IT1164936B - Albero rotore a comandi interni per elicotteri - Google Patents
Albero rotore a comandi interni per elicotteriInfo
- Publication number
- IT1164936B IT1164936B IT67431/79A IT6743179A IT1164936B IT 1164936 B IT1164936 B IT 1164936B IT 67431/79 A IT67431/79 A IT 67431/79A IT 6743179 A IT6743179 A IT 6743179A IT 1164936 B IT1164936 B IT 1164936B
- Authority
- IT
- Italy
- Prior art keywords
- helicopters
- rotor shaft
- internal control
- control rotor
- internal
- 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
- B64C27/72—Means acting on blades
-
- 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
- B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Transmission Devices (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67431/79A IT1164936B (it) | 1979-02-27 | 1979-02-27 | Albero rotore a comandi interni per elicotteri |
DE3002470A DE3002470C2 (de) | 1979-02-27 | 1980-01-24 | Rotorwelle für Hubschrauber |
US06/114,963 US4375940A (en) | 1979-02-27 | 1980-01-24 | Rotor shaft with internal controls for helicopters |
GB8002620A GB2043010B (en) | 1979-02-27 | 1980-01-25 | Helicopter rotor shaft with internal pitch control linkages |
JP1981280A JPS55114697A (en) | 1979-02-27 | 1980-02-21 | Rotor shaft for helicopter |
FR8003994A FR2450201A1 (fr) | 1979-02-27 | 1980-02-22 | Arbre de rotor avec commandes internes pour helicopteres |
JP1989092595U JPH0316800Y2 (it) | 1979-02-27 | 1989-08-08 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67431/79A IT1164936B (it) | 1979-02-27 | 1979-02-27 | Albero rotore a comandi interni per elicotteri |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7967431A0 IT7967431A0 (it) | 1979-02-27 |
IT1164936B true IT1164936B (it) | 1987-04-15 |
Family
ID=11302333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT67431/79A IT1164936B (it) | 1979-02-27 | 1979-02-27 | Albero rotore a comandi interni per elicotteri |
Country Status (6)
Country | Link |
---|---|
US (1) | US4375940A (it) |
JP (2) | JPS55114697A (it) |
DE (1) | DE3002470C2 (it) |
FR (1) | FR2450201A1 (it) |
GB (1) | GB2043010B (it) |
IT (1) | IT1164936B (it) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0075407B1 (en) * | 1981-09-18 | 1986-05-07 | WESTLAND plc | Helicopter rotor |
FR2542695B1 (fr) * | 1983-03-18 | 1985-07-26 | Aerospatiale | Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees |
IT1161529B (it) * | 1983-10-26 | 1987-03-18 | Agusta Aeronaut Costr | Assieme di rotore anticoppia per elicotteri |
FR2564057B1 (fr) * | 1984-05-14 | 1986-10-31 | Aerospatiale | Dispositif a plateaux cycliques montes sur articulations lamifiees pour la commande du pas des pales d'un rotor |
US4688993A (en) * | 1985-03-21 | 1987-08-25 | United Technologies Corporation | Tangential link swashplate centering member |
FR2584997B1 (fr) * | 1985-07-22 | 1987-11-13 | Aerospatiale | Dispositif de butees de battement pour rotor de giravion |
FR2584996B1 (fr) * | 1985-07-22 | 1987-11-13 | Aerospatiale | Mat-moyeu integre et tete de rotor de giravion le comportant |
FR2584995B1 (fr) * | 1985-07-22 | 1987-11-13 | Aerospatiale | Mat-moyeu integre et tete de rotor de giravion le comportant |
US4778340A (en) * | 1985-11-25 | 1988-10-18 | Costruzioni Aeronautiche Giovanni Augusta S.P.A. | Main helicopter rotor |
FR2768996B1 (fr) * | 1997-09-30 | 1999-12-03 | Eurocopter France | Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec entraineur de plateau tournant |
FR2770827B1 (fr) * | 1997-11-13 | 2000-01-14 | Eurocopter France | Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule par clavettes sur une rotule centrale |
FR2770828B1 (fr) * | 1997-11-13 | 2000-01-14 | Eurocopter France | Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule sur une rotule centrale |
FR2771707B1 (fr) * | 1997-11-28 | 2000-02-04 | Eurocopter France | Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec patins cylindriques glissant sur colonnes non-tournantes |
FR2771708B1 (fr) * | 1997-12-03 | 2000-02-04 | Eurocopter France | Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec organes guides rotatifs sur coulisseaux translates selon l'axe du rotor |
IT1308395B1 (it) | 1999-02-26 | 2001-12-17 | Finmeccanica Spa | Dispositivo di controllo dei passi ciclico e collettivo per un rotoredi un elicottero. |
DE19910449A1 (de) | 1999-03-10 | 2000-09-14 | Zf Luftfahrttechnik Gmbh | Hubschrauber |
DE19910448C1 (de) * | 1999-03-10 | 2000-05-18 | Zf Luftfahrttechnik Gmbh | Hubschrauber |
US7828482B2 (en) * | 2006-08-28 | 2010-11-09 | Roller Bearing Company Of America, Inc. | Tungsten carbide enhanced bearing |
US7674091B2 (en) * | 2006-11-14 | 2010-03-09 | The Boeing Company | Rotor blade pitch control |
FR2951699B1 (fr) * | 2009-10-23 | 2011-11-11 | Eurocopter France | Ensemble de plateaux cycliques de commande de pas de pales d'un rotor principal, et un rotor muni d'un tel ensemble |
US8961138B2 (en) | 2011-12-09 | 2015-02-24 | Bell Helicopter Textron Inc. | Preventing rotation of a fixed ring of a swashplate |
US9039373B2 (en) * | 2011-12-14 | 2015-05-26 | Textron Innovations Inc. | Blade-pitch control system with feedback lever |
US9151162B2 (en) * | 2012-11-08 | 2015-10-06 | Bell Helicopter Textron Inc. | Preventing rotation of a fixed ring of a swashplate |
EP3201077B1 (en) | 2014-10-01 | 2020-05-20 | Sikorsky Aircraft Corporation | Dual rotor, rotary wing aircraft |
WO2016053408A1 (en) | 2014-10-01 | 2016-04-07 | Sikorsky Aircraft Corporation | Acoustic signature variation of aircraft utilizing a clutch |
CN210027884U (zh) * | 2018-11-06 | 2020-02-07 | 珠海隆华直升机科技有限公司 | 直升机变距联动系统及直升机 |
US11472534B2 (en) | 2019-06-28 | 2022-10-18 | The Boeing Company | Rotor hubs having pitch control systems and related methods |
WO2021034973A1 (en) | 2019-08-20 | 2021-02-25 | Kinetic Analytics Llc | Individual blade control system for rotorcraft |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE21041C (de) * | M. FLÜRSCHEIM, Eisenwerk Gaggenau in Gaggenau | Lampe zum Anzünden vonCigarren | ||
DE610434C (de) * | 1932-03-02 | 1935-03-12 | Otto Reder Dipl Ing | Quer- und Hoehensteuerung fuer Flugzeuge mit kreisenden Tragflaechen |
FR795623A (fr) * | 1934-07-27 | 1936-03-18 | Kay Gyroplanes Ltd | Perfectionnements relatifs aux aéroplanes |
GB531608A (en) * | 1938-01-18 | 1941-01-08 | Brandenburgische Motorenwerke | Improvements in or relating to aircraft with rotating wing systems |
US2444070A (en) * | 1942-05-14 | 1948-06-29 | Autogiro Co Of America | Aircraft rotor providing for tilting of axis and blade pitch regulation |
GB634529A (en) * | 1942-08-07 | 1950-03-22 | Autogiro Co Of America | Pitch control for aircraft sustaining rotors |
US2439089A (en) * | 1944-05-22 | 1948-04-06 | Fairey Aviat Co Ltd | Control of rotating wing aircraft |
US2474362A (en) * | 1944-09-14 | 1949-06-28 | Theodore S Keranen | Helicopter |
GB605561A (en) * | 1945-03-24 | 1948-07-27 | John Sidney Neale | Improved pitch controlling means for rotor blades of helicopters |
US2573016A (en) * | 1945-12-10 | 1951-10-30 | Harold D Harby | Helicopter rotor control |
FR941626A (fr) * | 1946-04-23 | 1949-01-17 | Hélicoptère à réaction | |
US2932353A (en) * | 1956-10-08 | 1960-04-12 | Victor O Armstrong | Simplified controls for a ram jet helicopter |
US2984306A (en) * | 1958-05-08 | 1961-05-16 | United Aircraft Corp | Helicopter rotor head and its controls |
US3002569A (en) * | 1959-05-28 | 1961-10-03 | Mcdonnell Aircraft Corp | Locking device for floating hub helicopter rotors |
US3095931A (en) * | 1961-05-10 | 1963-07-02 | Kaman Aircraft Corp | Blade pitch control mechanism for a helicopter |
US3080002A (en) * | 1961-06-29 | 1963-03-05 | Doman Helicopters Inc | Rotor with fixed pylon |
CH443007A (de) * | 1964-02-29 | 1967-08-31 | Berger Hans | Vorrichtung zur Rotorblattverstellung bei Helikoptern |
US3207226A (en) * | 1964-09-10 | 1965-09-21 | Frank W Caldwell | Rotor driving mechanism |
FR1542617A (fr) * | 1967-07-31 | 1968-10-18 | Sud Aviation | Perfectionnements apportés aux rotors pour aérodynes à voilure tournante |
US3521971A (en) * | 1968-07-17 | 1970-07-28 | United Aircraft Corp | Method and apparatus for controlling aircraft |
US3637322A (en) * | 1969-02-26 | 1972-01-25 | Dornier Ag | Rotor head for a helicopter |
GB1258505A (it) * | 1969-03-25 | 1971-12-30 | ||
US3759629A (en) * | 1969-05-12 | 1973-09-18 | J Abramopaulos | Combined land and air vehicle |
US3572616A (en) * | 1969-09-18 | 1971-03-30 | United Aircraft Corp | Pitch control mechanism for bladed rotor |
US3756743A (en) * | 1970-04-15 | 1973-09-04 | F Robertson | Rotors for rotary winged aircraft |
US3738772A (en) * | 1972-03-07 | 1973-06-12 | Siai Marchetti Spa | Oscillating plate for helicopters |
DE2459543C3 (de) * | 1974-12-17 | 1979-05-17 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Längenverstellbare Steuerstange zur Veränderung des Blatteinstellwinkels eines Drehflügelflugzeuges |
GB1529870A (en) * | 1975-10-13 | 1978-10-25 | Westland Aircraft Ltd | Helicopter rotors |
DE2658828C3 (de) * | 1976-12-24 | 1982-02-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor für ein Drehflügelflugzeug |
-
1979
- 1979-02-27 IT IT67431/79A patent/IT1164936B/it active
-
1980
- 1980-01-24 DE DE3002470A patent/DE3002470C2/de not_active Expired - Lifetime
- 1980-01-24 US US06/114,963 patent/US4375940A/en not_active Expired - Lifetime
- 1980-01-25 GB GB8002620A patent/GB2043010B/en not_active Expired
- 1980-02-21 JP JP1981280A patent/JPS55114697A/ja active Pending
- 1980-02-22 FR FR8003994A patent/FR2450201A1/fr active Granted
-
1989
- 1989-08-08 JP JP1989092595U patent/JPH0316800Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPH0316800Y2 (it) | 1991-04-10 |
DE3002470A1 (de) | 1980-09-04 |
FR2450201B1 (it) | 1983-05-13 |
GB2043010B (en) | 1983-04-13 |
IT7967431A0 (it) | 1979-02-27 |
FR2450201A1 (fr) | 1980-09-26 |
JPS55114697A (en) | 1980-09-04 |
GB2043010A (en) | 1980-10-01 |
US4375940A (en) | 1983-03-08 |
DE3002470C2 (de) | 1994-04-28 |
JPH0227000U (it) | 1990-02-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19970227 |