DE102005003028A1 - Rotor arrangement for model or micro helicopter has main rotor with further drive rotors connected rigidly or vertically adjustable for fixing immovable anywhere along relevant motor on drive sleeve - Google Patents
Rotor arrangement for model or micro helicopter has main rotor with further drive rotors connected rigidly or vertically adjustable for fixing immovable anywhere along relevant motor on drive sleeve Download PDFInfo
- Publication number
- DE102005003028A1 DE102005003028A1 DE102005003028A DE102005003028A DE102005003028A1 DE 102005003028 A1 DE102005003028 A1 DE 102005003028A1 DE 102005003028 A DE102005003028 A DE 102005003028A DE 102005003028 A DE102005003028 A DE 102005003028A DE 102005003028 A1 DE102005003028 A1 DE 102005003028A1
- Authority
- DE
- Germany
- Prior art keywords
- rotor
- rotors
- control units
- main rotor
- rotor arrangement
- 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- Withdrawn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
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/12—Helicopters ; Flying tops
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/80—UAVs characterised by their small size, e.g. micro air vehicles [MAV]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/60—UAVs characterised by the material
- B64U20/65—Composite materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Description
Die Erfindung betrifft eine Rotoranordnung für einen Modellhubschrauber oder Mikrohubschrauber nach dem Oberbegriff des Hauptanspruchs (1).The The invention relates to a rotor assembly for a model helicopter or micro helicopter according to the preamble of the main claim (1).
Im Stand der Technik werden Ausführungsformen verschiedenartiger Rotoranordnungen beschrieben.in the The state of the art becomes embodiments various rotor assemblies described.
Aufgabe der Erfindung ist es eine Rotoranordnung vorzustellen, deren Eigenschaften ein stabileres aerodynamisches Verhalten erwarten lassen.task The invention is to present a rotor assembly whose properties to expect a more stable aerodynamic behavior.
Diese Aufgabe wird durch eine Rotoranordnung nach den Merkmalen des Anspruchs 1 gelöst.These The object is achieved by a rotor assembly according to the features of the claim 1 solved.
In folgendem wird die Erfindung anhand eines bevorzugten Ausführungsbeispiels in Verbindung mit zwei Zeichnungen beschrieben. Dabei zeigt:In The following is the invention with reference to a preferred embodiment described in conjunction with two drawings. Showing:
Erfindungsgemäß weist
der Hauptrotor (
Die
Steuereinheiten (A, B, C) mit den Steuerrotoren (
- 11
- Mikrohubschraubermicro helicopter
- 22
- Steuerrotorcontrol rotor
- 33
- Motorengine
- 44
- Drehrichtungdirection of rotation
- 55
- Rumpfhull
- 66
- Hauptrotormain rotor
- 77
- Antriebshülse drive sleeve
- 88th
- Motorengine
- 9 9
- Drehrichtungdirection of rotation
- 1010
- luftdurchlässige Öffnungenair-permeable openings
- 11 11
- Antriebshülsedrive sleeve
- 20, 21, 2220 21, 22
- Landevorrichtunglanding device
- 3030
- ovalförmiges Schutzgitteroval shaped protective grid
- AA
- Steuereinheitcontrol unit
- B, C B C
- Steuereinheitcontrol unit
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005003028A DE102005003028A1 (en) | 2005-01-22 | 2005-01-22 | Rotor arrangement for model or micro helicopter has main rotor with further drive rotors connected rigidly or vertically adjustable for fixing immovable anywhere along relevant motor on drive sleeve |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005003028A DE102005003028A1 (en) | 2005-01-22 | 2005-01-22 | Rotor arrangement for model or micro helicopter has main rotor with further drive rotors connected rigidly or vertically adjustable for fixing immovable anywhere along relevant motor on drive sleeve |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102005003028A1 true DE102005003028A1 (en) | 2006-07-27 |
Family
ID=36650529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102005003028A Withdrawn DE102005003028A1 (en) | 2005-01-22 | 2005-01-22 | Rotor arrangement for model or micro helicopter has main rotor with further drive rotors connected rigidly or vertically adjustable for fixing immovable anywhere along relevant motor on drive sleeve |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102005003028A1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2937306A1 (en) * | 2008-10-20 | 2010-04-23 | Breizhtech | Amphibious gyropendular drone for use in e.g. defense application, has safety device arranged in periphery of propulsion device for assuring floatability of drone, and upper propulsion device for maintaining drone in air during levitation |
FR2959208A1 (en) * | 2010-04-22 | 2011-10-28 | Eurl Jmdtheque | GYROPENDULAR ENGINE WITH COMPENSATORY PROPULSION AND COLLIMATION OF MULTIMODAL MULTI-MEDIUM FLUID FLOWING GRADIENT WITH VERTICAL LANDING AND LANDING |
CN102390528A (en) * | 2011-10-21 | 2012-03-28 | 南京理工大学 | Air flight and omnibearing adsorption micro-robot |
WO2013060693A2 (en) | 2011-10-27 | 2013-05-02 | Desaulniers Jean-Marc Joseph | Active geometric exoskeleton with pseudo-rhombohedral annular fairing for gyropendular craft |
ITPI20130081A1 (en) * | 2013-09-10 | 2015-03-11 | Sandro Moretti | PERFECT STRUCTURE OF DRONE |
WO2015061857A1 (en) * | 2013-11-01 | 2015-05-07 | The University Of Queensland | A rotorcraft |
WO2015109322A1 (en) * | 2014-01-20 | 2015-07-23 | Robodub Inc. | Multicopters with variable flight characteristics |
CN105034729A (en) * | 2015-07-21 | 2015-11-11 | 中国科学院自动化研究所 | Deformable multi-mode ground and air flying robot |
FR3032687A1 (en) * | 2015-02-16 | 2016-08-19 | Hutchinson | AERODYNE VTOL WITH A SOUFFLANTE (S) AXIALE (S) CARRIER (S) |
WO2018139661A1 (en) * | 2017-01-30 | 2018-08-02 | 日本電産株式会社 | Unmanned aircraft |
US10315759B2 (en) * | 2015-04-04 | 2019-06-11 | California Institute Of Technology | Multi-rotor vehicle with yaw control and autorotation |
CN110127053A (en) * | 2019-05-08 | 2019-08-16 | 重庆大学 | Portable and collapsible flies-adsorbs patrol unmanned machine |
WO2020002147A1 (en) * | 2018-06-29 | 2020-01-02 | Robert Bosch Gmbh | Flying device |
US20220194573A1 (en) * | 2020-12-22 | 2022-06-23 | California Institute Of Technology | Thrusters for Multi-Copter Yaw Control and Forward Flight |
-
2005
- 2005-01-22 DE DE102005003028A patent/DE102005003028A1/en not_active Withdrawn
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2937306A1 (en) * | 2008-10-20 | 2010-04-23 | Breizhtech | Amphibious gyropendular drone for use in e.g. defense application, has safety device arranged in periphery of propulsion device for assuring floatability of drone, and upper propulsion device for maintaining drone in air during levitation |
FR2959208A1 (en) * | 2010-04-22 | 2011-10-28 | Eurl Jmdtheque | GYROPENDULAR ENGINE WITH COMPENSATORY PROPULSION AND COLLIMATION OF MULTIMODAL MULTI-MEDIUM FLUID FLOWING GRADIENT WITH VERTICAL LANDING AND LANDING |
WO2011131733A3 (en) * | 2010-04-22 | 2011-12-29 | Desaulniers Jean-Marc Joseph | Vertical take-off and landing multimodal, multienvironment, gyropendular craft with compensatory propulsion and fluidic gradient collimation |
CN102390528A (en) * | 2011-10-21 | 2012-03-28 | 南京理工大学 | Air flight and omnibearing adsorption micro-robot |
CN102390528B (en) * | 2011-10-21 | 2014-01-08 | 南京理工大学 | Air flight and omnibearing adsorption micro-robot |
WO2013060693A2 (en) | 2011-10-27 | 2013-05-02 | Desaulniers Jean-Marc Joseph | Active geometric exoskeleton with pseudo-rhombohedral annular fairing for gyropendular craft |
ITPI20130081A1 (en) * | 2013-09-10 | 2015-03-11 | Sandro Moretti | PERFECT STRUCTURE OF DRONE |
WO2015036907A1 (en) * | 2013-09-10 | 2015-03-19 | Università Degli Studi Di Firenze | An improved drone structure |
US10081432B2 (en) | 2013-09-10 | 2018-09-25 | Universita Degli Studi Di Firenze | Drone structure |
WO2015061857A1 (en) * | 2013-11-01 | 2015-05-07 | The University Of Queensland | A rotorcraft |
AU2014344813B2 (en) * | 2013-11-01 | 2018-09-13 | The University Of Queensland | A rotorcraft |
US10124888B2 (en) | 2013-11-01 | 2018-11-13 | The University Of Queensland | Rotorcraft |
US10407162B2 (en) | 2014-01-20 | 2019-09-10 | Robodub Inc. | Multicopters with variable flight characteristics |
CN106061838A (en) * | 2014-01-20 | 2016-10-26 | 罗博杜伯公司 | Multicopters with variable flight characteristics |
WO2015109322A1 (en) * | 2014-01-20 | 2015-07-23 | Robodub Inc. | Multicopters with variable flight characteristics |
FR3032687A1 (en) * | 2015-02-16 | 2016-08-19 | Hutchinson | AERODYNE VTOL WITH A SOUFFLANTE (S) AXIALE (S) CARRIER (S) |
WO2016132040A1 (en) * | 2015-02-16 | 2016-08-25 | Hutchinson | Vtol aerodyne with supporting axial blower(s) |
US9902493B2 (en) | 2015-02-16 | 2018-02-27 | Hutchinson | VTOL aerodyne with supporting axial blower(s) |
US10315759B2 (en) * | 2015-04-04 | 2019-06-11 | California Institute Of Technology | Multi-rotor vehicle with yaw control and autorotation |
CN105034729B (en) * | 2015-07-21 | 2017-05-24 | 中国科学院自动化研究所 | Deformable multi-mode ground and air flying robot |
CN105034729A (en) * | 2015-07-21 | 2015-11-11 | 中国科学院自动化研究所 | Deformable multi-mode ground and air flying robot |
WO2018139661A1 (en) * | 2017-01-30 | 2018-08-02 | 日本電産株式会社 | Unmanned aircraft |
CN110167839A (en) * | 2017-01-30 | 2019-08-23 | 日本电产株式会社 | Unmanned flight's body |
JPWO2018139661A1 (en) * | 2017-01-30 | 2019-11-14 | 日本電産株式会社 | Unmanned aerial vehicle |
WO2020002147A1 (en) * | 2018-06-29 | 2020-01-02 | Robert Bosch Gmbh | Flying device |
CN110127053A (en) * | 2019-05-08 | 2019-08-16 | 重庆大学 | Portable and collapsible flies-adsorbs patrol unmanned machine |
CN110127053B (en) * | 2019-05-08 | 2021-03-26 | 重庆大学 | Portable foldable flying-adsorbing inspection unmanned aerial vehicle |
US20220194573A1 (en) * | 2020-12-22 | 2022-06-23 | California Institute Of Technology | Thrusters for Multi-Copter Yaw Control and Forward Flight |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8122 | Nonbinding interest in granting licences declared | ||
8139 | Disposal/non-payment of the annual fee |