DE202006013909U1 - Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires - Google Patents
Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires Download PDFInfo
- Publication number
- DE202006013909U1 DE202006013909U1 DE202006013909U DE202006013909U DE202006013909U1 DE 202006013909 U1 DE202006013909 U1 DE 202006013909U1 DE 202006013909 U DE202006013909 U DE 202006013909U DE 202006013909 U DE202006013909 U DE 202006013909U DE 202006013909 U1 DE202006013909 U1 DE 202006013909U1
- Authority
- DE
- Germany
- Prior art keywords
- base unit
- fixed
- aircraft according
- aircraft
- plug
- 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.)
- Expired - Lifetime
Links
- 230000035939 shock Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical class C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000002918 waste heat Substances 0.000 description 1
Classifications
-
- 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
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/291—Detachable rotors or rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2211/00—Modular constructions of airplanes or helicopters
-
- 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
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
Description
Technisches UmfeldTechnical environment
Offenbarung der ErfindungDisclosure of the invention
Technisches ProblemTechnical problem
Technische LösungTechnical solution
Kurze Beschreibung von ZeichnungenShort description of drawings
Die Neuerung betrifft ein Fluggerät, insbesondere einen Quadrocopter.The Innovation relates to an aircraft, especially a quadrocopter.
Der Neuerung liegt die Aufgabe zugrunde, Fluggerät, insbesondere einen Quadrocopter, anzubieten, der vorteilhaft montierbar ist.Of the Innovation is based on the object, aircraft, in particular a quadrocopter, offer, which is advantageous mountable.
Funktionsprinzip Quadrocopter – Prinzipieller AufbauOperating principle Quadrocopter - Prinzipieller construction
Ein Quadrocopter definiert sich durch einen vorzugsweise kreuzförmigen Aufbau mit jeweils einer Antriebseinheit samt Luftschraube an den vier Enden. Durch Variation der Schubleistung der einzelnen Antriebseinheiten ist eine nahezu uneingeschränkte Bewegung im dreidimensionalen Raum möglich. Eine prozessorgestützte Elektronik setzt die Steuersignale des Piloten für die Motorregelung um und unterstützt durch Sensoren die Lagestabilisierung. Das Funktionsprinzip definiert die bauliche Umsetzung weitgehend. Die Basis bildet die mittig angeordnete Elektronik und Spannungsversorgung in der die Lagesensorik integriert ist. Die 4 Motoreinheiten befinden sich kreuzförmig punktsymmetrisch im Bezug auf die Basis.One Quadrocopter defined by a preferably cross-shaped structure each with a drive unit including propeller at the four End up. By varying the thrust of the individual drive units is an almost unrestricted movement possible in three-dimensional space. A processor-based Electronics converts the pilot control signals for engine control and supports by sensors the position stabilization. The functional principle defined the structural implementation largely. The basis is the centrally arranged electronics and power supply in which the position sensor is integrated. The 4 motor units are crosswise point symmetrical with respect to the base.
Modularer Aufbau des neuerungsgemäßen QuadrocoptersModular structure of the inventive quadrocopter
Eine wesentliche Eigenschaft des hier beschriebenen Aufbaus stellt die Modularität dar. Die Elemente sind durch leicht lösbare Verbindungen gefügt und können dadurch im Service- oder Versagensfall leicht ausgetauscht werden. Der Funktion folgend wurden Leichtbaumaterialien wie Aluminium, Magnesium oder Kohlefaserverbundwerkstoffe gewählt. Je nach Bedarf und Anspruch an die Konstruktion (geringes Gewicht/hohe Steifigkeit) ist es durch definierte und kompatible Schnittstellen möglich verschiedene Werkstoffkombinationen einzusetzen.A essential property of the structure described here represents the modularity The elements are joined by easily detachable connections and can thereby be easily replaced in case of service or failure. Following the function were lightweight materials such as aluminum, magnesium or carbon fiber composites selected. Depending on requirements and design requirements (low weight / high Stiffness) it is through defined and compatible interfaces possible to use different material combinations.
Einfach zu lösendes, formschlüssiges StecksystemEasy to solve, form-fitting plug-in system
Die leicht lösbaren Verbindungen des Quadrocopters können als formschlüssiges Stecksystem ausgeführt werden. Dabei ist keinerlei Klebung notwendig und alle Bauteile werden durch Formschluss zusammen gehalten. Schwankungen der Materialstärke (bei CFK bis zu +–10% haben bei dieser Art der Verbindung nahezu keine negativen Auswirkungen auf die Steifigkeit der Konstruktion. Die Fixierung der Einheit erfolgt dabei nur durch eine Schraube pro Strebenverbinder.The easily detachable Connections of the Quadrocopter can as form-fitting Plug system executed become. No gluing is necessary and all components are held together by positive locking. Fluctuations in material thickness (at CFRP up to + -10% have almost no negative effects with this type of connection on the rigidity of the construction. The fixation of the unit takes place only by a screw per strut connector.
Beispiel eines modular aufgebauten Quadrocopters gemäß den ZeichnungsfigurenExample of a modular constructed Quadrocopters according to the drawings
Im
gezeigten Beispiel (
Mehrere
in Längs-
und Querrichtung überspannende
Stoßbügel (Part
Die
kreuzförmig
angebrachten Ausleger (Part
Ein Landegestell kann aus Federstahldrähten aufgebaut sein. Diese Konstruktion des Landegestells kann schnell und kostengünstig hergestellt werden. Zudem federt es harte Landestöße optimal ab bei einem nur sehr geringen Eigengewicht. Ein Austausch aufgrund von zu harten Landungen kann aufgrund der Montage in Steckhülsen sofort und ohne Werkzeug geschehen.One Landing frame can be constructed of spring steel wires. These Construction of the landing gear can be made quickly and inexpensively become. In addition, it absorbs hard land shocks optimally from one only very low weight. An exchange due to too hard Landings may occur immediately and without tools due to mounting in receptacles happen.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE202006013909U DE202006013909U1 (en) | 2006-11-17 | 2006-12-15 | Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE202006013905.2 | 2006-11-17 | ||
DE202006013905 | 2006-11-17 | ||
DE202006013909U DE202006013909U1 (en) | 2006-11-17 | 2006-12-15 | Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires |
Publications (1)
Publication Number | Publication Date |
---|---|
DE202006013909U1 true DE202006013909U1 (en) | 2007-02-22 |
Family
ID=37833002
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE202006013909U Expired - Lifetime DE202006013909U1 (en) | 2006-11-17 | 2006-12-15 | Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE202006013909U1 (en) |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008014853A1 (en) | 2008-03-18 | 2009-10-08 | Ascending Technologies Gmbh | Rotary-wing aircraft |
DE102009001759A1 (en) * | 2009-03-23 | 2010-10-07 | Gregor Schnoell | locking system |
DE102012202698A1 (en) * | 2012-02-22 | 2013-08-22 | Syntern Gmbh | Vertical take-off and landing aircraft for transporting people or loads, has signal processing unit performing position control such that aircraft is horizontally located in space without pilot's control inputs or remote control |
CN103359282A (en) * | 2012-04-10 | 2013-10-23 | 深圳市大疆创新科技有限公司 | Multi-rotor aircraft |
WO2014067224A1 (en) * | 2012-10-29 | 2014-05-08 | 深圳市哈博森科技有限公司 | Quadcopter |
CN103786891A (en) * | 2014-01-10 | 2014-05-14 | 江苏艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle and line arrangement method thereof |
DE202014003727U1 (en) | 2014-05-06 | 2014-05-28 | Fachhochschule Westküste Hochschule für Wirtschaft & Technik | Multifunctional boom with at least one drive, in particular for use in a multi-copter system |
DE102013000168A1 (en) * | 2013-01-09 | 2014-07-10 | microdrones GmbH | Aerodynamic Multicopter / Quadrocopter |
DE102013000409A1 (en) * | 2013-01-11 | 2014-07-17 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Flying platform for military purposes as strategic drones, has mechanical- or electrical interface, through which drive- and control modules are available together for forming flight platform in direct- or indirect manner |
DE102013101194A1 (en) | 2013-02-07 | 2014-08-07 | Thorsten Boeker | Method for e.g. coloring uneven surface of house wall with hover-enabled aircraft e.g. quadrocopter, involves filling tank with treatment agent, and carrying out continuous travel of aircraft at location proximity to treatment surface |
DE102013005509A1 (en) | 2013-04-02 | 2014-10-02 | Evelin Färber | Unmanned aerial vehicle |
DE102013011378A1 (en) | 2013-07-09 | 2015-01-15 | Rauf Guliyev | Framework for a missile |
DE102013108076A1 (en) * | 2013-07-29 | 2015-01-29 | OIC-GmbH | Aircraft for carrying one or more recording devices and system therefor |
CN104627374A (en) * | 2013-11-08 | 2015-05-20 | 珠海羽人飞行器有限公司 | Agricultural unmanned aircraft |
DE102013225304A1 (en) | 2013-12-09 | 2015-06-11 | Martin Johannes Fengler | FLIGHT UNIT |
EP2933189A1 (en) * | 2014-04-17 | 2015-10-21 | Puy du Fou International | Motormount for a flying drone apparatus |
WO2015162613A1 (en) * | 2014-04-24 | 2015-10-29 | Neustadt Roi | Hovering device for drawing on walls |
WO2016124068A1 (en) * | 2015-02-02 | 2016-08-11 | 上海坚柏国际贸易有限公司 | Mobile phone shell capable of being changed into unmanned aerial vehicle |
CN105939927A (en) * | 2015-12-24 | 2016-09-14 | 深圳市大疆创新科技有限公司 | Quick-detachable structure, multi-rotor unmanned aerial vehicle, assembly, and rotor assembly |
WO2018036231A1 (en) * | 2016-08-22 | 2018-03-01 | Boe Technology Group Co., Ltd. | Unmanned aerial vehicle, wearable apparatus including unmanned aerial vehicle, wristwatch including wearable apparatus, method of operating unmanned aerial vehicle, and apparatus for operating unmanned aerial vehicle |
DE102016010873A1 (en) | 2016-09-02 | 2018-03-08 | Mario Hintze | Multicopter lightweight construction |
US10155584B2 (en) | 2012-11-15 | 2018-12-18 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
WO2019149784A1 (en) | 2018-01-30 | 2019-08-08 | Nicolle Guillaume Emmanuel Marie | Unmanned aerodyne |
EP3670965A1 (en) | 2018-12-20 | 2020-06-24 | ZF Friedrichshafen AG | Transmission device for a multicopter |
DE102013022527B3 (en) | 2013-08-23 | 2023-04-20 | DG Aviation GmbH | Central pod, boom and buoyancy support unit for a multicopter and multicopter |
DE102019128202B4 (en) | 2019-10-18 | 2023-12-07 | Emqopter GmbH | System and method for ad-hoc configuration of a modular multicopter |
-
2006
- 2006-12-15 DE DE202006013909U patent/DE202006013909U1/en not_active Expired - Lifetime
Cited By (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008014853A1 (en) | 2008-03-18 | 2009-10-08 | Ascending Technologies Gmbh | Rotary-wing aircraft |
DE102008014853B4 (en) * | 2008-03-18 | 2010-11-18 | Ascending Technologies Gmbh | Rotary-wing aircraft |
DE102009001759A1 (en) * | 2009-03-23 | 2010-10-07 | Gregor Schnoell | locking system |
DE102009001759B4 (en) * | 2009-03-23 | 2013-02-21 | Gregor Schnoell | locking system |
EP2233393A3 (en) * | 2009-03-23 | 2013-04-17 | Gregor Schnoell | Locking system |
DE102012202698B4 (en) | 2012-02-22 | 2023-06-07 | Volocopter Gmbh | aircraft |
DE102012202698A1 (en) * | 2012-02-22 | 2013-08-22 | Syntern Gmbh | Vertical take-off and landing aircraft for transporting people or loads, has signal processing unit performing position control such that aircraft is horizontally located in space without pilot's control inputs or remote control |
CN103359282A (en) * | 2012-04-10 | 2013-10-23 | 深圳市大疆创新科技有限公司 | Multi-rotor aircraft |
WO2014067224A1 (en) * | 2012-10-29 | 2014-05-08 | 深圳市哈博森科技有限公司 | Quadcopter |
US10155584B2 (en) | 2012-11-15 | 2018-12-18 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
US11338912B2 (en) | 2012-11-15 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
US10472056B2 (en) | 2012-11-15 | 2019-11-12 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
US10272994B2 (en) | 2012-11-15 | 2019-04-30 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
US10196137B2 (en) | 2012-11-15 | 2019-02-05 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
US10189562B2 (en) | 2012-11-15 | 2019-01-29 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and operations thereof |
DE102013000168A1 (en) * | 2013-01-09 | 2014-07-10 | microdrones GmbH | Aerodynamic Multicopter / Quadrocopter |
DE102013000168B4 (en) * | 2013-01-09 | 2021-06-17 | Mdgroup Germany Gmbh | Aerodynamic multicopter / quadrocopter |
DE102013000409A1 (en) * | 2013-01-11 | 2014-07-17 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Flying platform for military purposes as strategic drones, has mechanical- or electrical interface, through which drive- and control modules are available together for forming flight platform in direct- or indirect manner |
DE102013101194A1 (en) | 2013-02-07 | 2014-08-07 | Thorsten Boeker | Method for e.g. coloring uneven surface of house wall with hover-enabled aircraft e.g. quadrocopter, involves filling tank with treatment agent, and carrying out continuous travel of aircraft at location proximity to treatment surface |
DE102013005509A1 (en) | 2013-04-02 | 2014-10-02 | Evelin Färber | Unmanned aerial vehicle |
DE202013012262U1 (en) | 2013-07-09 | 2015-11-23 | Rauf Guliyev | Framework for a missile |
DE102013011378A1 (en) | 2013-07-09 | 2015-01-15 | Rauf Guliyev | Framework for a missile |
DE102013108076A1 (en) * | 2013-07-29 | 2015-01-29 | OIC-GmbH | Aircraft for carrying one or more recording devices and system therefor |
DE102013022527B3 (en) | 2013-08-23 | 2023-04-20 | DG Aviation GmbH | Central pod, boom and buoyancy support unit for a multicopter and multicopter |
CN104627374A (en) * | 2013-11-08 | 2015-05-20 | 珠海羽人飞行器有限公司 | Agricultural unmanned aircraft |
DE102013225304B4 (en) * | 2013-12-09 | 2021-06-24 | Meteomatics Gmbh | Aircraft |
US9650132B2 (en) | 2013-12-09 | 2017-05-16 | Meteomatics Gmbh | Flying machine |
DE102013225304A1 (en) | 2013-12-09 | 2015-06-11 | Martin Johannes Fengler | FLIGHT UNIT |
CN103786891B (en) * | 2014-01-10 | 2016-04-20 | 江苏艾锐泰克无人飞行器科技有限公司 | The method for sorting of unmanned vehicle and unmanned vehicle circuit |
CN103786891A (en) * | 2014-01-10 | 2014-05-14 | 江苏艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle and line arrangement method thereof |
EP2933189A1 (en) * | 2014-04-17 | 2015-10-21 | Puy du Fou International | Motormount for a flying drone apparatus |
US9815078B2 (en) | 2014-04-24 | 2017-11-14 | Roi Neustadt | Hovering device for drawing on walls |
WO2015162613A1 (en) * | 2014-04-24 | 2015-10-29 | Neustadt Roi | Hovering device for drawing on walls |
DE202014003727U1 (en) | 2014-05-06 | 2014-05-28 | Fachhochschule Westküste Hochschule für Wirtschaft & Technik | Multifunctional boom with at least one drive, in particular for use in a multi-copter system |
WO2015169279A1 (en) | 2014-05-06 | 2015-11-12 | Fachhochschule Westküste Hochschule für Wirtschaft & Technik | Multifunctional boom with at least one drive, in particular for use in a multicopter system |
WO2016124068A1 (en) * | 2015-02-02 | 2016-08-11 | 上海坚柏国际贸易有限公司 | Mobile phone shell capable of being changed into unmanned aerial vehicle |
CN105939927A (en) * | 2015-12-24 | 2016-09-14 | 深圳市大疆创新科技有限公司 | Quick-detachable structure, multi-rotor unmanned aerial vehicle, assembly, and rotor assembly |
CN105939927B (en) * | 2015-12-24 | 2020-12-08 | 深圳市大疆创新科技有限公司 | Multi-rotor unmanned aerial vehicle, assembly and rotor assembly |
US10202189B2 (en) | 2016-08-22 | 2019-02-12 | Boe Technology Group Co., Ltd. | Unmanned aerial vehicle, wearable apparatus including unmanned aerial vehicle, wristwatch including wearable apparatus, method of operating unmanned aerial vehicle, and apparatus for operating unmanned aerial vehicle |
WO2018036231A1 (en) * | 2016-08-22 | 2018-03-01 | Boe Technology Group Co., Ltd. | Unmanned aerial vehicle, wearable apparatus including unmanned aerial vehicle, wristwatch including wearable apparatus, method of operating unmanned aerial vehicle, and apparatus for operating unmanned aerial vehicle |
DE102016010873A1 (en) | 2016-09-02 | 2018-03-08 | Mario Hintze | Multicopter lightweight construction |
WO2019149784A1 (en) | 2018-01-30 | 2019-08-08 | Nicolle Guillaume Emmanuel Marie | Unmanned aerodyne |
DE102018222513A1 (en) | 2018-12-20 | 2020-06-25 | Zf Friedrichshafen Ag | Gear device for a multicopter |
EP3670965A1 (en) | 2018-12-20 | 2020-06-24 | ZF Friedrichshafen AG | Transmission device for a multicopter |
DE102019128202B4 (en) | 2019-10-18 | 2023-12-07 | Emqopter GmbH | System and method for ad-hoc configuration of a modular multicopter |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE202006013909U1 (en) | Aircraft e.g. quadrocopter, has centrally fixed base unit, hoist arms detachably fixed at base unit by plug-in and screw connections, electronic components fixed at base unit, and landing frame formed from simple wires | |
DE102013106141B4 (en) | Bearing frame for an electrically powered motor vehicle | |
EP2945856B1 (en) | Watercraft comprising a redundant energy accumulator | |
EP2860085B1 (en) | Subframe for a motor vehicle | |
DE102009040896A1 (en) | Arrangement for attaching drive assembly in engine compartment of motor vehicle, has hinged column whose axle is arranged on Y-coordinate of vehicle when viewing from vehicle transverse direction | |
DE102012215099A1 (en) | Axle carrier for a motor vehicle | |
DE102013021009A1 (en) | Engine / transmission mounting for a motor vehicle | |
DE102011106619A1 (en) | Front axle system for a vehicle and motor vehicle | |
DE102012104292A1 (en) | Isolator system for structure-borne noise decoupling for a large electrical machine | |
DE102011119590A1 (en) | Remote controllable flight platform | |
EP3197742B1 (en) | Chassis frame with drive unit | |
EP1670672A1 (en) | Fixing element of a unit for a motor vehicle | |
DE102009040164A1 (en) | Supporting structure for rail vehicle, has supporting plate made of fiber-reinforced plastic and provided with reinforcing ribs, and elastomeric connection elements provided for attaching supporting plate at component of rail vehicle | |
DE102005008636B4 (en) | Drive unit for a windscreen wiper system on a vehicle | |
DE102018103467B4 (en) | Shock damping system | |
DE19633421A1 (en) | Ship propulsion drive with vibration-damped drive motor mounting | |
DE102005014938B4 (en) | Improved engine mount for a commercial vehicle | |
DE102012206641B4 (en) | Axle bridge of a working machine | |
DE1069004B (en) | ||
DE102015107216A1 (en) | torque arm | |
DE202017006861U1 (en) | drone | |
DE2406271C3 (en) | Suspension of a unit connected to a subframe and lying with its axis in the direction of travel in the underframe of rail vehicles | |
DE202019003764U1 (en) | Detachable shock absorber mount | |
DE102014210924A1 (en) | motor vehicle | |
DE1081488B (en) | Storage of the driver's cab of a rail vehicle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
R207 | Utility model specification |
Effective date: 20070329 |
|
R156 | Lapse of ip right after 3 years |
Effective date: 20100701 |