Plate, it can be that battery pack charges, meet field immediate operational readiness demand while energy-conserving and environment-protective.
Preferably, sound wave interference unit is installed at the top of the propeller hub, by analyzing noise frequency caused by airship, so as to produce
Raw corresponding interference sound wave offsets therewith.
Preferably, driving cabin, underground cabin are provided with the hull, and chaise longue is disposed with deck, the airship has
The repertoire of yacht, it can carry out shining the recreations such as sunbath.
Beneficial effect:It is provided by the invention it is a kind of can VTOL the amphibious airship of air-sea, relative to prior art, have
Advantages below:1st, have the dual-use function of yacht and aircraft concurrently, hull is realized by the lift system that can be verted and fold
Can VTOL at any time, greatly reduce the use limitation of seaplane, it is economical and practical, it is flexible and changeable, securely and reliably;2nd, with
Supplementary energy of the solar energy as airship, available for the side such as the illuminator of airship, control loop, air-conditioning system and Aided Machine
Face, meet field immediate operational readiness demand while energy-conserving and environment-protective;3rd, using advanced noise reduction technology, to meet the wars such as antisubmarine, scouting
Slightly need, there is the widely purposes such as military, civilian.
Brief description of the drawings
Fig. 1 is the internal structure schematic diagram of the embodiment of the present invention;
Fig. 2 is the structural representation of propeller in the present invention;
Fig. 3 is the structural representation of fold mechanism in the present invention;
Fig. 4 is the structural representation of the embodiment of the present invention in a folded configuration;
Figure includes:1st, deck, 2, hull, 3, wing, 4, vertical fin, 5, horizontal tail, 6, engine nacelle, 7, propeller, 8,
Propeller hub, 9, blade, 10, central rotating shaft, 11, hinge, 12, propeller storage cabin, 13, affixed side hydraulic stem, 14, folded sides hydraulic pressure
Bar, 15, A-frame, 16, pole, 17, first connecting rod, 18, second connecting rod, 19, driving cabin, 20, underground cabin, 21, chaise longue,
22nd, stair, 23, interior wing, 24, outer wing.
Embodiment
The present invention is further described below in conjunction with the accompanying drawings.
As shown in Figure 1 for it is a kind of can VTOL the amphibious airship of air-sea, including the hull 2 with deck 1,2 liang of hull
Wing 3 that side is symmetrically installed, the vertical fin 4 and horizontal tail 5 for being installed on the afterbody of hull 2;
Wherein, be separately installed with rotor driver on both sides wing 3, the rotor driver include engine nacelle 6 and with hair
The connected propeller 7 of motivation nacelle 6, and rotor driver can make the pitching of 0-90 degree around wing 3 and vert;As shown in Fig. 2 the spiral shell
Rotation oar 7 includes propeller hub 8 and is uniformly distributed along the circumference in the blade 9 on propeller hub 8, and propeller hub 8 passes through central rotating shaft 10 and engine nacelle 6
Rotation connection;The blade 9 is connected by hinge 11 with propeller hub 8, and blade 9 can around hinge 11 fold 0-90 degree and abut in hair
Around motivation nacelle 6;
Fold mechanism is respectively arranged with both sides wing 3, is divided wing 3 for interior wing 23 and outer wing by fold mechanism
24, and pass through the foldable connection of the outer wing 24 of fold mechanism realization and interior wing 23;The lower section of 2 both sides wing of hull 3 is set
Propeller storage cabin 12 is equipped with, for the rotor driver under folded for storage.
As shown in figure 3, the fold mechanism includes 13, one groups of one group of affixed side hydraulic stem being connected with interior wing 23 and outside
Connected 14, the one groups of A-frames 15 of folded sides hydraulic stem of wing 24 and the pole 16 being fixed on the interior outer face of wing 23, and
Affixed side hydraulic stem 13, folded sides hydraulic stem 14 and A-frame 15 mutually correspond;One top of the A-frame 15
Point is socketed on pole 16, and its another summit is hinged phase by first connecting rod 17 with the telescopic end of corresponding affixed side hydraulic stem 13
Even, its last summit is hinged and connected by second connecting rod 18 with the telescopic end of corresponding folded sides hydraulic stem 14.
In the present embodiment, fuel oil-cell hybrid power system is disposed with the hull 2, it includes being arranged under deck
The fuel tank and energy-storage battery of side, the fuel tank are started by the pipeline being arranged in wing 3 with the turbine wheel shaft in engine nacelle 6
Machine is connected, and covered with the solar charging panel being connected with energy-storage battery on hull 2, illuminator, driving available for airship
System, air-conditioning system and Aided Machine etc..
In the present embodiment, the top of propeller hub 8 is provided with sound wave interference unit, by analyzing noise frequency caused by airship,
So as to which the interference sound wave for producing corresponding offsets therewith;Be provided with the hull 2 driving cabin 19, underground cabin 20 and up and down
Stair 22, and chaise longue 21 is disposed with deck 1.
The embodiment of the present invention is as follows:
Under grown form, the airship has the repertoire of yacht, can carry out shining the recreations such as sunbath, in the water surface
It is upper to be pushed ahead by two secondary rotor drivers as power;As shown in figure 4, it can arrive wing-folding by fold mechanism when berthing
Hull interior, to reduce space-consuming;It is that a frame can be at any time from the water surface to aerial special airship simultaneously, use can vert 0-
90 degree of two secondary rotors fly as lift system and the power to advance before can realizing VTOL and high speed.
During rotor normal work, blade 9 and propeller hub 8 synchronously rotate around central rotating shaft 10, when blade 9 needs to fold, oar
Leaf can around hinge fold 0-90 degree, blade is folded in around engine nacelle, to reduce space-consuming.
Control affixed side hydraulic stem 13 to forward extend out during wing-folding, promote first connecting rod 17 to promote A-frame 15 around branch
Bar 16 rotates, and then promotes the rotation of second connecting rod 18, while in the presence of second connecting rod 18, folded sides hydraulic stem 14 is inside
Compression, to realize the folding of outer wing 24, and the rotor driver under folded state is stored by propeller storage cabin 12.It is similarly anti-
The outer wing 24 that can be folded to operation restores to the original state.
Described above is only the preferred embodiment of the present invention, it should be pointed out that:For the ordinary skill people of the art
For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should
It is considered as protection scope of the present invention.
Claims (5)
1. it is a kind of can VTOL the amphibious airship of air-sea, it is characterised in that including hull (2), hull with deck (1)
(2) both sides are symmetrically installed wing (3), the vertical fin (4) and horizontal tail (5) for being installed on hull (2) afterbody;
Wherein, be separately installed with rotor driver on both sides wing (3), the rotor driver include engine nacelle (6) and with hair
The connected propeller (7) of motivation nacelle (6), and rotor driver can make the pitching of 0-90 degree around wing (3) and vert;The propeller
(7) include propeller hub (8) and be uniformly distributed along the circumference in the blade (9) on propeller hub (8), and propeller hub (8) passes through central rotating shaft (10) and hair
Motivation nacelle (6) is rotatablely connected;The blade (9) is connected by hinge (11) with propeller hub (8), and blade (9) can around hinge
(11) fold 0-90 degree and abut in around engine nacelle (6);
Fold mechanism is respectively arranged with both sides wing (3), wing (3) is divided into by interior wing (23) and outer machine by fold mechanism
The wing (24), and outer wing (24) and the foldable connection of interior wing (23) are realized by fold mechanism;Hull (2) both sides machine
Propeller storage cabin (12) is provided with below the wing (3), for the rotor driver under folded for storage.
2. it is according to claim 1 it is a kind of can VTOL the amphibious airship of air-sea, it is characterised in that the fold mechanism
Including one group of affixed side hydraulic stem (13) being connected with interior wing (23), one group of folded sides hydraulic stem being connected with outer wing (24)
(14), one group of A-frame (15) and the pole (16) being fixed on interior wing (23) outer face, and affixed side hydraulic stem (13),
Folded sides hydraulic stem (14) mutually corresponds with A-frame (15);One summit of the A-frame (15) is socketed on branch
On bar (16), its another summit is hinged and connected by first connecting rod (17) with the telescopic end of corresponding affixed side hydraulic stem (13),
Its last summit is hinged and connected by second connecting rod (18) with the telescopic end of corresponding folded sides hydraulic stem (14).
3. it is according to claim 1 it is a kind of can VTOL the amphibious airship of air-sea, it is characterised in that the hull (2)
On be disposed with fuel oil-cell hybrid power system, and covered with solar charging panel on hull (2).
4. it is according to claim 1 it is a kind of can VTOL the amphibious airship of air-sea, it is characterised in that the propeller hub (8)
Top is provided with sound wave interference unit.
5. it is according to claim 1 it is a kind of can VTOL the amphibious airship of air-sea, it is characterised in that the hull (2)
On be provided with driving cabin (19), underground cabin (20), and chaise longue (21) is disposed with deck (1).
Priority Applications (1)
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CN201720506566.0U CN206782019U (en) | 2017-05-09 | 2017-05-09 | It is a kind of can VTOL the amphibious airship of air-sea |
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CN201720506566.0U CN206782019U (en) | 2017-05-09 | 2017-05-09 | It is a kind of can VTOL the amphibious airship of air-sea |
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CN206782019U true CN206782019U (en) | 2017-12-22 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107128443A (en) * | 2017-05-09 | 2017-09-05 | 南京航空航天大学 | It is a kind of can VTOL the amphibious airship of air-sea |
CN108312795A (en) * | 2018-02-05 | 2018-07-24 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind |
CN112520015A (en) * | 2020-11-25 | 2021-03-19 | 常州市长昊机械有限公司 | Convertible aviation folding blade |
-
2017
- 2017-05-09 CN CN201720506566.0U patent/CN206782019U/en active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107128443A (en) * | 2017-05-09 | 2017-09-05 | 南京航空航天大学 | It is a kind of can VTOL the amphibious airship of air-sea |
CN108312795A (en) * | 2018-02-05 | 2018-07-24 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind |
CN108312795B (en) * | 2018-02-05 | 2019-06-11 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | Aerial-underwater paleocinetic amphibious aircraft and sailing method can be achieved in one kind |
CN112520015A (en) * | 2020-11-25 | 2021-03-19 | 常州市长昊机械有限公司 | Convertible aviation folding blade |
CN112520015B (en) * | 2020-11-25 | 2023-06-20 | 常州市长昊机械有限公司 | Convertible aviation folding blade |
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