MC200172B1 - Dispositif aérien comprenant une structure porteuse et un élément rotatif pourvu de moyens de fixation permettant de fixer au moins une pale - Google Patents
Dispositif aérien comprenant une structure porteuse et un élément rotatif pourvu de moyens de fixation permettant de fixer au moins une paleInfo
- Publication number
- MC200172B1 MC200172B1 MC2608A MC2608A MC200172B1 MC 200172 B1 MC200172 B1 MC 200172B1 MC 2608 A MC2608 A MC 2608A MC 2608 A MC2608 A MC 2608A MC 200172 B1 MC200172 B1 MC 200172B1
- Authority
- MC
- Monaco
- Prior art keywords
- attaching
- blade
- fastening means
- rotating element
- carrier structure
- Prior art date
Links
Classifications
-
- 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
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- 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
- B64C2027/8245—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 using air jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Toys (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MC2608A MC200172B1 (fr) | 2015-02-13 | 2015-02-13 | Dispositif aérien comprenant une structure porteuse et un élément rotatif pourvu de moyens de fixation permettant de fixer au moins une pale |
US15/547,757 US10800520B2 (en) | 2015-02-13 | 2016-02-05 | Aviation device comprising a bearing structure and a rotating member equipped with fixing means which make it possible to fix at least one blade |
PCT/EP2016/052561 WO2016128330A1 (fr) | 2015-02-13 | 2016-02-05 | Dispositif aerien comprenant une structure porteuse et un element rotatif pourvu de moyens de fixation permettant de fixer au moins une pale et un dispositif pour controler le lacet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MC2608A MC200172B1 (fr) | 2015-02-13 | 2015-02-13 | Dispositif aérien comprenant une structure porteuse et un élément rotatif pourvu de moyens de fixation permettant de fixer au moins une pale |
Publications (1)
Publication Number | Publication Date |
---|---|
MC200172B1 true MC200172B1 (fr) | 2016-04-15 |
Family
ID=55409808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MC2608A MC200172B1 (fr) | 2015-02-13 | 2015-02-13 | Dispositif aérien comprenant une structure porteuse et un élément rotatif pourvu de moyens de fixation permettant de fixer au moins une pale |
Country Status (3)
Country | Link |
---|---|
US (1) | US10800520B2 (fr) |
MC (1) | MC200172B1 (fr) |
WO (1) | WO2016128330A1 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11186363B2 (en) | 2015-10-21 | 2021-11-30 | Sikorsky Aircraft Corporation | Electric propulsion system for a rotary wing aircraft |
US10526085B2 (en) | 2016-06-03 | 2020-01-07 | Bell Textron Inc. | Electric distributed propulsion anti-torque redundant power and control system |
US10377479B2 (en) | 2016-06-03 | 2019-08-13 | Bell Helicopter Textron Inc. | Variable directional thrust for helicopter tail anti-torque system |
US10703471B2 (en) | 2016-06-03 | 2020-07-07 | Bell Helicopter Textron Inc. | Anti-torque control using matrix of fixed blade pitch motor modules |
US10752343B2 (en) | 2016-10-18 | 2020-08-25 | Sikorsky Aircraft Corporation | Electric propulsion system for a rotary wing aircraft |
US10577090B2 (en) | 2017-02-16 | 2020-03-03 | Sikorsky Aircraft Corporation | Electric propulsion system with overrunning clutch for a rotary-wing aircraft |
CN107150788A (zh) * | 2017-04-26 | 2017-09-12 | 朱晓义 | 一种产生更大升力的固定翼飞行器 |
US11186185B2 (en) | 2017-05-31 | 2021-11-30 | Textron Innovations Inc. | Rotor brake effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor |
US10974824B2 (en) | 2017-07-20 | 2021-04-13 | Sikorsky Aircraft Corporation | Electric powered direct drive rotor motor |
US10676182B2 (en) | 2017-07-20 | 2020-06-09 | Sikorsky Aircraft Corporation | Tilting coaxial rotor for a rotary wing aircraft |
US10407166B2 (en) | 2018-01-08 | 2019-09-10 | Sikorsky Aircraft Corporation | Yaw moment supplement for directional control |
CN112424065A (zh) * | 2018-03-28 | 2021-02-26 | 德瓦尔奇多元化有限责任合伙公司 | 航空器推进和扭矩减缓技术 |
Family Cites Families (46)
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US2437700A (en) * | 1948-03-16 | Aircraft | ||
US2509359A (en) * | 1945-06-28 | 1950-05-30 | Margolis Isadore | Rotary jet engine |
GB612189A (en) | 1946-05-17 | 1948-11-09 | Cierva Autogiro Co Ltd | Improvements in aircraft with rotary wings |
CH260009A (fr) | 1946-05-18 | 1949-02-15 | Sncaso | Propulseur à réaction pour appareil volant. |
US2667226A (en) * | 1946-05-18 | 1954-01-26 | Fairey Aviat Co Ltd | Jet-driven helicopter rotor |
US2894589A (en) * | 1955-08-12 | 1959-07-14 | Westinghouse Electric Corp | Jet propelled helicopter rotor |
US2814349A (en) * | 1956-04-30 | 1957-11-26 | Westinghouse Electric Corp | Aircraft propulsion apparatus |
US3032120A (en) * | 1960-07-11 | 1962-05-01 | United Aircraft Corp | Helicopter with jet driven blades |
US3116040A (en) * | 1961-06-26 | 1963-12-31 | Us Industries Inc | Supersonic rotary wing platform |
US3176413A (en) * | 1963-03-20 | 1965-04-06 | Dornier Werke Gmbh | Flyable helicopter pilot training apparatus |
US3768926A (en) * | 1971-11-30 | 1973-10-30 | R Pegg | Pulse jet rotor drive for helicopter |
US3792827A (en) * | 1972-11-10 | 1974-02-19 | Teledyne Ryan Aeronautical Inc | Vtol aircraft with cruciform rotor wing |
US3930625A (en) * | 1973-09-24 | 1976-01-06 | Alexander Krivka | Steam-powered aircraft |
US4589611A (en) * | 1983-03-01 | 1986-05-20 | Maurice Ramme | Air jet reaction contrarotating rotor gyrodyne |
US4893656A (en) * | 1989-01-30 | 1990-01-16 | Walter Willhoft | Diverter valve |
DE3906109C2 (de) * | 1989-02-27 | 2000-09-07 | Alexander Faller Maschinen U G | Drehflügelflugzeug |
GB9114085D0 (en) | 1991-06-29 | 1997-09-17 | Rolls Royce Plc | Improvements in or relating to helicopters |
US5516060A (en) * | 1993-03-29 | 1996-05-14 | Mcdonnell; William R. | Vertical take off and landing and horizontal flight aircraft |
US5454530A (en) * | 1993-05-28 | 1995-10-03 | Mcdonnell Douglas Helicopter Company | Canard rotor/wing |
US5788181A (en) * | 1995-10-16 | 1998-08-04 | Mcdonnell Douglas Helicopter Co. | Thermostatic metal actuator for nozzle actuation |
US5842665A (en) * | 1996-09-09 | 1998-12-01 | Hmx, Inc. | Launch vehicle with engine mounted on a rotor |
US5765776A (en) * | 1996-10-22 | 1998-06-16 | The United States Of America As Represented By The Secretary Of The Navy | Omnidirectional and controllable wing using fluid ejection |
US5984635A (en) * | 1998-08-24 | 1999-11-16 | Keller; Merrill Manson | Keller pressure jet rotor system |
US6131849A (en) * | 1998-12-02 | 2000-10-17 | Mcdonnell Douglas Helicopter Company | Articulating/telescoping duct for reaction drive helicopters |
GB2360752A (en) | 2000-04-01 | 2001-10-03 | Glyn Jones | Helicopter without tail rotor |
US6709023B2 (en) * | 2002-01-11 | 2004-03-23 | Perkinelmer Inc. | Flexible slide joint |
US20040000614A1 (en) * | 2002-06-27 | 2004-01-01 | Leyva Ivett Alejandra | Method and apparatus for lifting and propelling rotorcraft |
US6789764B2 (en) * | 2002-09-24 | 2004-09-14 | The Boeing Company | Dual-flight mode tandem rotor wing |
US6885917B2 (en) * | 2002-11-07 | 2005-04-26 | The Boeing Company | Enhanced flight control systems and methods for a jet powered tri-mode aircraft |
US7014142B2 (en) * | 2004-02-03 | 2006-03-21 | The Boeing Company | Low-drag rotor/wing flap |
US7275711B1 (en) * | 2004-02-23 | 2007-10-02 | Kenneth Warren Flanigan | Gas-powered tip-jet-driven compound VTOL aircraft |
US7766274B1 (en) * | 2006-03-13 | 2010-08-03 | Lockheed Martin Corporation | Active maple seed flyer |
US7600711B1 (en) * | 2006-05-16 | 2009-10-13 | The Boeing Company | Flexible ducting system including an articulable sealed joint |
US7624942B2 (en) * | 2006-06-20 | 2009-12-01 | United Technologies Corporation | Decoupled ducting for twin-engine reaction rotor drive |
US8011614B2 (en) * | 2007-04-10 | 2011-09-06 | Bird Stanley W | Bird vortex flying machine |
DE202007006976U1 (de) | 2007-05-15 | 2008-09-18 | Jung, Nadine | Hubschrauber |
MC200107A1 (fr) | 2007-07-24 | 2008-02-13 | Jean-Claude Tourn | Dispositif aérien |
EA018176B1 (ru) * | 2007-11-07 | 2013-06-28 | ХЕЛИСКАНДИА АпС | Автономная роторная система для воздушного летательного аппарата |
US8931728B1 (en) * | 2010-09-09 | 2015-01-13 | Groen Brothers Aviation, Inc. | Fail safe, multiple source, tip-jet supply apparatus and method |
US9038940B1 (en) * | 2011-05-16 | 2015-05-26 | Groen Brothers Aviation, Inc. | Rotor configuration for reaction drive rotor system |
US8991748B1 (en) * | 2011-04-19 | 2015-03-31 | Groen Brothers Aviation, Inc. | Solid lubricated blade pitch control system for use within a compressed airstream of a reaction driven rotorcraft |
US9073631B1 (en) * | 2010-09-09 | 2015-07-07 | Groen Brothers Aviation, Inc. | Feathering-spindle-bearing lubrication and temperature control |
CN102556345B (zh) * | 2012-01-18 | 2016-04-13 | 朱晓义 | 飞机动力装置 |
EP2899118B1 (fr) * | 2014-01-27 | 2019-01-16 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Hélicoptère comprenenat un fuselage et au moins un rotor principal |
FR3028838B1 (fr) * | 2014-11-20 | 2016-11-18 | Airbus Helicopters | Aeronef a voilure tournante muni d'un rotor arriere non carene comprenant au moins cinq pales |
US9545903B2 (en) * | 2015-02-02 | 2017-01-17 | Goodrich Corporation | Electromechanical brake actuator with variable speed epicyclic gearbox |
-
2015
- 2015-02-13 MC MC2608A patent/MC200172B1/fr unknown
-
2016
- 2016-02-05 US US15/547,757 patent/US10800520B2/en active Active
- 2016-02-05 WO PCT/EP2016/052561 patent/WO2016128330A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
US20180022450A1 (en) | 2018-01-25 |
WO2016128330A1 (fr) | 2016-08-18 |
US10800520B2 (en) | 2020-10-13 |
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