CN109760816A - A kind of mixed layout dirigible of bandwidth paddle power and vector power device - Google Patents
A kind of mixed layout dirigible of bandwidth paddle power and vector power device Download PDFInfo
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- CN109760816A CN109760816A CN201910184760.5A CN201910184760A CN109760816A CN 109760816 A CN109760816 A CN 109760816A CN 201910184760 A CN201910184760 A CN 201910184760A CN 109760816 A CN109760816 A CN 109760816A
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- 239000007789 gas Substances 0.000 claims description 7
- 239000002775 capsule Substances 0.000 claims description 5
- 239000001307 helium Substances 0.000 claims description 5
- 229910052734 helium Inorganic materials 0.000 claims description 5
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 5
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- 239000006260 foam Substances 0.000 claims description 3
- 230000006641 stabilisation Effects 0.000 claims description 3
- 238000011105 stabilization Methods 0.000 claims description 3
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The invention discloses the mixed layout dirigibles of a kind of bandwidth paddle power and vector power device, including dirigible, the dirigible includes the 2-10 floatage air bag arranged parallel, wide blade power device and duct power device, the floatage air bag central junction line angle of attack is -3 °~15 °, the quantity of the width blade power device is 2-20, and the two sides of floatage air bag are symmetrically mounted on by roof support, the quantity of the duct power device is 2-20, and the two sides of floatage air bag and the tail portion of dirigible are symmetrically mounted on by roof support, dirigible further includes empennage, internal mechanism and air cushion landing gear, wherein, empennage is mounted on the rear portion of floatage air bag, air cushion landing gear is mounted on the bottom of air bag.Wide blade power is combined by the present invention with duct power, while guaranteeing lifting capacity, additionally provides VTOL, the flat control ability for flying hovering, maneuvering flight.
Description
Technical field
The present invention relates to aviation field, the mixed layout of especially a kind of bandwidth paddle power and vector power device flies
Ship.
Background technique
With air transportation industry development, the requirement to aircraft lifting capacity and flexibility is higher and higher, to load-carrying number
Hundred tons, the flexible aircraft of landing be in urgent need, and at present carrier lifting capacity be typically not greater than hundred tons, heavy dependence machine
Field and runway.Dirigible has natural heavy-duty advantage using the self weight lift-off of helium buoyancy overcoming, in particular by it is pneumatic rise with
The novel airship that buoyancy combines becomes one of the solution of heavy haul transport, but the novel airship is to flight control, dynamical system
System proposes very high request.Therefore, the invention proposes the combined dynamic system schemes of a kind of wide blade power and duct power
Novel load-carrying dirigible provide VTOL, the flat control energy for flying hovering, maneuvering flight while guaranteeing lifting capacity
Power.
Summary of the invention
In view of the deficiencies of the prior art, the present invention provides the mixing cloth of a kind of bandwidth paddle power and vector power device
Office's dirigible is combined using pneumatic rise with buoyancy, with VTOL, the flat control ability for flying hovering, maneuvering flight.
The present invention solves its technical problem and adopts the following technical solutions to achieve:
A kind of mixed layout dirigible of bandwidth paddle power and vector power device, including dirigible, the dirigible include simultaneously
2-10 floatage air bag of row arrangement, wide blade power device and duct power device, 2-10 floatage air bag central junction line
The angle of attack is -3 °~15 °, and the quantity of the width blade power device is 2-20, and is symmetrically mounted on by the second roof support
The two sides of floatage air bag, the quantity of the duct power device are 2-20, and are symmetrically mounted on by third roof support floating
The two sides of strength capsule and the tail portion that dirigible is symmetrically mounted on by the first roof support.
Preferably, the 2-10 floatage air bag arranged parallel is all made of lower resistance streamlined structure and lateral symmetry, 2-10
A floatage air bag link position is processed using thermal weld, and link position passes through rope net and cord power transmission.
Preferably, helium is filled inside the floatage air bag, the inside of floatage air bag is equipped with balloonet, balloonet and buoyancy
Air bag is connected using thermal weld, and the balloonet is connected with control pressurer system, and air is filled inside balloonet, passes through pressure control
System processed adjusts air inlet amount to adjust the size of balloonet.
Preferably, the wide blade power device includes propeller, blade dynamical system and blade vector system, the spiral shell
Rotation paddle includes 2-6 piece blade, and the aspect ratio range of blade is 10-100；The blade dynamical system uses turbogenerator, work
Piston engine or motor driven；The blade vector system is bowed using uniaxial vector design, controllable dynamical system and propeller
Rotation is faced upward, rotational angle is 110 °~-110 ° of ﹢ on the basis of horizontal line.
Preferably, the duct power device includes duct, duct dynamical system, duct paddle and duct vector system group
At duct is made using composite material foam sandwich construction, and duct dynamical system uses turbogenerator, piston engine
Or motor driven, duct paddle include 2-6 piece blade, duct vector system designed using twin shaft vector, it can be achieved that thrust direction around
Two axis are in 100 °~-100 ° range rotations of ﹢.
Preferably, dirigible further includes empennage, internal mechanism and air cushion landing gear, wherein empennage is mounted on floatage air bag
Rear portion, air cushion landing gear is mounted on the bottom of air bag, gondola be mounted on the lower part of air bag, internal mechanism and floatage air bag and
Gondola is connected.
Preferably, the empennage includes empennage edge strip, the main stabilization of empennage and empennage rudder face, and empennage uses rib covering knot
Structure, main body load-carrying construction are prepared using composite material honeycomb or foamed composite, and empennage rudder face is turned using Aircraft Steering Engine control
It is dynamic.
Compared with prior art, the embodiment of the present invention bring it is following the utility model has the advantages that
1, dirigible includes the 2-10 floatage air bag arranged parallel, and 2-10 floatage air bag is all made of the streamlined knot of lower resistance
Structure and lateral symmetry fills helium inside floatage air bag, and the 2-10 floatage air bag central junction line angle of attack is -3 °~15 °, winged
It can provide lift when flying before ship, wherein the inside of floatage air bag is equipped with balloonet, and air, and balloonet are filled inside balloonet
It is connected with control pressurer system, the size of balloonet is adjusted by control pressurer system adjusting air inlet amount, so as to
It is convenient to adjust lift size.
2, dirigible includes wide blade power device, and the quantity of wide blade power device is 2-20, promotes branch by second
Frame is mounted on floatage air bag two sides, can be used for providing dirigible VTOL and preceding winged active force.
3, dirigible includes duct power device, and the quantity of duct power device is 2-20, and passes through third roof support
It is symmetrically mounted on the two sides of floatage air bag and is symmetrically mounted on the tail portion of dirigible by the first roof support, for being provided to dirigible
Exact posture control force, duct power device include vector system, and duct vector system is designed using twin shaft vector, it can be achieved that pushing away
Power direction is around two axis in 100 °~-100 ° range rotations of ﹢.
4, empennage is mounted on air bag rear portion, it is ensured that the stability flown before dirigible；Internal mechanism and air bag and gondola connect
It connects, carrying and intermal force can be played；Air cushion landing gear is mounted on air bag bottom, can play a supporting role when berthing；It hangs
Cabin is mounted on air bag lower part, can be used for loading ship and carries equipment, cargo and fuel.
Detailed description of the invention
Fig. 1 is the overall structure signal of the mixed layout dirigible of a kind of bandwidth paddle power of the present invention and vector power device
Figure；
Fig. 2 is that culvert device is being just in a kind of bandwidth paddle power of the present invention and the mixed layout dirigible of vector power device
View；
Fig. 3 is air cushion landing gear in a kind of bandwidth paddle power of the present invention and the mixed layout dirigible of vector power device
Structural schematic diagram；
Fig. 4 is wide blade power dress in a kind of bandwidth paddle power of the present invention and the mixed layout dirigible of vector power device
The structural schematic diagram set；
Fig. 5 is the interior of floatage air bag in a kind of bandwidth paddle power of the present invention and the mixed layout dirigible of vector power device
Portion's structural schematic diagram.
In figure: 1, floatage air bag；101, gas chamber；102, air door；103, snorkel；2, empennage；3, first branch is promoted
Frame；4, duct；5, duct paddle；6, the second roof support；7, propeller；701, the first swingle；702, the second swingle；703,
Motor；8, third roof support；9, cord；10, air cushion landing gear.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-5, a kind of embodiment provided by the invention: a kind of bandwidth paddle power and vector power device it is mixed
Layout dirigible, including dirigible are closed, the dirigible includes the 2-10 floatage air bag 1 arranged parallel, wide blade power device and culvert
Road power device, 2-10 floatage air bag 1 are all made of lower resistance streamlined structure and lateral symmetry, the 2-10 company of floatage air bag 1
It connects position to process using thermal weld, and link position passes through 9 power transmission of rope net and cord, fills helium, 2-10 inside floatage air bag 1
A 1 central junction line angle of attack of floatage air bag be -3 °~15 °, before dirigible fly when can provide lift, wherein floatage air bag 1 it is interior
Portion is equipped with balloonet, and balloonet is connected with floatage air bag 1 using thermal weld, and air, and balloonet and pressure are filled inside balloonet
Force control system is connected, and adjusts air inlet amount by control pressurer system to adjust the size of balloonet, so as to convenient
Adjusting lift size；The quantity of the width blade power device can be 2-20, in the present embodiment, wide blade power device
Quantity is 4, and the two sides of floatage air bag 1 are symmetrically mounted on by the second roof support 6, can be used for providing dirigible VTOL
With preceding winged active force, wherein the wide blade power device includes propeller 7, blade dynamical system and blade vector system,
The propeller 7 may include 2-6 piece blade, and in the present embodiment, the blade quantity of propeller 7 is 2, the aspect ratio range of blade
For 10-100；The blade dynamical system uses turbogenerator, piston engine or motor driven；The blade vector system
It is designed using uniaxial vector, can control 7 pitch rotation of dynamical system and propeller, rotational angle is on the basis of horizontal line
110 °~-110 ° of ﹢；The quantity of the duct power device can be 2-20, and in the present embodiment, the quantity of duct power device is
4, and the two sides of floatage air bag 1 are symmetrically mounted on by third roof support 8 and are symmetrically mounted on by the first roof support 3
The tail portion of dirigible, for providing exact posture control force to dirigible, the duct power device includes duct 4, duct dynamical system
System, duct paddle 5 and duct vector system composition, duct 4 are made using composite material foam sandwich construction, duct dynamical system
System uses turbogenerator, piston engine or motor driven, and duct paddle 5 includes 2-6 piece blade, in the present embodiment, duct paddle 5
Blade quantity be 4, duct vector system designed using twin shaft vector, it can be achieved that thrust direction around two axis 100 ° of ﹢~-
100 ° of range rotations；Dirigible further includes empennage 2, internal mechanism and air cushion landing gear 10, wherein empennage 2 is mounted on buoyancy gas
The rear portion of capsule 1, it is ensured that the stability flown before dirigible, air cushion landing gear 10 are mounted on the bottom of air bag, can when berthing
It plays a supporting role, gondola is mounted on the lower part of air bag, and it can be used for loading ship and carry equipment, cargo and fuel, internal mechanism and floating
Strength capsule 1 is connected with gondola, and the empennage 2 includes empennage edge strip, the main stabilization of empennage and empennage rudder face, and empennage 2 uses the wing
Rib stressed-skin construction, main body load-carrying construction are prepared using composite material honeycomb or foamed composite, and empennage rudder face uses aviation rudder
Machine control rotation.
Fig. 4 is a kind of embodiment that invention provides, and wide blade power device includes propeller 7, blade dynamical system and paddle
Leaf vector system, the propeller 7 may include 2-6 piece blade, and in the present embodiment, the blade quantity of propeller 7 is 2, blade
Aspect ratio range be 10-100, the blade dynamical system uses motor driven, and blade vector system is set using uniaxial vector
Meter, first motor 703 drive the rotation of the first swingle 701, and rotational angle is 110 °~-110 ° of ﹢ on the basis of horizontal line,
It is thus achieved that the function of control 7 pitch rotation of propeller, the second swingle 702 can be used for that propeller 7 is driven to rotate.
As shown in figure 5, being equipped with 3 individual gas chambers 101 in the floatage air bag 1 of the present embodiment, it is all provided on each gas chamber 101
There is air door 102, is connected between gas chamber 101 by snorkel 103；Wherein the air door 102 is controlled with pressure
System is connected, for by air door 102 to being filled with air in gas chamber 101.
Working principle: rope net be one kind it is well known, suitable for the load-carrying construction of large scale aviation spacecraft outer surface top surface,
Rope net in the present invention is made of being woven as fibre bundle；Cord 9 is also a kind of common load-carrying construction, including several loads
Item, 9 lining cloth of cord, reversed anti-tear item connect lining cloth with transition, and general load item is connected by heat seal mode and 9 lining cloth of cord
It connects, reversed anti-tear item connect lining cloth heat seal connection with transition again after connecting by heat seal mode with 9 lining cloth of cord；The present invention is logical
It crosses and is processed in 2-10 1 link position of floatage air bag using thermal weld, and made in link position by 9 power transmission of rope net and cord
It obtains dirigible floatage air bag 1 and bears the conformal effect that can achieve inflatable structure when internal pressure；Dirigible can realize the vertical of material equipment
Deliver, can to no harbour, without bridge, without airport, without water surface navigation channel, without land transportation road, the island without boom hoisting, submerged reef, beach
Corresponding material equipment is vertically delivered in painting；When not having landing conditions, can hovering, the corresponding goods and materials of vertical unloading, when having
When landing conditions, can vertical landing, after landing rolling unload goods and materials.
Finally, it should be noted that embodiment described above, only a specific embodiment of the invention, to illustrate the present invention
Technical solution, rather than its limitations, scope of protection of the present invention is not limited thereto, although with reference to the foregoing embodiments to this hair
It is bright to be described in detail, those skilled in the art should understand that: anyone skilled in the art
In the technical scope disclosed by the present invention, it can still modify to technical solution documented by previous embodiment or can be light
It is readily conceivable that variation or equivalent replacement of some of the technical features；And these modifications, variation or replacement, do not make
The essence of corresponding technical solution is detached from the spirit and scope of technical solution of the embodiment of the present invention, should all cover in protection of the invention
Within the scope of.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (7)
1. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device, including dirigible, which is characterized in that described to fly
Ship includes the 2-10 floatage air bag (1) arranged parallel, wide blade power device and duct power device, 2-10 floatage air bag
(1) the central junction line angle of attack is -3 °~15 °, and the quantity of the width blade power device is 2-20, and promotes branch by second
Frame (6) is symmetrically mounted on the two sides of floatage air bag (1), and the quantity of the duct power device is 2-20, and is pushed away by third
The two sides of floatage air bag (1) are symmetrically mounted on into bracket (8) and the tail of dirigible is symmetrically mounted on by the first roof support (3)
Portion.
2. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 1, feature
It is, the 2-10 floatage air bag (1) arranged parallel is all made of lower resistance streamlined structure and lateral symmetry, 2-10 buoyancy gas
Capsule (1) link position is processed using thermal weld, and link position passes through rope net and cord (9) power transmission.
3. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 1, feature
It is, helium is filled inside the floatage air bag (1), and the inside of floatage air bag (1) is equipped with balloonet, balloonet and floatage air bag
(1) it is connected using thermal weld, the balloonet is connected with control pressurer system, and air is filled inside balloonet, passes through pressure control
System processed adjusts air inlet amount to adjust the size of balloonet.
4. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 1, feature
It is, the width blade power device includes propeller (7), blade dynamical system and blade vector system, the propeller (7)
Including 2-6 piece blade, the aspect ratio range of blade is 10-100；The blade dynamical system is sent out using turbogenerator, piston
Motivation or motor driven；The blade vector system can control dynamical system and propeller (7) pitching using uniaxial vector design
Rotation, rotational angle are 110 °~-110 ° of ﹢ on the basis of horizontal line.
5. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 1, feature
It is, the duct power device includes duct (4), duct dynamical system, duct paddle (5) and duct vector system composition, is contained
Road (4) is made using composite material foam sandwich construction, duct dynamical system using turbogenerator, piston engine or
Motor driven, duct paddle (5) include 2-6 piece blade, duct vector system designed using twin shaft vector, it can be achieved that thrust direction around
Two axis are in 100 °~-100 ° range rotations of ﹢.
6. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 1, feature
It is, dirigible further includes empennage (2), internal mechanism and air cushion landing gear (10), wherein empennage (2) is mounted on floatage air bag
(1) rear portion, air cushion landing gear (10) are mounted on the bottom of air bag, and gondola is mounted on the lower part of air bag, internal mechanism and floating
Strength capsule (1) is connected with gondola.
7. the mixed layout dirigible of a kind of bandwidth paddle power and vector power device according to claim 6, feature
It is, the empennage (2) includes empennage edge strip, the main stabilization of empennage and empennage rudder face, and empennage (2) uses rib stressed-skin construction,
Main body load-carrying construction is prepared using composite material honeycomb or foamed composite, and empennage rudder face is using Aircraft Steering Engine control rotation.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910184760.5A CN109760816A (en) | 2019-03-12 | 2019-03-12 | A kind of mixed layout dirigible of bandwidth paddle power and vector power device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910184760.5A CN109760816A (en) | 2019-03-12 | 2019-03-12 | A kind of mixed layout dirigible of bandwidth paddle power and vector power device |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979623A (en) * | 2019-12-13 | 2020-04-10 | 中国特种飞行器研究所 | Near-ground safe landing protection system for airship |
| CN111055989A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Small multi-vector airship |
| CN111846191A (en) * | 2020-07-27 | 2020-10-30 | 重庆交通大学 | Combined power airship |
| CN113562153A (en) * | 2021-08-31 | 2021-10-29 | 合肥工业大学 | Solar power-based air quality monitoring unmanned airship and control method thereof |
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| CN113562153A (en) * | 2021-08-31 | 2021-10-29 | 合肥工业大学 | Solar power-based air quality monitoring unmanned airship and control method thereof |
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