CN109878693A - A kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles - Google Patents
A kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles Download PDFInfo
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- CN109878693A CN109878693A CN201910255024.4A CN201910255024A CN109878693A CN 109878693 A CN109878693 A CN 109878693A CN 201910255024 A CN201910255024 A CN 201910255024A CN 109878693 A CN109878693 A CN 109878693A
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- 239000007787 solid Substances 0.000 title claims abstract description 35
- 239000004744 fabric Substances 0.000 claims abstract description 25
- 239000001307 helium Substances 0.000 claims abstract description 6
- 229910052734 helium Inorganic materials 0.000 claims abstract description 6
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 6
- 230000008878 coupling Effects 0.000 claims description 24
- 238000010168 coupling process Methods 0.000 claims description 24
- 238000005859 coupling reaction Methods 0.000 claims description 24
- 230000007246 mechanism Effects 0.000 claims description 4
- 239000010408 film Substances 0.000 claims 3
- 238000009434 installation Methods 0.000 claims 1
- 239000010409 thin film Substances 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 230000009466 transformation Effects 0.000 abstract description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000000386 athletic effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 241000255777 Lepidoptera Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
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Abstract
The invention discloses a kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles, including ship cloth, rotor and solar film battery plate, the inside of the ship cloth is equipped with framework type ship lid, it and is to be fixedly connected between framework type ship lid and ship cloth, the rotor is fixed on the outside of framework type ship lid, and vane is connected with above rotor, it is to be flexibly connected between the rotor and vane, the solar film battery plate is placed in the top of ship cloth, ship carrying platform is connected with below the framework type ship lid, and it is fixed with helium at the top of ship carrying platform and fills air extractor and charge and discharge power supply system automatically, horizontal Solid rocket engine duct is installed on the outside of the ship carrying platform.The two ducts Solid rocket engine quadrotor solar energy butterfly variant dirigible is provided with connecting rod, framework type ship cover connecting rod and framework type ship lid connecting rod and improves the lift of dirigible so that the shape of dirigible is able to carry out transformation, fall when in use so as to avoid dirigible.
Description
Technical field
The present invention relates to aircraft technical field, specially a kind of two duct Solid rocket engine quadrotor solar energy butterfly variants
Dirigible.
Background technique
The cruising ability of traditional pure electric aviation aircraft excessively relies on battery, is limited to current battery technology development bottleneck
Restriction, cause the problem that current pure electric aircraft generally existing cruise duration is short, be unable to satisfy the needs of current aerial mission,
And the further genralrlization of its use scope is hindered, though dirigible has a long-endurance advantage, traditional dirigible wind resistance is poor,
The factors such as understeer work limit the use of dirigible.
Pure electric aircraft cruise duration in the market is short, anti-crash ability is poor and dirigible wind resistance is poor, influences user
Usage experience, for this purpose, it is proposed that a kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles.
Summary of the invention
The purpose of the present invention is to provide a kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles, to solve
Pure electric aircraft cruise duration mentioned above in the background art is short, anti-crash ability is poor and dirigible wind resistance is poor, influences to make
The problem of usage experience of user.
To achieve the above object, the invention provides the following technical scheme: a kind of two duct Solid rocket engine quadrotor solar energy
Butterfly variant dirigible, including ship cloth, rotor and solar film battery plate, the inside of the ship cloth are equipped with framework type ship lid,
And to be fixedly connected between framework type ship lid and ship cloth, the rotor is fixed on the outside of framework type ship lid, and the top of rotor
It is connected with vane, is flexibly connected between the rotor and vane, the solar film battery plate is placed in the top of ship cloth,
Ship carrying platform is connected with below the framework type ship lid, and be fixed at the top of ship carrying platform helium fill automatically air extractor and
Charge and discharge power supply system is equipped with horizontal Solid rocket engine duct, the inside of the framework type ship lid on the outside of the ship carrying platform
It is mounted with framework type ship lid screw rod slide, and to be fixedly connected between framework type ship lid and framework type ship lid screw rod slide, it is described
Motor cabinet is installed on the inside of framework type ship lid screw rod slide, and is that activity connects between motor cabinet and framework type ship lid screw rod slide
It connects.
Preferably, it is fitted closely between the bottom of the solar film battery plate and the outside of ship cloth, and solar energy is thin
Bonding connection between film battery plate and ship cloth.
Preferably, there are two the horizontal Solid rocket engine duct settings, and its outside for being evenly distributed in ship carrying platform,
It and is to be fixedly connected between horizontal Solid rocket engine duct and framework type ship lid.
Preferably, the framework type ship lid screw rod slide include middle connecting rod, connecting rod ship and resell on another market, connecting rod, framework type ship cover connecting rod
It ships and resell on another market, framework type ship cover connecting rod, framework type ship lid connecting rod are shipped and resell on another market, framework type ship lid connecting rod and framework type ship lid are shipped and resell on another market, institute
It states and is connected with middle connecting rod on the outside of framework type ship lid screw rod slide, and the outside at the top of middle connecting rod is fixed with connecting rod and ships and resell on another market, it is described
The outside that connecting rod is shipped and resell on another market is connected with connecting rod, and is fixed with framework type ship cover connecting rod on the outside of connecting rod and ships and resell on another market, the connecting rod ship and resell on another market with
To be flexibly connected between connecting rod, the outside that the framework type ship cover connecting rod is shipped and resell on another market is equipped with framework type ship cover connecting rod, and framework type
It is connected with framework type ship lid connecting rod on the outside of ship cover connecting rod to ship and resell on another market, the framework type ship cover connecting rod is shipped and resell on another market to be connected with framework type ship lid
To be flexibly connected between bar, the outside that the framework type ship lid connecting rod is shipped and resell on another market is connected with framework type ship lid connecting rod, and framework
It is connected with framework type ship lid on the outside of formula ship lid connecting rod to ship and resell on another market, the framework type ship lid connecting rod is shipped and resell on another market to be connected with framework type ship lid
To be flexibly connected between hack lever, the connecting rod is shipped and resell on another market by connecting rod and constitutes rotational structure, and framework type ship cover connecting rod with middle connecting rod
It is shipped and resell on another market by framework type ship cover connecting rod and constitutes rotational structure with connecting rod, and framework type ship lid connecting rod is connected by framework type ship lid
Hack lever, which is shipped and resell on another market, constitutes rotational structure, and connecting rod, framework type ship cover connecting rod and framework type ship lid frame linking with framework type ship cover connecting rod
The slewing area of bar is 0-178 °.
Preferably, the motor cabinet includes motor, motor flap, bolt, shaft coupling and screw rod, the inside of the motor cabinet
Motor is installed, and motor flap is installed at the top of motor, the top of the motor flap through there is a bolt, the bolt it is interior
Side is mounted with shaft coupling, and screw rod is mounted on the inside of shaft coupling, is fixedly connected between the shaft coupling and motor flap, and
To be fixedly connected between shaft coupling and screw rod, the screw rod constitutes drive mechanism by shaft coupling and motor, and motor passes through electricity
Base lid and motor cabinet constitute detaching structure.
It preferably, is nested structure between the framework type ship lid screw rod slide and screw rod, and framework type ship lid screw rod is sliding
Seat constitutes lifting structure by middle connecting rod and motor cabinet.
Compared with prior art, the beneficial effects of the present invention are:
1, the two ducts Solid rocket engine quadrotor solar energy butterfly variant dirigible is provided with solar film battery plate, passes through
The use of solar film battery plate can allow dirigible to be flown for a long time, reduce dependence of the unmanned plane to battery, from
And the weight that dirigible takes off is alleviated, dirigible is more smoothly taken off, and then increase substantially the continuation of the journey of dirigible
Ability can be improved the stability of airship flight, reduce dirigible by being applied in combination for horizontal Solid rocket engine duct and rotor
The possibility fallen when flight, comes to harm so as to avoid dirigible, improves the service life of dirigible；
2, the two ducts Solid rocket engine quadrotor solar energy butterfly variant dirigible be provided with connecting rod, framework type ship cover connecting rod and
Framework type ship lid connecting rod, by the use of connecting rod, framework type ship cover connecting rod and framework type ship lid connecting rod, so that the shape of dirigible
Shape is able to carry out transformation, improves the lift of dirigible, falls when in use so as to avoid dirigible, and because increases
The area of kayak body falls when avoiding airship flight so can be improved the wind resistance of dirigible；
3, the two ducts Solid rocket engine quadrotor solar energy butterfly variant dirigible is provided with two-way motor and shaft coupling, leads to
The use for crossing two-way motor and shaft coupling enables the flight of dirigible more steady, avoid dirigible because lift not
It falls enough in flight, the possibility of accident occurs when to reducing airship flight, improve the stability that flight uses.
Detailed description of the invention
Fig. 1 is complete structure schematic diagram in the case of the variant of dirigible part of the present invention；
Fig. 2 is skeleton structure schematic diagram in the case of the variant of dirigible part of the present invention；
Fig. 3 is link mechanism schematic diagram in the present invention；
Fig. 4 is motor cabinet structural schematic diagram of the present invention.
In figure: 1, ship cloth；2, rotor；3, vane；4, framework type ship lid；5, solar film battery plate；6, ship carrying platform；
7, helium fills air extractor and charge and discharge power supply system automatically；8, horizontal Solid rocket engine duct；9, framework type ship lid screw rod slide；
901, middle connecting rod；902, connecting rod is shipped and resell on another market；903, connecting rod；904, framework type ship cover connecting rod is shipped and resell on another market；905, framework type ship cover connecting rod；
906, framework type ship lid connecting rod is shipped and resell on another market；907, framework type ship lid connecting rod；908, framework type ship lid is shipped and resell on another market；10, motor cabinet；
1001, motor；1002, motor flap；1003, bolt；1004, shaft coupling；1005, screw rod.
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.
Fig. 1-4 is please referred to, the present invention provides a kind of technical solution: a kind of two duct Solid rocket engine quadrotor solar energy butterflies
Variant dirigible, including ship cloth 1, rotor 2, vane 3, framework type ship lid 4, solar film battery plate 5, ship carrying platform 6, helium are certainly
It is dynamic to fill air extractor and charge and discharge power supply system 7, horizontal Solid rocket engine duct 8, framework type ship lid screw rod slide 9, middle connecting rod
901, connecting rod ship and resell on another market 902, connecting rod 903, framework type ship cover connecting rod ship and resell on another market 904, framework type ship cover connecting rod 905, framework type ship lid connect
Ship and resell on another market 906, framework type ship lid connecting rod 907, framework type ship lid of hack lever is shipped and resell on another market 908, motor cabinet 10, motor 1001, motor flap
1002, bolt 1003, shaft coupling 1004 and screw rod 1005, the inside of ship cloth 1 are equipped with framework type ship lid 4, and framework type ship lid 4
To be fixedly connected between ship cloth 1, the apex angle range of the framework type ship lid 4 is 98-150 degree, which flies in conjunction with it
The structure of ship is easier manipulation dirigible, and the rotor 2 is fixed on the outside of framework type ship lid 4,4 bottom surface of framework type ship lid half
The length of rotor 2 of the diameter equal to 2 times, the top of rotor 2 are connected with vane 3, are flexibly connected between rotor 2 and vane 3, vane
3 is parallel with rotor 2, the movement in the vertical direction of the rotor 2 on vane 3 and variable hull control dirigible, solar energy film
Solar panel 5 is placed in the top of ship cloth 1, fits closely between the bottom of solar film battery plate 5 and the outside of ship cloth 1, and
Bonding connection between solar film battery plate 5 and ship cloth 1, by the use of solar film battery plate 5, can allow dirigible into
The prolonged flight of row, reduces dependence of the unmanned plane to battery, to alleviate the weight that dirigible takes off, enables dirigible
It more smoothly takes off, and then increases substantially the cruising ability of dirigible；The lower section of framework type ship lid 4 is connected with ship carrying platform
6, and the top of ship carrying platform 6 is fixed with helium and fills air extractor and charge and discharge power supply system 7, the outside of ship carrying platform 6 automatically
Horizontal Solid rocket engine duct 8 is installed, there are two the horizontal settings of Solid rocket engine duct 8, and it is evenly distributed in ship carrying platform 6
Outside, and to be fixedly connected between horizontal Solid rocket engine duct 8 and framework type ship lid 4, horizontal Solid rocket engine duct 8 is transported
Row drives dirigible to retreat, and by being applied in combination for horizontal Solid rocket engine duct 8 and rotor 3, can be improved airship flight
Stability reduces the possibility fallen when airship flight, comes to harm so as to avoid dirigible, improves the use of dirigible
Service life；
The inside of framework type ship lid 4 is mounted with framework type ship lid screw rod slide 9, and framework type ship lid 4 and framework type ship lid
To be fixedly connected between screw rod slide 9, framework type ship lid screw rod slide 9 include middle connecting rod 901, connecting rod ship and resell on another market 902, connecting rod 903,
Framework type ship cover connecting rod ship and resell on another market 904, framework type ship cover connecting rod 905, framework type ship lid connecting rod ship and resell on another market 906, framework type ship lid company
Hack lever 907 and framework type ship lid ship and resell on another market 908, and connecting rod 903 is identical with framework type ship 905 length of cover connecting rod, framework type ship lid screw rod
The outside of slide 9 is connected with middle connecting rod 901, and the outside at 901 top of middle connecting rod is fixed with connecting rod and ships and resell on another market 902, and connecting rod ships and resell on another market 902
Outside be connected with connecting rod 903, and the outside of connecting rod 903 is fixed with framework type ship cover connecting rod and ships and resell on another market 904, connecting rod ship and resell on another market 902 with
To be flexibly connected between connecting rod 903, ship and resell on another market 904 outside of framework type ship cover connecting rod is equipped with framework type ship cover connecting rod 905, and structure
The outside of posture ship cover connecting rod 905 is connected with framework type ship lid connecting rod and ships and resell on another market 906, and framework type ship cover connecting rod is shipped and resell on another market 904 and structure
Between posture ship cover connecting rod 905 for be flexibly connected, framework type ship lid connecting rod ship and resell on another market 906 outside be connected with framework type ship lid company
Hack lever 907, and the outside of framework type ship lid connecting rod 907 is connected with framework type ship lid and ships and resell on another market 908, framework type ship lid connecting rod turns
To be flexibly connected between pin 906 and framework type ship lid connecting rod 907, connecting rod 903 is shipped and resell on another market 902 and middle 901 structure of connecting rod by connecting rod
At rotational structure, connecting rod 903 and the rotatable angular range of middle connecting rod 901 are 1-89 degree, and the setting of angular range prevents connecting rod
903 is direct mechanical stuck with middle connecting rod 901, and framework type ship cover connecting rod 905 by framework type ship cover connecting rod ship and resell on another market 904 with company
Bar 903 constitutes rotational structure, and framework type ship lid connecting rod 907 is shipped and resell on another market 906 and framework type by framework type ship lid connecting rod
Ship cover connecting rod 905 constitutes rotational structure, and connecting rod 903, framework type ship cover connecting rod 905 and framework type ship lid connecting rod 907
Slewing area is 0-178 °, and dirigible is passed through nitrogen, under the influence of air pressure, connecting rod 903,905 and of framework type ship cover connecting rod
Framework type ship lid connecting rod 907 is holded up, and then ship cloth 1 is strutted, and passes through connecting rod 903, framework type ship cover connecting rod 905 and framework type
The use of ship lid connecting rod 907 improves the lift of dirigible so that the shape of dirigible is able to carry out transformation, so as to avoid flying
Ship falls when in use, and because increasing the area of kayak body, can be improved the wind resistance of dirigible, avoid
It falls when airship flight；
The inside of framework type ship lid screw rod slide 9 is equipped with motor cabinet 10, and motor cabinet 10 and framework type ship lid screw rod are sliding
To be flexibly connected between seat 9, motor cabinet 10 includes motor 1001, motor flap 1002, bolt 1003, shaft coupling 1004 and screw rod
1005, the inside of motor cabinet 10 is equipped with motor 1001, and motor flap 1002 is equipped at the top of motor 1001, motor flap
Through there is bolt 1003, the inside of bolt 1003 is mounted with shaft coupling 1004, and the inside peace of shaft coupling 1004 for 1002 top
Be equipped with screw rod 1005, to be fixedly connected between shaft coupling 1004 and motor flap 1002, and shaft coupling 1004 and screw rod 1005 it
Between to be fixedly connected, screw rod 1005 constitutes drive mechanism by shaft coupling 1004 and motor 1001, and motor 1001 passes through motor
Flap 1002 and motor cabinet 10 constitute detaching structure, are nested structure between framework type ship lid screw rod slide 9 and screw rod 1005, and
Framework type ship lid screw rod slide 9 constitutes lifting structure by middle connecting rod 901 and motor cabinet 10, and two-way motor 1001 rotates, band
Dynamic shaft coupling 1004 rotates, so that screw rod 1005 be driven to rotate, by the use of two-way motor 1001 and shaft coupling 1004, makes
The flight for obtaining dirigible can be more steady, avoid dirigible and fall because lift is insufficient in flight, to reduce winged
The possibility that accident occurs when ship flight improves the stability that flight uses.
Working principle: for this kind of dirigible, being passed through nitrogen for dirigible, under the influence of air pressure, connecting rod 903, framework type
Ship cover connecting rod 905 and framework type ship lid connecting rod 907 are holded up, and then ship cloth 1 is strutted, and are connected by connecting rod 903, framework type ship lid
The use of bar 905 and framework type ship lid connecting rod 907 improves the lift of dirigible so that the shape of dirigible is able to carry out transformation,
Then the two-way motor 1001 of model 60KTYZ rotates, and shaft coupling 1004 is driven to rotate, so that screw rod 1005 is driven to rotate,
Then 3 revolving speed of vane in quadrotor 2 is consistent, with the athletic posture of variable hull co- controlling dirigible in the vertical direction；Two
A horizontal Solid rocket engine duct 8 controls the athletic posture in dirigible horizontal direction, i.e., horizontal Solid rocket engine duct 8 and vane 3 etc.
Horizontal linear advancing movement or the wind resistance positioning of dirigible, differential between horizontal Solid rocket engine duct 8 and vane 3 can be realized when revolving speed
The turning action control course in dirigible horizontal direction can be realized when rotation, complete the use process of entire dirigible like this.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of two duct Solid rocket engine quadrotor solar energy dish variant dirigibles, including ship cloth (1), rotor (2) and solar energy
Thin film panels (5), it is characterised in that: the inside of the ship cloth (1) is equipped with framework type ship lid (4), and framework type ship lid (4)
To be fixedly connected between ship cloth (1), the rotor (2) is fixed on the outside of framework type ship lid (4), and the top of rotor (2)
It is connected with vane (3), is flexibly connected between the rotor (2) and vane (3), solar film battery plate (5) placement
It is connected with ship carrying platform (6) below the top of ship cloth (1), the framework type ship lid (4), and the top of ship carrying platform (6)
It is fixed with helium and fills air extractor and charge and discharge power supply system (7) automatically, level is installed on the outside of the ship carrying platform (6) and is pushed away
Into control duct (8), framework type ship lid screw rod slide (9), and framework type ship lid are mounted on the inside of the framework type ship lid (4)
(4) to be fixedly connected between framework type ship lid screw rod slide (9), the inside installation of the framework type ship lid screw rod slide (9)
Have motor cabinet (10), and is to be flexibly connected between motor cabinet (10) and framework type ship lid screw rod slide (9).
2. a kind of two ducts Solid rocket engine quadrotor solar energy dish variant dirigible according to claim 1, feature exist
In: it is fitted closely between the bottom of the solar film battery plate (5) and the outside of ship cloth (1), and solar film battery
Bonding connection between plate (5) and ship cloth (1).
3. a kind of two ducts Solid rocket engine quadrotor solar energy dish variant dirigible according to claim 1, feature exist
In: there are two horizontal Solid rocket engine duct (8) settings, and its outside for being evenly distributed in ship carrying platform (6), and water
It is to be fixedly connected between flat Solid rocket engine duct (8) and framework type ship lid (4).
4. a kind of two ducts Solid rocket engine quadrotor solar energy dish variant dirigible according to claim 1, feature exist
In: the framework type ship lid screw rod slide (9) include middle connecting rod (901), connecting rod ship and resell on another market (902), connecting rod (903), framework type ship
Cover connecting rod is shipped and resell on another market (904), framework type ship cover connecting rod (905), framework type ship lid connecting rod are shipped and resell on another market (906), framework type ship lid frame linking
Bar (907) and framework type ship lid are shipped and resell on another market (908), are connected with middle connecting rod on the outside of the framework type ship lid screw rod slide (9)
(901), and the outside at the top of middle connecting rod (901) is fixed with connecting rod and ships and resell on another market (902), the connecting rod ship and resell on another market (902) outside connection
Have connecting rod (903), and be fixed with framework type ship cover connecting rod on the outside of connecting rod (903) and ship and resell on another market (904), the connecting rod ships and resell on another market (902)
To be flexibly connected between connecting rod (903), the framework type ship cover connecting rod, which is shipped and resell on another market, to be equipped with framework type ship lid on the outside of (904) and connects
Bar (905), and be connected with framework type ship lid connecting rod on the outside of framework type ship cover connecting rod (905) and ship and resell on another market (906), the framework type
Ship cover connecting rod is shipped and resell on another market to be flexibly connected between (904) and framework type ship cover connecting rod (905), and the framework type ship lid connecting rod is shipped and resell on another market
(906) it is connected with framework type ship lid connecting rod (907) on the outside of, and is connected with structure on the outside of framework type ship lid connecting rod (907)
Posture ship lid is shipped and resell on another market (908), and the framework type ship lid connecting rod, which is shipped and resell on another market (906) between framework type ship lid connecting rod (907), is
It is flexibly connected, the connecting rod (903) is shipped and resell on another market (902) and middle connecting rod (901) composition rotational structure by connecting rod, and framework type ship lid
Connecting rod (905) constitutes rotational structure by ship and resell on another market (904) and connecting rod (903) of framework type ship cover connecting rod, and framework type ship lid connects
Hack lever (907) is shipped and resell on another market (906) by framework type ship lid connecting rod and framework type ship cover connecting rod (905) constitutes rotational structure, and
The slewing area of connecting rod (903), framework type ship cover connecting rod (905) and framework type ship lid connecting rod (907) is 0-178 °.
5. a kind of two ducts Solid rocket engine quadrotor solar energy dish variant dirigible according to claim 1, feature exist
In: the motor cabinet (10) includes motor (1001), motor flap (1002), bolt (1003), shaft coupling (1004) and screw rod
(1005), the inside of the motor cabinet (10) is equipped with motor (1001), and is equipped with motor flap at the top of motor (1001)
(1002), the top of the motor flap (1002) is mounted with connection on the inside of the bolt (1003) through having bolt (1003)
Axis device (1004), and screw rod (1005) are mounted on the inside of shaft coupling (1004), the shaft coupling (1004) and motor flap
(1002) to be fixedly connected between, and to be fixedly connected between shaft coupling (1004) and screw rod (1005), the screw rod (1005)
Drive mechanism is constituted by shaft coupling (1004) and motor (1001), and motor (1001) passes through motor flap (1002) and motor
Seat (10) constitutes detaching structure.
6. a kind of two ducts Solid rocket engine quadrotor solar energy dish variant dirigible according to claim 5, feature exist
In: it is nested structure between the framework type ship lid screw rod slide (9) and screw rod (1005), and framework type ship lid screw rod slide
(9) lifting structure is constituted by middle connecting rod (901) and motor cabinet (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910255024.4A CN109878693A (en) | 2019-03-29 | 2019-03-29 | A kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910255024.4A CN109878693A (en) | 2019-03-29 | 2019-03-29 | A kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles |
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| Publication Number | Publication Date |
|---|---|
| CN109878693A true CN109878693A (en) | 2019-06-14 |
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ID=66935478
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910255024.4A Pending CN109878693A (en) | 2019-03-29 | 2019-03-29 | A kind of two duct Solid rocket engine quadrotor solar energy butterfly variant dirigibles |
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Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205667717U (en) * | 2016-06-01 | 2016-11-02 | 曹晓旭 | A kind of balloon flighter |
| CN109319082A (en) * | 2018-09-07 | 2019-02-12 | 江苏航空职业技术学院 | Quadrotor morphing aircraft |
-
2019
- 2019-03-29 CN CN201910255024.4A patent/CN109878693A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205667717U (en) * | 2016-06-01 | 2016-11-02 | 曹晓旭 | A kind of balloon flighter |
| CN109319082A (en) * | 2018-09-07 | 2019-02-12 | 江苏航空职业技术学院 | Quadrotor morphing aircraft |
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Application publication date: 20190614 |