CN108750080A - A kind of ring-type honeycomb excitation vector propulsion double-rotor aerobat - Google Patents
A kind of ring-type honeycomb excitation vector propulsion double-rotor aerobat Download PDFInfo
- Publication number
- CN108750080A CN108750080A CN201810399003.5A CN201810399003A CN108750080A CN 108750080 A CN108750080 A CN 108750080A CN 201810399003 A CN201810399003 A CN 201810399003A CN 108750080 A CN108750080 A CN 108750080A
- Authority
- CN
- China
- Prior art keywords
- umbrella
- propeller
- connecting rod
- cover connecting
- soil
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
Abstract
The invention discloses a kind of cyclic annular honeycomb excitation vectors to promote double-rotor aerobat, include the connecting bridge of two rotor ontologies of two rotor ontologies and connection, rotor ontology includes excitation pole shell, excitation pole shell is annular, its inner wall has excitation wall, excitation pole upper part of the housing is equipped with supporting rack, flexural pivot spindle is installed at supporting rack center, ball-joint shaft end is equipped with propeller, so that propeller is rotated around flexural pivot spindle, the propeller center has propeller ball-joint hole, it cooperatively forms and is flexibly connected with flexural pivot spindle, there are four blades for the propeller tool, blade tip has permanent magnet, permanent magnet is belly shirt, middle part is hollow chamber, chamber inner wall is fixed with spring.
Description
Technical field
The present invention relates to a kind of cyclic annular honeycomb excitation vectors to promote double-rotor aerobat.
Background technology
Aircraft mostly uses single rotor design at present, and the promotion of flying speed and efficiency relies primarily on improvement engine and sets
It counts, and the engine research, development period is very long, it is relatively difficult by motor power promotion aircraft performance is improved in the short time, it is existing
Some double-rotor aerobats cannot achieve the flight of aircraft by usual propeller motor and control system.
Invention content
In view of the above problems, the present invention provides a kind of cyclic annular honeycomb excitation vector propulsion double-rotor aerobat, leads to
Cross the normal control that vector pushes screw motor that double-vane aircraft may be implemented.
To achieve the goals above, technical solution provided by the invention is：A kind of ring-type honeycomb excitation vector propulsion bispin
Rotor aircraft, including two rotor ontologies and the connecting bridge for connecting two rotor ontologies,
The rotor ontology includes excitation pole shell, and excitation pole shell is annular, and inner wall has excitation wall,
Excitation pole upper part of the housing is equipped with supporting rack, and flexural pivot spindle, the installation of ball-joint shaft end are equipped at supporting rack center
There is propeller so that propeller is rotated around flexural pivot spindle, and the propeller center has propeller ball-joint hole, with flexural pivot
Spindle cooperatively forms flexible connection, and for propeller tool there are four blade, it is hollow that blade tip, which has permanent magnet, permanent magnet,
Dress, middle part are hollow chamber, and chamber inner wall is fixed with spring,
Sliding ball wheel is installed on the outside of permanent magnet, the sliding ball wheel is fixedly connected by ball wheel support upright one end, ball wheel branch
The column other end is fixed on the spring inside permanent magnet so that and ball wheel support upright can be controlled to be moved with telescopic spring,.
Existing gyroplane is mostly directly to drive propeller by motor, due to the connection side between motor shaft and propeller
Formula is to be fixedly connected, and the operative orientation and mode to propeller have prodigious limitation, propeller to be only capable of the rotation around fixing axle.
This programme proposes that one kind adding permanent magnet in propeller end, and is revolved using electromagnetism power drive propeller by way of honeycomb excitation
Turn, while can also adjust propeller pose, to realize that vectored thrust, this mode are more flexible and efficient.
Description of the drawings
Fig. 1 is shaft side figure of the present invention；
Fig. 2 is front view of the present invention；
Fig. 3 is vertical view of the present invention；
Fig. 4 is the A-A full sectional views of Fig. 3；
Fig. 5 is propeller arrangement schematic diagram of the present invention；
Fig. 6 is propeller overlooking structure diagram of the present invention；
Fig. 7 is the B-B full sectional views of Fig. 6；
Fig. 8 is excitation wall construction schematic diagram of the present invention；
Fig. 9 is that vector of the present invention promotes operating diagram.
Figure 10 is the partial enlarged view of Fig. 7.
Figure 11 is excitation wall local structural graph.
In figure：1 excitation pole shell, 2 excitation walls, 3 supporting racks, 4 propellers, 5 flexural pivot spindles, 6 aircraft connecting bridges, 7 spiral shells
Revolve paddle ball-joint shell, 8 permanent magnets, 9 sliding ball wheels, 10 springs, 11 ball wheel support uprights, 12 excitation rings, 13 cellular excitation poles
Wall；14, electromagnet；15, triangle is evenly distributed with iron plate.
Specific implementation mode
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 describes, 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.
It please refers to Fig.1-10, including two rotor ontologies and connects the connecting bridge of two rotor ontologies,
The rotor ontology includes excitation pole shell 1, and excitation pole shell 1 is annular, and excitation pole shell 1 is by multiple
Triangle is evenly distributed with the ring-shaped shell that iron plate 15 is spliced,
1 top of excitation pole shell is equipped with supporting rack 3, and flexural pivot spindle 5, ball-joint shaft end peace are equipped at supporting rack center
Equipped with propeller so that propeller is rotated around flexural pivot spindle, and the propeller center has propeller ball-joint hole, with ball
Articulated shaft 5 cooperatively forms flexible connection, and there are four blade, blade tips to have permanent magnet 8, permanent magnet 8 for propeller tool
For belly shirt, middle part is hollow chamber, and chamber inner wall is fixed with spring 10,
Sliding ball wheel 9 is installed on the outside of permanent magnet, the sliding ball wheel 9 is fixedly connected by 11 one end of ball wheel support upright, ball
11 other end of wheel support upright is fixed on the spring inside permanent magnet 8 so that and ball wheel support upright 11 can be controlled to be moved with telescopic spring,
There is excitation wall 2, the excitation wall to have multiple triangles to be evenly distributed with what iron plate 15 was spliced for the inside of excitation pole shell 1
Ring bodies, each triangle are evenly distributed with 15 side of iron plate and are respectively and fixedly provided with electromagnet 14, are powered to shape by different electromagnet 14
At the excitation ring 12 of different angle, as the excitation of motor, control close to propeller position triangle be evenly distributed with iron plate and
Permanent magnet 8 is magnetic on the contrary, to realize attraction, and then driving propeller rotation, and which is peculiar for this patent, Ke Yitong
It crosses and controls multiple electromagnet, realize that excitation changes 12 rotation, to drive the vector of propeller to rotate so that propeller can be with
Excitation ring is parallel to realize oblique blowing.
Claims (2)
1. a kind of Soil K+adsorption Mining Test device, which is characterized in that including soil cutting part and soil support portion, soil cutting
Portion be mounted on soil support portion side, soil support portion includes several cutting wheels, the soil support portion be it is multiple simultaneously
The trigone rail of arrangement is arranged, there is gap between adjacent trigone rail,
The end of trigone rail has the three point arbitrage of corresponding triangle, is installed on three point arbitrage there are two cutting wheel,
For soil support portion bottom tool there are four hydraulic lifting post, four hydraulic lifting post lower parts are mounted on umbrella shaped support foot.
2. a kind of Soil K+adsorption Mining Test device according to claim 1, which is characterized in that the umbrella shaped support foot
Including upper drive block, the upper drive block is annular, and ring-shaped inner part is hydraulic column, what hydraulic column and upper drive block can be autonomous
Upper and lower relative motion,
Upper drive block is uniformly equipped with multiple umbrella cover connecting rods, and umbrella cover connecting rod upper end is equipped with outer hinged block, umbrella cover connecting rod
Hinged by outer hinged block and upper drive block, the Connectable umbrella side axis of the lower end of umbrella cover connecting rod are hinged, and multiple umbrella side axis are hingedly led to
Cross fixed ring connection circlewise,
Umbrella side axis are hingedly also associated with interior umbrella cover connecting rod, the other side of interior umbrella cover connecting rod and the interior hinged block of hydraulic pressure column bottom
It connects, umbrella cover plate is installed between two neighboring interior umbrella cover connecting rod, pass through the joint of upper drive block and hydraulic column in this way and move
It is dynamic, the contraction of umbrella cover connecting rod and interior umbrella cover connecting rod is formd, to form umbrella shaped support foot contractile motion up and down,
Umbrella shaped support foot-shape is at the relative motion of three levels, the i.e. fixed multiple outer hinged block layers of upper drive block institute, hydraulic column
The umbrella side axis hinge layer that is connected of fixed interior hinged block layer and fixed ring, the mutual movement of these three layers realize layer
Shape is progressive to banket, the effect raised.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810399003.5A CN108750080A (en) | 2018-04-28 | 2018-04-28 | A kind of ring-type honeycomb excitation vector propulsion double-rotor aerobat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810399003.5A CN108750080A (en) | 2018-04-28 | 2018-04-28 | A kind of ring-type honeycomb excitation vector propulsion double-rotor aerobat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108750080A true CN108750080A (en) | 2018-11-06 |
Family
ID=64012317
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810399003.5A Withdrawn CN108750080A (en) | 2018-04-28 | 2018-04-28 | A kind of ring-type honeycomb excitation vector propulsion double-rotor aerobat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108750080A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110815981A (en) * | 2019-12-02 | 2020-02-21 | 嘉善泰力蜂窝制品有限公司 | Manufacturing method of high-strength aluminum honeycomb core plate |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201647124U (en) * | 2009-10-30 | 2010-11-24 | 北京工业大学 | Magnetic suspension electrodynamic rotor wing flying disk |
| CN106741918A (en) * | 2017-01-14 | 2017-05-31 | 陕西捷恒新材料有限责任公司 | The axle flying vehicles control structure of skew product vector two |
| CN206654193U (en) * | 2017-04-16 | 2017-11-21 | 中国石油大学(华东) | A kind of new unmanned vehicle drive device |
| CN107364568A (en) * | 2017-07-07 | 2017-11-21 | 范家铭 | Combined type blended wing-body high-speed helicopter |
| EP3263456A1 (en) * | 2016-07-01 | 2018-01-03 | Bell Helicopter Textron Inc. | Aircraft having a versatile propulsion system |
| CN206939072U (en) * | 2016-06-15 | 2018-01-30 | 崔基铉 | Aircraft |
-
2018
- 2018-04-28 CN CN201810399003.5A patent/CN108750080A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201647124U (en) * | 2009-10-30 | 2010-11-24 | 北京工业大学 | Magnetic suspension electrodynamic rotor wing flying disk |
| CN206939072U (en) * | 2016-06-15 | 2018-01-30 | 崔基铉 | Aircraft |
| EP3263456A1 (en) * | 2016-07-01 | 2018-01-03 | Bell Helicopter Textron Inc. | Aircraft having a versatile propulsion system |
| CN106741918A (en) * | 2017-01-14 | 2017-05-31 | 陕西捷恒新材料有限责任公司 | The axle flying vehicles control structure of skew product vector two |
| CN206654193U (en) * | 2017-04-16 | 2017-11-21 | 中国石油大学(华东) | A kind of new unmanned vehicle drive device |
| CN107364568A (en) * | 2017-07-07 | 2017-11-21 | 范家铭 | Combined type blended wing-body high-speed helicopter |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110815981A (en) * | 2019-12-02 | 2020-02-21 | 嘉善泰力蜂窝制品有限公司 | Manufacturing method of high-strength aluminum honeycomb core plate |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181106 |