CN205469757U - Novel but four rotor dirigibles of lathe turner's style of calligraphy - Google Patents
Novel but four rotor dirigibles of lathe turner's style of calligraphy Download PDFInfo
- Publication number
- CN205469757U CN205469757U CN201620020387.1U CN201620020387U CN205469757U CN 205469757 U CN205469757 U CN 205469757U CN 201620020387 U CN201620020387 U CN 201620020387U CN 205469757 U CN205469757 U CN 205469757U
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- CN
- China
- Prior art keywords
- bearing
- air bag
- rotor
- gasbag
- wing
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Abstract
The utility model discloses a novel but four rotor dirigibles of lathe turner's style of calligraphy. It includes the organism: gasbag, nacelle, four rotor frames of I shape, four rotor motors, antifriction bearing axle pipe support cover etc. The device takes off and land through four rotors control aircraft, and the gasbag provides overall lift, and four rotors are rotatory 90 degrees, provide the cruising power forward. This dirigible is in the horizontality in lift in -process frame, and 90 degrees are rotated to four whole rotor frames of the in -process that cruises, is in vertical position. The horizontal axis position of gasbag is link up, realizes through the bearing that four rotors rotate around the frame axis in the space. The shaft seal links firmly in outer port of gasbag and the frame. 90 degrees rotations can be realized to the gasbag between the sealed end of bearing and gasbag.
Description
Technical field
This utility model relate to a kind of novel can lathe turner's font four rotor dirigible.
Background technology
Conventional four rotor dirigible structures drive air bag utricule integral-rotation when rotated, and required moment of flexure is relatively big, requires higher to motor.This patent preferably resolves this problem so that air bag utricule under conditions of level, reduces pitching moment in meeting flight course, reduces motor requirement.
Utility model content
The purpose of this utility model Patent design scheme is to be combined with dirigible by four rotors, utilizes both advantage to carry out operation.Being lifted by four rotors during landing, overall lift is provided by air bag, and under cruising condition, four rotor motor rotary frames, provides forward thrust.Four rotor frames are connected with air bag simply, it is simple to dismounting.
This utility model is achieved through the following technical solutions: a kind of novel can lathe turner's font four rotor dirigible, mainly including cell parts, axis part, wing arm section, motor, gondola, cell parts includes air bag utricule, air bag step A, air bag step B, caulking gum hoop A, caulking gum hoop B, air-filled pore；Middle shaft part divides and includes central shaft rod, bearing, bearing sleeve, bearing positioning sleeve；Wing arm section includes wing armed lever, threeway, hexagon socket head cap screw, pipe clamp, electric baseboard, hexagon socket head cap screw；It is characterized in that: described bearing is fixed in central shaft rod by bearing positioning sleeve, bearing outside upper bearing (metal) sleeve pipe, bearing sleeve is fixed together by caulking gum hoop A with air bag step A, air bag step B is glued together with central shaft rod glue and fixes with caulking gum hoop B, central shaft rod two ends are connected with wing armed lever by threeway, and fix with hexagon socket head cap screw, pipe clamp is fixed on the two ends of wing armed lever together with electric baseboard by hexagon socket head cap screw；Motor is fixed on electric baseboard, and gondola is fixed on air bag utricule.
It is provided with air-filled pore on this utility model air bag utricule.
This utility model frame uses the mode that runs through, air bag and frame axis to utilize bearing to realize rotating with the connected mode of air bag, and bearing is in air bag, and air bag uses glue sealing with frame axis outermost end and fixes with clip.
This utility model is in the case of the sealing that will not destroy air bag, and between air bag inner bearing and air sac sealing, utricule can realize 90 degree of rotations.
Component of the present utility model can be freely lifted guaranteeing, and cruise, under the function of long-time stagnant sky, it is simple to the convenient transport when operation, it is simple to dismounting.
Accompanying drawing explanation
Fig. 1 is overall structure schematic diagram of the present utility model；
Fig. 2 is CONSTRUCTED SPECIFICATION figure of the present utility model；
Fig. 3 is CONSTRUCTED SPECIFICATION figure of the present utility model；
Fig. 4 is CONSTRUCTED SPECIFICATION figure of the present utility model；
Fig. 5 is CONSTRUCTED SPECIFICATION figure of the present utility model；
Fig. 6 is CONSTRUCTED SPECIFICATION figure of the present utility model；
Fig. 7 is air bag view of the present utility model；
Fig. 8 is top view of the present utility model；
Fig. 9 is left view of the present utility model.
In the drawings, 1 is cell parts, wherein air bag utricule 11, air bag step A (12), air bag step B (13), caulking gum hoop A(14), caulking gum hoop B(15), air-filled pore 16,2 be axis part, wherein central shaft rod 21, bearing 22, bearing sleeve 23, bearing positioning sleeve 24, wing arm section 3, wing armed lever 31, threeway 32, hexagon socket head cap screw 33, pipe clamp 34, electric baseboard 35, hexagon socket head cap screw 36, motor 4, gondola 5.
Detailed description of the invention
Below in conjunction with accompanying drawing, this utility model is described in detail.
Referring to the drawings, this utility model is by including cell parts 1, air bag utricule 11, air bag step A (12), air bag step B (13), caulking gum hoop A(14), caulking gum hoop B(15), air-filled pore 16, axis part 2, central shaft rod 21, bearing 22, bearing sleeve 23, bearing positioning sleeve 24, wing arm section 3, wing armed lever 31, threeway 32, hexagon socket head cap screw 33, pipe clamp 34, electric baseboard 35, hexagon socket head cap screw 36, motor 4, gondola 5.Described bearing 22 is fixed in central shaft rod 21 by bearing positioning sleeve 24, bearing 22 overcoat upper bearing (metal) sleeve pipe 23, bearing sleeve 23 and air bag step A(12) it is fixed together by caulking gum hoop A (14), air bag step B (13) and central shaft rod 21 glued together with glue and with caulking gum hoop B(15) fixing, central shaft rod 21 two ends are connected with wing armed lever 31 by threeway 32, and fix with hexagon socket head cap screw 33.Pipe clamp 34 is fixed on the two ends of wing armed lever 31 together with electric baseboard 35 by hexagon socket head cap screw 36.Motor 4 is fixed on electric baseboard 35, and gondola 5 is fixed on air bag utricule 11.During aircraft work, four rotor motors 4 horizontally rotate, drive aircraft rises overally, after arriving cruising altitude, regulate four Rotor thrust sizes and drive rotor frame 90-degree rotation, air bag utricule 11 is connected by bearing 22 with frame central shaft rod 21, keep level, will not be with gantry rotation, during cruise, on utricule 11, empennage ensures air bag utricule 11 course-stability.After cruise terminates, four rotor motors 4 change thrust size and drive gantry rotation, return to horizontal level, and motor 4 reversion drives aircraft to decline, the end of job.
Claims (2)
1. novel can lathe turner's font four rotor dirigible, mainly include cell parts, axis part, wing arm section, motor, gondola, cell parts includes air bag utricule, air bag step A, air bag step B, caulking gum hoop A, caulking gum hoop B, air-filled pore；Middle shaft part divides and includes central shaft rod, bearing, bearing sleeve, bearing positioning sleeve；Wing arm section includes wing armed lever, threeway, hexagon socket head cap screw, pipe clamp, electric baseboard；It is characterized in that: described bearing is fixed in central shaft rod by bearing positioning sleeve, bearing outside upper bearing (metal) sleeve pipe, bearing sleeve is fixed together by caulking gum hoop A with air bag step A, air bag step B is glued together with central shaft rod glue and fixes with caulking gum hoop B, central shaft rod two ends are connected with wing armed lever by threeway, and fix with hexagon socket head cap screw, pipe clamp is fixed on the two ends of wing armed lever together with electric baseboard by hexagon socket head cap screw；Motor is fixed on electric baseboard, and gondola is fixed on air bag utricule.
One the most according to claim 1 is novel can lathe turner's font four rotor dirigible, it is characterised in that: it is provided with air-filled pore on air bag utricule.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620020387.1U CN205469757U (en) | 2016-01-11 | 2016-01-11 | Novel but four rotor dirigibles of lathe turner's style of calligraphy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620020387.1U CN205469757U (en) | 2016-01-11 | 2016-01-11 | Novel but four rotor dirigibles of lathe turner's style of calligraphy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205469757U true CN205469757U (en) | 2016-08-17 |
Family
ID=56666485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620020387.1U Expired - Fee Related CN205469757U (en) | 2016-01-11 | 2016-01-11 | Novel but four rotor dirigibles of lathe turner's style of calligraphy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205469757U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116215900A (en) * | 2023-03-07 | 2023-06-06 | 深圳技术大学 | Double-airbag unmanned aerial vehicle |
-
2016
- 2016-01-11 CN CN201620020387.1U patent/CN205469757U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116215900A (en) * | 2023-03-07 | 2023-06-06 | 深圳技术大学 | Double-airbag unmanned aerial vehicle |
| CN116215900B (en) * | 2023-03-07 | 2023-11-14 | 深圳技术大学 | Double-airbag unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 Termination date: 20170111 |