EA200900826A1 - Система привода воздушного винта летательного аппарата, способ привода воздушного винта летательного аппарата, применение подшипника и применение электрической машины для привода воздушного винта летательного аппарата - Google Patents
Система привода воздушного винта летательного аппарата, способ привода воздушного винта летательного аппарата, применение подшипника и применение электрической машины для привода воздушного винта летательного аппаратаInfo
- Publication number
- EA200900826A1 EA200900826A1 EA200900826A EA200900826A EA200900826A1 EA 200900826 A1 EA200900826 A1 EA 200900826A1 EA 200900826 A EA200900826 A EA 200900826A EA 200900826 A EA200900826 A EA 200900826A EA 200900826 A1 EA200900826 A1 EA 200900826A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- air screw
- screw drive
- application
- drive system
- electric machine
- Prior art date
Links
- 230000005540 biological transmission Effects 0.000 abstract 2
- 238000013016 damping Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/12—Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
- F16F15/131—Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses
- F16F15/133—Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon the rotating system comprising two or more gyratory masses using springs as elastic members, e.g. metallic springs
- F16F15/134—Wound springs
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2121—Flywheel, motion smoothing-type
- Y10T74/2132—Structural detail, e.g., fiber, held by magnet, etc.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Hybrid Electric Vehicles (AREA)
- Motor Power Transmission Devices (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Vibration Prevention Devices (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Arrangement Of Transmissions (AREA)
Abstract
В предлагаемом изобретении раскрывается обеспечивающая более эффективное гашение вибраций система привода винта летательного аппарата, содержащая винт, двигатель и приводную трансмиссию между винтом и двигателем. Приводная трансмиссия предлагаемой системы привода винта летательного аппарата снабжена торсионным демпфером.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007002889 | 2007-01-15 | ||
DE102007055336A DE102007055336A1 (de) | 2007-01-15 | 2007-11-19 | Flugzeugpropellerantrieb, Verfahren zum Antreiben eines Flugzeugpropellers und Verwendung eines Lagers eines Flugzeugpropellerantriebs sowie Verwendung einer Elektromaschine |
PCT/DE2008/000036 WO2008086774A2 (de) | 2007-01-15 | 2008-01-14 | Flugzeugpropellerantrieb, verfahren zum antreiben eines flugzeugpropellers und verwendung eines lagers eines flugzeugpropellerantriebs sowie verwendung einer elektromaschine |
Publications (1)
Publication Number | Publication Date |
---|---|
EA200900826A1 true EA200900826A1 (ru) | 2010-04-30 |
Family
ID=39628258
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA200900826A EA200900826A1 (ru) | 2007-01-15 | 2008-01-14 | Система привода воздушного винта летательного аппарата, способ привода воздушного винта летательного аппарата, применение подшипника и применение электрической машины для привода воздушного винта летательного аппарата |
Country Status (6)
Country | Link |
---|---|
US (1) | US20100038473A1 (ru) |
EP (1) | EP2109566A2 (ru) |
CN (1) | CN101610949A (ru) |
DE (2) | DE102007055336A1 (ru) |
EA (1) | EA200900826A1 (ru) |
WO (1) | WO2008086774A2 (ru) |
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WO2012102698A1 (en) * | 2011-01-24 | 2012-08-02 | Smith Frick A | Apparatus and method for vertical take-off and landing aircraft |
DE102012203778A1 (de) | 2011-04-04 | 2012-10-04 | Schaeffler Technologies AG & Co. KG | Verfahren zur Steuerung eines hybridischen Antriebsstrangs und Akkumulatoreinrichtung in diesem |
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US3103604A (en) * | 1963-09-10 | Combination clutch | ||
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DE2528508A1 (de) * | 1975-06-26 | 1977-01-20 | Ernst Pfeifer | Kolbentriebwerk zum antrieb einer luftschraube |
EP0304577B1 (en) * | 1984-07-19 | 1994-04-20 | Aisin Seiki Kabushiki Kaisha | Torque variation absorbing device |
DE19803947C1 (de) * | 1998-02-02 | 1999-03-18 | Deutsch Zentr Luft & Raumfahrt | Anordnung und Verfahren zur Minderung des Überfluggeräusches von Propellerflugzeugen |
DE19930397B4 (de) * | 1999-07-01 | 2005-02-10 | Daimlerchrysler Ag | Zweimassenschwungrad |
DE10042674A1 (de) * | 2000-08-31 | 2002-03-14 | Baier Wolfgang | Antriebsaggregat für Flugzeuge |
-
2007
- 2007-11-19 DE DE102007055336A patent/DE102007055336A1/de not_active Withdrawn
-
2008
- 2008-01-14 US US12/448,900 patent/US20100038473A1/en not_active Abandoned
- 2008-01-14 DE DE112008000117T patent/DE112008000117A5/de not_active Ceased
- 2008-01-14 EP EP08706739A patent/EP2109566A2/de not_active Withdrawn
- 2008-01-14 CN CNA2008800023129A patent/CN101610949A/zh active Pending
- 2008-01-14 WO PCT/DE2008/000036 patent/WO2008086774A2/de active Application Filing
- 2008-01-14 EA EA200900826A patent/EA200900826A1/ru unknown
Also Published As
Publication number | Publication date |
---|---|
DE112008000117A5 (de) | 2010-05-06 |
EP2109566A2 (de) | 2009-10-21 |
WO2008086774A2 (de) | 2008-07-24 |
WO2008086774A8 (de) | 2008-12-04 |
DE102007055336A1 (de) | 2008-08-21 |
WO2008086774A3 (de) | 2008-09-18 |
CN101610949A (zh) | 2009-12-23 |
US20100038473A1 (en) | 2010-02-18 |
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