WO2009013323A3 - Aerodynamisches profil, aktor zur verwendung darin sowie damit versehenes versuchsmodell - Google Patents
Aerodynamisches profil, aktor zur verwendung darin sowie damit versehenes versuchsmodell Download PDFInfo
- Publication number
- WO2009013323A3 WO2009013323A3 PCT/EP2008/059673 EP2008059673W WO2009013323A3 WO 2009013323 A3 WO2009013323 A3 WO 2009013323A3 EP 2008059673 W EP2008059673 W EP 2008059673W WO 2009013323 A3 WO2009013323 A3 WO 2009013323A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rear edge
- actuator
- aerodynamic profile
- test model
- model provided
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
- B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
- B64C27/615—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including flaps mounted on blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N30/00—Piezoelectric or electrostrictive devices
- H10N30/20—Piezoelectric or electrostrictive devices with electrical input and mechanical output, e.g. functioning as actuators or vibrators
- H10N30/204—Piezoelectric or electrostrictive devices with electrical input and mechanical output, e.g. functioning as actuators or vibrators using bending displacement, e.g. unimorph, bimorph or multimorph cantilever or membrane benders
- H10N30/2041—Beam type
- H10N30/2042—Cantilevers, i.e. having one fixed end
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/72—Means acting on blades
- B64C2027/7205—Means acting on blades on each blade individually, e.g. individual blade control [IBC]
- B64C2027/7261—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps
- B64C2027/7266—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators
- B64C2027/7283—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators of the piezoelectric type
-
- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
Die Erfindung betrifft ein aerodynamisches Profil (400), das an einer einer Anströmung (S) abzuwendenden Seite einen eine Hinterkante (412) bildenden Hinterkantenbereich (410) hat. Um die Hinterkante (412) auch für schnelle Regelungen bei einfachem Aufbau und extremer Miniaturisierbarkeit verlagern oder verformen zu können, wird vorgeschlagen, dass ein Aktor (418), der ein gesteuert kontrahierbares oder expandierbares Material oder Element (432) aufweist, im Inneren des Hinterkantenbereichs (410) zur zumindest teilweisen Lageveränderung und/oder Verformung der Hinterkante (412) und/oder des des Hinterkantenbereichs (410) vorgesehen ist.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007035463.2 | 2007-07-26 | ||
DE102007035463A DE102007035463A1 (de) | 2007-07-26 | 2007-07-26 | Aerodynamisches Profil, Aktor zur Verwendung darin sowie damit versehenes Versuchsmodell |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009013323A2 WO2009013323A2 (de) | 2009-01-29 |
WO2009013323A3 true WO2009013323A3 (de) | 2009-04-02 |
Family
ID=40175657
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2008/059673 WO2009013323A2 (de) | 2007-07-26 | 2008-07-23 | Aerodynamisches profil, aktor zur verwendung darin sowie damit versehenes versuchsmodell |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102007035463A1 (de) |
WO (1) | WO2009013323A2 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013107453A1 (en) * | 2012-01-17 | 2013-07-25 | Danfoss Polypower A/S | Transducer activated morphing structure |
CN104502056B (zh) * | 2014-11-28 | 2017-12-05 | 中国航空工业空气动力研究院 | 飞机风洞试验模型边条翼上反角可控运动系统 |
CN109000911B (zh) * | 2018-06-26 | 2024-02-02 | 哈尔滨电气股份有限公司 | 一种用于叶片热机械疲劳-蠕变的试验装置 |
CN114412953B (zh) * | 2021-12-24 | 2022-11-25 | 南京航空航天大学 | 基于被动控制的直升机旋翼压电薄膜抑振结构及方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5224826A (en) * | 1989-07-26 | 1993-07-06 | Massachusetts Institute Of Technology | Piezoelectric helicopter blade flap actuator |
US6048622A (en) * | 1994-04-19 | 2000-04-11 | Massachusetts Institute Of Technology | Composites for structural control |
US6375127B1 (en) * | 2000-07-07 | 2002-04-23 | Kari Appa | Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression |
WO2004069651A1 (de) * | 2003-02-04 | 2004-08-19 | Eads Deutschland Gmbh | Verformbares aerodynamisches profil |
DE10334267A1 (de) * | 2003-07-25 | 2005-02-24 | Eurocopter Deutschland Gmbh | Rotorblatt mit elastisch beweglicher Rotorblatt-Klappe sowie Drehflügelflugzeug mit einem solchen Rotorblatt |
WO2007071231A1 (de) * | 2005-12-21 | 2007-06-28 | Eads Deutschland Gmbh | Dreidimensionales stapelpiezoelement und piezoelektrischer aktuator mit einem solchen stapelpiezoelement |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19923087B4 (de) * | 1999-05-20 | 2004-02-26 | Eads Deutschland Gmbh | Vorrichtung zur Druck-, Schall- und Vibrationsmessung, sowie Verfahren zur Strömungsanalyse an Bauteiloberflächen |
US7015624B1 (en) * | 1999-10-22 | 2006-03-21 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Non-uniform thickness electroactive device |
DE102004055996A1 (de) * | 2004-11-19 | 2006-05-24 | Stefan Eickenberg | Biegeaktuator |
-
2007
- 2007-07-26 DE DE102007035463A patent/DE102007035463A1/de not_active Withdrawn
-
2008
- 2008-07-23 WO PCT/EP2008/059673 patent/WO2009013323A2/de active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5224826A (en) * | 1989-07-26 | 1993-07-06 | Massachusetts Institute Of Technology | Piezoelectric helicopter blade flap actuator |
US6048622A (en) * | 1994-04-19 | 2000-04-11 | Massachusetts Institute Of Technology | Composites for structural control |
US6375127B1 (en) * | 2000-07-07 | 2002-04-23 | Kari Appa | Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression |
WO2004069651A1 (de) * | 2003-02-04 | 2004-08-19 | Eads Deutschland Gmbh | Verformbares aerodynamisches profil |
DE10334267A1 (de) * | 2003-07-25 | 2005-02-24 | Eurocopter Deutschland Gmbh | Rotorblatt mit elastisch beweglicher Rotorblatt-Klappe sowie Drehflügelflugzeug mit einem solchen Rotorblatt |
WO2007071231A1 (de) * | 2005-12-21 | 2007-06-28 | Eads Deutschland Gmbh | Dreidimensionales stapelpiezoelement und piezoelektrischer aktuator mit einem solchen stapelpiezoelement |
Also Published As
Publication number | Publication date |
---|---|
WO2009013323A2 (de) | 2009-01-29 |
DE102007035463A1 (de) | 2009-02-05 |
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