CN105882962A - Rotating umbrella mechanism - Google Patents
Rotating umbrella mechanism Download PDFInfo
- Publication number
- CN105882962A CN105882962A CN201410542483.8A CN201410542483A CN105882962A CN 105882962 A CN105882962 A CN 105882962A CN 201410542483 A CN201410542483 A CN 201410542483A CN 105882962 A CN105882962 A CN 105882962A
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- CN
- China
- Prior art keywords
- umbrella
- lift
- crank
- rotating
- rotating parachute
- 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.)
- Pending
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Abstract
The invention provides a rotating umbrella mechanism. An umbrella which is arranged on a crank link mechanism of a stationary gear and a rotating gear is provided, during a rotary movement, the umbrella generates an upward lift force by means of unfolding and folding under the effects of air resistance, so that levitation and hovering of a machine body are realized. The rotating umbrella mechanism can be used for realizing vertical take-off and landing as well as hovering functions for one person or a large-scale flying machine; the mechanism has the advantages of simple structure, low manufacture cost, wide application range, easy operation, reduced fuel oil, etc.
Description
The present invention relates to " rotating parachute mechanism ".Vertically taking off and landing flyer originally the most all have employed traditional
Propeller rotates and improves lift, grasps direction with tail vane.Here it is " traditional propeller helicopter " is
Big shortcoming.
" rotating parachute mechanism " proposed by the invention just solves disadvantage mentioned above, original " propeller ",
Make the device of " umbrella " formula into, it is possible to play the effect of propeller.
" rotating parachute mechanism " provided by the present invention its for a kind of by being located at stationary gear, widely different rotation gear crank
Umbrella above linkage, in rotary motion by umbrella under the resistance of air, an exhibition one is closed and is created up
Lift make fuselage lift-off and rotation stop.
" rotating parachute mechanism " provided by the present invention, its be a kind of by umbrella combination 1, umbrella stem 2, swing pinion 3,
Swing pinion axis hole 4, rotary crank axle 5, crank 6, cingulum 7, stationary gear 8, frame 9, board 10,
The mechanism that crank bearing oil slinger 11 and crank axle 12 are formed.Further illustrate the present invention's below in conjunction with accompanying drawing
Architectural feature and purpose.
Brief Description Of Drawings:
Fig. 1 is the main schematic diagram of basic structure of " rotating parachute mechanism " provided by the present invention.
Fig. 2 is the basic structure side view of " rotating parachute mechanism " provided by the present invention.
Fig. 3, Fig. 4, Fig. 5, Fig. 6, it is the action diagram of " rotating parachute mechanism " provided by the present invention.
Please see Figure 3, shown in Fig. 4, Fig. 5, Fig. 6, it is mainly stirring rotary crank axle 5, rotation counterclockwise
Turn gear 3 and umbrella combination 1 rotates around stationary gear 8 under the effect of crank 6 and cingulum 7, and force
Widely different rotation is made in swing pinion 3 and umbrella combination 1；All the time umbrella is made to combine 1 position upward.When umbrella combination 1 from
When 12 inverse position hour hands go to 6 positions, it is in full swing under the resistance of air so that it is produce lift,
Make frame 9 promotion；When umbrella continues up to rotate from 6 positions counterclockwise, at this moment umbrella 1 is in air pressure
Under make umbrella cover Guan Bi make air drag reduce；When umbrella forwards 12 positions counterclockwise to, air drag reduces to
Minimum, when crossing 12 positions, umbrella 1 starts again descending, under the resistance of air, makes umbrella 1 launch to continue next
Individual circulation；Continuous print rotating circulating makes umbrella one open up one to close and create lift, make frame 9 go up to the air normally like this
Flight.
" rotating parachute mechanism " single or Large Scale Space Vehicle should be can be used for can realize VTOL, hovering merit
Energy；.Simple in construction, manufacturing expense are cheap, applied range；Easily operation；Save the advantages such as fuel oil.
Claims (5)
- Rotating parachute mechanism the most provided by the present invention its for a kind of by being located at stationary gear, widely different rotation gear crank connecting rod Umbrella above mechanism, in rotary motion by umbrella under the resistance of air, the lift created up is closed in an exhibition one Fuselage lift-off and rotation is made to stop.
- Rotating parachute mechanism the most according to claim 1 its be a kind of by umbrella combination 1, umbrella stem 2, rotary teeth Wheel 3, swing pinion axis hole 4, rotary crank axle 5, crank 6, cingulum 7, stationary gear 8, frame 9, machine The mechanism that platform 10, crank bearing oil slinger 11 and crank axle 12 are formed.It is located at stationary gear, widely different rotation gear crank Umbrella above linkage, in rotary motion by umbrella under the resistance of air, an exhibition one is closed and is created up Lift makes fuselage lift-off and rotation stop.
- Rotating parachute mechanism the most according to claim 2 is below in conjunction with Brief Description Of Drawings:Fig. 1 is the main schematic diagram of basic structure of rotating parachute mechanism provided by the present invention.Fig. 2 is the basic structure side view of rotating parachute mechanism provided by the present invention.Fig. 3, Fig. 4, Fig. 5, Fig. 6, it is the action diagram of rotating parachute mechanism provided by the present invention.
- Rotating parachute mechanism the most according to claim 3 please see Figure 3, shown in Fig. 4, Fig. 5, Fig. 6, it is main If stirring rotary crank axle 5, swing pinion 3 and umbrella combination 1 counterclockwise in crank 6 and the effect of cingulum 7 Under rotate around stationary gear 8, and force swing pinion 3 and umbrella combination 1 to make widely different rotation；All the time umbrella combination 1 is made Position upward.When umbrella combination 1 goes to 6 positions from 12 inverse position hour hands, complete under the resistance of air Face is launched so that it is produces lift, makes frame 9 promotion；When umbrella continues up to rotate from 6 positions counterclockwise, At this moment umbrella 1 makes umbrella cover Guan Bi make air drag reduce under air pressure；When umbrella forwards 12 positions counterclockwise to Time, air drag is minimized, and when crossing 12 positions, umbrella 1 starts again descending, under the resistance of air, makes umbrella 1 launches to continue next one circulation；Continuous print rotating circulating makes umbrella one open up one to close and create lift, make frame like this 9 lift-off normal flights.
- Rotating parachute mechanism the most according to claim 4 can be with Multiple Combination to reach scope and the requirement of design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410542483.8A CN105882962A (en) | 2014-10-14 | 2014-10-14 | Rotating umbrella mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410542483.8A CN105882962A (en) | 2014-10-14 | 2014-10-14 | Rotating umbrella mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105882962A true CN105882962A (en) | 2016-08-24 |
Family
ID=57001319
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410542483.8A Pending CN105882962A (en) | 2014-10-14 | 2014-10-14 | Rotating umbrella mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105882962A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191102978A (en) * | 1911-02-06 | 1911-12-07 | Joseph Maraviglia | Parachute for Flying Machines. |
| GB474005A (en) * | 1936-09-01 | 1937-10-25 | Holman Stanley Hinkson | Improvements in and relating to aircraft |
| CN2170268Y (en) * | 1993-07-15 | 1994-06-29 | 乔君旺 | Umbrella-shaped aircraft |
| CN102407941A (en) * | 2010-09-25 | 2012-04-11 | 施仲伟 | Bi-umbrella couple moment aircraft |
| CN103507952A (en) * | 2013-10-12 | 2014-01-15 | 柯依坤 | Pedaling spacecraft |
| CN103832588A (en) * | 2012-11-24 | 2014-06-04 | 刘祖学 | Large bird flying machine |
-
2014
- 2014-10-14 CN CN201410542483.8A patent/CN105882962A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191102978A (en) * | 1911-02-06 | 1911-12-07 | Joseph Maraviglia | Parachute for Flying Machines. |
| GB474005A (en) * | 1936-09-01 | 1937-10-25 | Holman Stanley Hinkson | Improvements in and relating to aircraft |
| CN2170268Y (en) * | 1993-07-15 | 1994-06-29 | 乔君旺 | Umbrella-shaped aircraft |
| CN102407941A (en) * | 2010-09-25 | 2012-04-11 | 施仲伟 | Bi-umbrella couple moment aircraft |
| CN103832588A (en) * | 2012-11-24 | 2014-06-04 | 刘祖学 | Large bird flying machine |
| CN103507952A (en) * | 2013-10-12 | 2014-01-15 | 柯依坤 | Pedaling spacecraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160824 |
|
| WD01 | Invention patent application deemed withdrawn after publication |