CN105799926A - Autorotation device - Google Patents
Autorotation device Download PDFInfo
- Publication number
- CN105799926A CN105799926A CN201610278860.0A CN201610278860A CN105799926A CN 105799926 A CN105799926 A CN 105799926A CN 201610278860 A CN201610278860 A CN 201610278860A CN 105799926 A CN105799926 A CN 105799926A
- Authority
- CN
- China
- Prior art keywords
- propeller
- rotor
- anger
- calming
- stator
- 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
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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
Abstract
The invention relates to an autorotation device. According to the autorotation device, novel aerodynamic configuration is adopted, air is pressed under lift-force rotor wings by air pressing propellers, then, secondary compression is carried out so as to enable the lift-force rotor wings to generate a lifting force, and thus an airframe can rise vertically. The device can be applied to all underwater, aerial and waterborne watercrafts and model airplane toys.
Description
The present invention relates to " from rotary body device ".It is that the innovation and creation that the present inventor proposes are called " a kind of manned No Tail Rotor vertically taking off and landing flyer "；Application number is 201310418431.5；The applying date is transform on the basis applied for a patent for 13rd for 09 month for 2013 to form.
Straight the traditional straight vapour used by aircraft, diesel internal combustion electromotor, turbojet or motor, rotary course is fixed on body motionless by the shell of electromotor or motor, armature spindle carrying screws rotates and produces lift, otherwise rotor is fixed on body motionless, rotarily driven propeller rotational by shell and produce the form of lift, its shortcoming, it is improving rotating speed and can to the certain side twisting resistance of aircraft lift while, especially the straight aircraft playing straight class shape, the device that have to arrange the counteracting force offset under the different rotating speeds that propeller produces on body just can stabilize it rising, the power of a part of electromotor can be lost, here it is a traditional straight straight aircraft disadvantage.
" from rotary body device " provided by the present invention just overcomes disadvantage mentioned above, it is possible to need not arrange the device of counteracting counterforce, such as rear empennage etc..The aerodynamic arrangement's " from rotary body device " utilizing state-of-the art calm the anger propeller and lifting rotor just can make stable machine directly straight.
" from rotary body device " provided by the present invention, is by bavin, gasoline engine；Under turbojet or the respective rotor of motor, axle 2 and stator 1 respectively arrange one pair of calm the anger propeller 6 and lifting rotor 9；The rotor upper shaft 3 of propeller 6 of calming the anger and stator 1 are arranged in square frame 10, square frame 10 is provided with the mechanism that the dead eye 7,8 of the rotor upper shaft 3 that may pass through propeller 6 of calming the anger and stator 1 correspondence mutually forms, the propeller that it is characterized in that calming the anger rotates towards the other side's rightabout with lifting rotor, just can balance the effect of body torsion without gear drive, make body can do VTOL campaign.Architectural feature and the purpose of the present invention is further illustrated below in conjunction with accompanying drawing.
Brief Description Of Drawings:
Fig. 1 is the basic structure schematic diagram for " from rotary body device " provided by the present invention.
Fig. 2 looks schematic diagram for the basic structure internal organs of " from rotary body device " provided by the present invention.
Please see Figure 1, shown in Fig. 2, it is mainly when energising, under motor rotor, axle 2 upper rotor part axle 3 rotates, band action pneumatic propeller 6 rotates simultaneously, gives stator 1 rightabout power simultaneously, makes stator 1 drive lifting rotor 9 opposite direction to rotate, along with faster rotational speed, 6 air of propeller of calming the anger are compressed in the bottom of lifting rotor 9, and lifting rotor 9 carries out second-compressed air again, make body create lift and make body ramp.Because motor is free body, so, square frame 10 is absent from counteracting force.
From rotary body device, can be used for, on aerial straight straight aircraft, under water aircraft and water surface ship ship, material to be saved；Reduce volume；Without travelling gear, the feature of weight saving.
Claims (6)
1. provided by the present invention from rotary body device, it is by bavin, gasoline engine；Under turbojet or the respective rotor of motor, axle 2 and stator 1 respectively arrange one pair of calm the anger propeller 6 and lifting rotor 9；The armature spindle upper shaft 3 of propeller 6 of calming the anger and stator 1 are arranged in square frame 10, are provided with the rotor upper shaft 3 that may pass through propeller 6 of calming the anger and mechanism that the mutually corresponding dead eye 7,8 of stator 1 forms on square frame 10.
2. rotate towards the other side's rightabout with lifting rotor from the rotary body device propeller that it is characterized in that calming the anger according to claim 1, just can balance the effect of body torsion without gear drive, make body can do VTOL campaign.
3. it is characterized in that main when energising in conjunction with accompanying drawing Fig. 1, Fig. 2 from rotary body device according to claim 1 and 2, under motor rotor, axle 2 rotates, simultaneously, rotor driven upper shaft 3 and propeller 6 of calming the anger rotate, and give stator 1 rightabout power simultaneously, make stator 1 drive lifting rotor 9 opposite direction to rotate, along with faster rotational speed, 6 air of propeller of calming the anger are compressed in the bottom of lifting rotor 9, and lifting rotor 9 carries out second-compressed air again, make body create lift and make body ramp.Because motor is free body, so, square frame 10 is absent from counteracting force.
4. according to claim 1,2,3 from rotary body device rotation body device, can be used for aerial straight rise on straight aircraft, under water aircraft and water surface ship ship, material can be saved；Reduce volume；Without travelling gear, the feature of weight saving.
5. can be used on ship model toy from rotary body device according to claim 1,2,3,4.
6. the rotating device according to claim 1,2,3,4,5 calm the anger propeller and lifting rotor can each be used alone electromotor or motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610278860.0A CN105799926A (en) | 2016-05-03 | 2016-05-03 | Autorotation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610278860.0A CN105799926A (en) | 2016-05-03 | 2016-05-03 | Autorotation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105799926A true CN105799926A (en) | 2016-07-27 |
Family
ID=56458104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610278860.0A Pending CN105799926A (en) | 2016-05-03 | 2016-05-03 | Autorotation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105799926A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2805398A1 (en) * | 2020-05-19 | 2021-02-11 | Gonzalez Unai Irastorza | Motor autorotation device (Machine-translation by Google Translate, not legally binding) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008094277A (en) * | 2006-10-12 | 2008-04-24 | Osaka Prefecture Univ | Double reversal rotation impeller machine |
| CN101177167A (en) * | 2007-12-11 | 2008-05-14 | 周公平 | Power-driven system of aircraft |
| CN201089520Y (en) * | 2007-07-19 | 2008-07-23 | 樊文炎 | Gyroscope type vertically elevating flight device |
| CN101244762A (en) * | 2008-03-21 | 2008-08-20 | 周公平 | Power-driven system of aerial vehicle |
| CN103847960A (en) * | 2014-03-20 | 2014-06-11 | 西北工业大学 | Composite rotation driving vertical take-off and landing aircraft |
-
2016
- 2016-05-03 CN CN201610278860.0A patent/CN105799926A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008094277A (en) * | 2006-10-12 | 2008-04-24 | Osaka Prefecture Univ | Double reversal rotation impeller machine |
| CN201089520Y (en) * | 2007-07-19 | 2008-07-23 | 樊文炎 | Gyroscope type vertically elevating flight device |
| CN101177167A (en) * | 2007-12-11 | 2008-05-14 | 周公平 | Power-driven system of aircraft |
| CN101244762A (en) * | 2008-03-21 | 2008-08-20 | 周公平 | Power-driven system of aerial vehicle |
| CN103847960A (en) * | 2014-03-20 | 2014-06-11 | 西北工业大学 | Composite rotation driving vertical take-off and landing aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2805398A1 (en) * | 2020-05-19 | 2021-02-11 | Gonzalez Unai Irastorza | Motor autorotation device (Machine-translation by Google Translate, not legally binding) |
| WO2021234195A1 (en) * | 2020-05-19 | 2021-11-25 | Irastorza Gonzalez Unai | Engine autorotation device |
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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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160727 |
|
| RJ01 | Rejection of invention patent application after publication |