CN206623980U - A kind of four rotor dirigibles - Google Patents
A kind of four rotor dirigibles Download PDFInfo
- Publication number
- CN206623980U CN206623980U CN201720349273.6U CN201720349273U CN206623980U CN 206623980 U CN206623980 U CN 206623980U CN 201720349273 U CN201720349273 U CN 201720349273U CN 206623980 U CN206623980 U CN 206623980U
- Authority
- CN
- China
- Prior art keywords
- utricule
- bracing piece
- inner bracing
- outer support
- support bar
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
It the utility model is related to a kind of four rotor dirigibles, including installation sleeve pipe, inner bracing piece, utricule, outer support bar and propeller；Installation sleeve pipe and inner bracing piece are horizontally set in utricule, the both ends of installation sleeve pipe are connected with utricule inwall, inner bracing piece both ends pass utricule and are tightly connected with utricule, inner bracing piece is located at the part in utricule and is located in installation sleeve pipe, propeller is located at the end outside utricule with inner bracing piece and is connected, outer support bar is vertical with inner bracing piece, and outer support bar and utricule external connection, and inner bracing piece and the junction of outer support bar and utricule are equipped with stopping means.The utility model is supported by inner bracing piece and outer support bar to utricule, reduces the stress in envelop materialses, it is retained certain redundancy counteracting and is being pullled deformation caused by motor-driven or collision；The design of sleeve pipe is installed so that inner bracing piece can be rapidly assembled and disassembled, and not only reduce built-up time, also improve the maintainability of dirigible.
Description
Technical field
Vehicle technology field is the utility model is related to, especially a kind of four rotor dirigibles.
Background technology
Conventional small dirigible employs the structure of blimp, and profile is kept by the pressure of the intracapsular floating life gas of ship.
Because blimp does not have rigid backbone, dirigible utricule is in addition to the pressure required for undertaking holding shape, it is also necessary to has remaining answer
Power resists Overall bending effect and carrying other structures, and the stress level undertaken which results in envelop materialses is higher.When winged
For ship motor-driven or when bumping against protrusion, envelop materialses easily pull breakage, cause gas leakage in dirigible so that dirigible
Security is relatively low.
Utility model content
Technical problem to be solved in the utility model is in view of the shortcomings of the prior art, there is provided one kind can be with Fast Installation
The four high rotor dirigibles with dismounting, general safety performance.
The technical scheme that the utility model solves above-mentioned technical problem is as follows：A kind of four rotor dirigibles, including installation sleeve pipe,
Inner bracing piece, utricule, outer support bar and propeller；The installation sleeve pipe and the inner bracing piece are horizontally set on the utricule
It is interior, it is described installation sleeve pipe both ends be connected with the utricule inwall, the inner bracing piece both ends pass the utricule and with institute
Utricule sealed connection is stated, the inner bracing piece is located at the part in the utricule and is located in the installation sleeve pipe, the spiral
Oar is located at the end outside the utricule with the inner bracing piece and is connected, and the outer support bar is vertical with the inner bracing piece, and institute
State outer support bar and the utricule external connection, the junction of the inner bracing piece and the outer support bar and the utricule is all provided with
Limited location device.
The beneficial effects of the utility model are：Utricule is supported by inner bracing piece and outer support bar, reduces utricule
Stress in material, it is retained certain redundancy counteracting and pullling deformation caused by motor-driven or collision；Sleeve pipe is installed
Design so that inner bracing piece can be rapidly assembled and disassembled, and not only reduce built-up time, also reduce occupation of land face when not in use
Product, also improve the maintainability of dirigible；The setting of stopping means, can effectively it prevent in installation inner bracing piece and outer support
During bar, inner bracing piece and the relative position of outer support bar and utricule can not be positioned.
On the basis of above-mentioned technical proposal, the utility model can also do following improvement.
Further, the installation sleeve pipe includes the first installation sleeve pipe being parallel to each other and the second installation sleeve pipe, the utricule
For elliposoidal, the first installation sleeve pipe and the second installation sleeve pipe are vertical with the long axis direction of the utricule, and described first
The both ends for installing sleeve pipe are connected with the both ends of the described second installation sleeve pipe with the utricule inwall.
Further, the inner bracing piece includes the first inner bracing piece and the second inner bracing piece that are parallel to each other, and described first
Inner bracing piece is set in the first installation sleeve pipe, and second inner bracing piece is set in the second installation sleeve pipe.
It is using the above-mentioned further beneficial effect of scheme：First inner bracing piece is set in the first installation sleeve pipe, and second
Inner bracing piece is set in the second installation sleeve pipe so that the first inner bracing piece and the second inner bracing piece with Fast Installation and can be torn open
Unload, not only reduce built-up time, also reduce floor space when not in use, also improve the maintainability of dirigible.
Further, the outer support bar includes the first outer support bar and the second outer support bar that are parallel to each other, and described first
Outer support bar and the second outer support bar are parallel with the long axis direction of the utricule, the first outer support bar and described
Two equal one end of outer support bar are connected with first inner bracing piece, and the other end is connected with second inner bracing piece.
Further, outer wall of the middle part of the first outer support bar and the second outer support bar with the utricule is connected.
Further, first inner bracing piece and second inner bracing piece are arranged symmetrically on the centre of buoyancy of the utricule,
The first outer support bar and the second outer support bar are arranged symmetrically on the centre of buoyancy of the utricule.
Further, the propeller is 4, and 4 propellers are separately mounted to the both ends of first inner bracing piece
With the both ends of second inner bracing piece.
Further, the installation sleeve pipe is made with the utricule outer wall of coated fabric.
Further, the inner bracing piece and the outer support bar are made of metal alloy or carbon fibre material.
It is using the above-mentioned further beneficial effect of scheme：Using inner bracing piece made of metal alloy or carbon fibre material
It is high with outer support bar light weight, specific strength, reduce the loss that skeleton installation brings buoyancy reduction.
Brief description of the drawings
Fig. 1 is the scheme of installation of the rotor dirigible of the utility model four；
Fig. 2 is the schematic diagram that the utility model installs sleeve pipe.
In accompanying drawing, the list of parts representated by each label is as follows：
The 1st, sleeve pipe is installed；11st, the first installation sleeve pipe；12nd, the second installation sleeve pipe；2nd, inner bracing piece；21st, the first inner support
Bar；22nd, the second inner bracing piece；3rd, utricule；4th, outer support bar；41st, the first outer support bar；42nd, the second outer support bar；5th, spiral
Oar；6th, stopping means.
Embodiment
Principle of the present utility model and feature are described below in conjunction with accompanying drawing, example is served only for explaining this practicality
It is new, it is not intended to limit the scope of the utility model.
As shown in Figure 1 and Figure 2, a kind of four rotors dirigible of the present utility model, including installation sleeve pipe 1, inner bracing piece 2, utricule
3rd, outer support bar 4 and propeller 5；Installation sleeve pipe 1 and inner bracing piece 2 are horizontally set in utricule 3, install the both ends of sleeve pipe 1
It is connected with the inwall of utricule 3, the both ends of inner bracing piece 2 pass utricule 3 and are tightly connected with utricule, and inner bracing piece 2 is located in utricule 3
Part be located in installation sleeve pipe 1 in, propeller 5 is located at the end outside utricule 3 with inner bracing piece 2 and is connected, outer support bar 4 with it is interior
Support bar 2 is vertical, and outer support bar 4 and the external connection of utricule 3, and the junction of inner bracing piece 2 and outer support bar 4 and utricule 3 is equal
Provided with stopping means 6.
The four rotor dirigibles of the present embodiment are supported by inner bracing piece 2 and outer support bar 4 to utricule 3, reduce utricule
Stress in material, it is retained certain redundancy counteracting and pullling deformation caused by motor-driven or collision；Sleeve pipe 1 is installed
Design so that inner bracing piece 2 can be rapidly assembled and disassembled, and not only reduce built-up time, also reduce occupation of land when not in use
Area, also improve the maintainability of dirigible；The setting of stopping means 6, can effectively it prevent in installation inner bracing piece 2 and outer
During support bar 4, the relative position of inner bracing piece 2 and outer support bar 4 and utricule 3 can not be positioned.
As shown in Fig. 2 the installation sleeve pipe 1 of the present embodiment includes the first installation installation set of sleeve pipe 11 and second being parallel to each other
Pipe 12, utricule 3 are elliposoidal, and the first installation installation sleeve pipe 12 of sleeve pipe 11 and second is vertical with the long axis direction of utricule 3, and the
The both ends of one installation sleeve pipe 11 are connected with the both ends of the second installation sleeve pipe 12 with the inwall of utricule 3.
As shown in figure 1, the inner bracing piece 2 of the present embodiment includes the first inner bracing piece 21 and the second inner support being parallel to each other
Bar 22, the first inner bracing piece 21 are set in 11 in the first installation sleeve pipe, and the second inner bracing piece 22 is set in the second installation sleeve pipe 12
It is interior；First inner bracing piece 21 is set in the first installation sleeve pipe 11, and the second inner bracing piece 22 is set in the second installation sleeve pipe 12,
First inner bracing piece 21 and the second inner bracing piece 22 are rapidly assembled and disassembled, built-up time is not only reduced, also reduces
Floor space when not in use, also improve the maintainability of dirigible.
As shown in figure 1, the outer support bar 4 of the present embodiment includes the first outer support bar 41 and the second outer support being parallel to each other
Bar 42, the first outer support bar 41 is parallel with the long axis direction of utricule 3 with the second outer support bar 42, the first outer support bar 41 and
Two outer support bars, 42 equal one end is connected with the first inner bracing piece 21, and the other end is connected with the second inner bracing piece 22.First inner support
The inner bracing piece 22 of bar 21 and second is arranged symmetrically on the centre of buoyancy of utricule 3, and the first outer support bar 41 and the second outer support bar 42 close
It is arranged symmetrically in the centre of buoyancy of utricule 3.Outside by the first inner bracing piece 21, the first outer support bar 41, the second inner bracing piece 22 and second
Support bar 42 constitutes support frame, and utricule 3 is supported, and is made by metal alloy or carbon fibre material, specific strength
It is higher with rigid, the stress in envelop materialses is reduced, it is retained certain redundancy and offsets in motor-driven or collision
It is caused to pull deformation；Meanwhile the lighter weight of support frame, reduce support frame and utricule 3 is damaged by buoyancy reduction
Lose.
As shown in Fig. 2 the installation sleeve pipe 1 of the present embodiment is arranged in utricule 3, it is made of coated fabric, intensity is high, soft
Tough performance is good, barrier property is excellent, can prevent attacking material when through installation sleeve pipe 1 of inner bracing piece 2, prevent in utricule 3
Gas is revealed along installation sleeve pipe 1.
The propeller 5 of the four rotor dirigibles of the present embodiment is 4, and 4 propellers 5 are separately mounted to the first inner bracing piece 21
Both ends and the second inner bracing piece 22 both ends.
Preferred embodiment of the present utility model is these are only, it is all in the utility model not to limit the utility model
Spirit and principle within, any modification, equivalent substitution and improvements made etc., should be included in protection model of the present utility model
Within enclosing.
Claims (9)
1. a kind of four rotor dirigibles, it is characterised in that including installation sleeve pipe (1), inner bracing piece (2), utricule (3), outer support bar
And propeller (5) (4)；The installation sleeve pipe (1) and the inner bracing piece (2) are horizontally set in the utricule (3), described
Installation sleeve pipe (1) both ends be connected with the utricule (3) inwall, inner bracing piece (2) both ends pass the utricule (3) and
It is tightly connected with the utricule (3), the part that the inner bracing piece (2) is located in the utricule (3) is located in the installation set
Manage in (1), the propeller (5) is located at the end of the utricule (3) outside with the inner bracing piece (2) and is connected, the outer support
Bar (4) is vertical with the inner bracing piece (2), and the outer support bar (4) and the utricule (3) external connection, the inner support
The junction of bar (2) and the outer support bar (4) and the utricule (3) is equipped with stopping means (6).
2. a kind of four rotor dirigibles according to claim 1, it is characterised in that the installation sleeve pipe (1) includes being parallel to each other
First installation sleeve pipe (11) and second installation sleeve pipe (12), the utricule (3) is elliposoidal, it is described first install sleeve pipe (11)
It is vertical with the long axis direction of the utricule (3) with the second installation sleeve pipe (12), and the both ends of the first installation sleeve pipe (11)
It is connected with the both ends of the described second installation sleeve pipe (12) with the utricule (3) inwall.
3. a kind of four rotor dirigibles according to claim 2, described in its feature, the inner bracing piece (2) includes being parallel to each other
The first inner bracing piece (21) and the second inner bracing piece (22), first inner bracing piece (21) is set in first installation set
Manage in (11), second inner bracing piece (22) is set in the second installation sleeve pipe (12).
4. a kind of four rotor dirigibles according to claim 3, described in its feature, the outer support bar (4) includes being parallel to each other
The first outer support bar (41) and the second outer support bar (42), the first outer support bar (41) and the second outer support bar
(42) it is parallel with the long axis direction of the utricule (3), the first outer support bar (41) and the second outer support bar (42)
Equal one end is connected with first inner bracing piece (21), and the other end is connected with second inner bracing piece (22).
5. a kind of four rotor dirigibles according to claim 4, described in its feature, the first outer support bar (41) and the second outer support
Outer wall of the middle part of bar (42) with the utricule (3) is connected.
6. according to a kind of four rotors dirigible of claim 4 or 5, it is characterised in that first inner bracing piece (21) and institute
The centre of buoyancy that the second inner bracing piece (22) is stated on the utricule (3) is arranged symmetrically, the first outer support bar (41) and described
Two outer support bars (42) are arranged symmetrically on the centre of buoyancy of the utricule (3).
7. according to a kind of any one of claim 3 to 5 four rotors dirigible, it is characterised in that the propeller (5) is 4,
4 propellers (5) are separately mounted to both ends and second inner bracing piece (22) of first inner bracing piece (21)
Both ends.
8. according to a kind of any one of claim 1 to 5 four rotors dirigible, described in its feature, the installation sleeve pipe (1) and institute
Utricule (3) outer wall is stated to be made of coated fabric.
9. according to a kind of any one of claim 1 to 5 four rotors dirigible, described in its feature, the inner bracing piece (2) and institute
Outer support bar (4) is stated to be made of metal alloy or carbon fibre material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720349273.6U CN206623980U (en) | 2017-04-05 | 2017-04-05 | A kind of four rotor dirigibles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720349273.6U CN206623980U (en) | 2017-04-05 | 2017-04-05 | A kind of four rotor dirigibles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206623980U true CN206623980U (en) | 2017-11-10 |
Family
ID=60207697
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720349273.6U Active CN206623980U (en) | 2017-04-05 | 2017-04-05 | A kind of four rotor dirigibles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206623980U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021169022A1 (en) * | 2020-02-28 | 2021-09-02 | 南京祖航航空科技有限公司 | Quick disassembly airship pod |
-
2017
- 2017-04-05 CN CN201720349273.6U patent/CN206623980U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021169022A1 (en) * | 2020-02-28 | 2021-09-02 | 南京祖航航空科技有限公司 | Quick disassembly airship pod |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8328516B2 (en) | Systems and methods of assembling a rotor blade extension for use in a wind turbine | |
| MX2007013790A (en) | Systems and methods for tethered turbines. | |
| CA2722182A1 (en) | Aerial wind power generating system using floating body | |
| CN108100242A (en) | A kind of external helicopter short limb floating drum cabin | |
| CN206623980U (en) | A kind of four rotor dirigibles | |
| TW201309909A (en) | An eddy-type wind power collection device | |
| CN103532274B (en) | There is the rotor support power generator of edge of a wing wheel hub | |
| CN104564539B (en) | Wind power generating set and its kuppe front supporting device | |
| CN102141014A (en) | Wind collecting tower structure for wind power generation | |
| US8113778B2 (en) | Wind turbine blade stowage | |
| CN104612905B (en) | Multilevel narrow tube wind-gathering wind power generation system | |
| CN1762763A (en) | Radial type screw propeller | |
| CN115285542B (en) | Reinforcing structure of oil storage cabin | |
| CN207791155U (en) | Unmanned propeller-parachuting | |
| CN205469759U (en) | Novel four rotor dirigibles | |
| CN107856834A (en) | Balloon flighter balloon draw off gear | |
| CN208069254U (en) | A kind of firm balloon arched door frame | |
| CN205221084U (en) | Rigid structure system of big size dirigible | |
| CN107972880A (en) | Multi-rotor unmanned aerial vehicle protective device | |
| CN204402768U (en) | Wind power generating set and air guide sleeve front supporting device thereof | |
| CN210443141U (en) | Suspension type stop board convenient to lift for monorail transit station | |
| CN219627624U (en) | High wind-resistant hydraulic lifting rod | |
| CN212172494U (en) | Auxiliary propulsion device for WIG craft | |
| CN207419298U (en) | A kind of guideboard upright bar with controllability | |
| CN106050552A (en) | Fan blade capable of resisting to bending and wind driven generator containing fan blade |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |