FR1484732A - Hélicoptère avec un système à rotor disposé à l'arrière et servant à la propulsion, à la commande de direction et à la compensation anticouple - Google Patents
Hélicoptère avec un système à rotor disposé à l'arrière et servant à la propulsion, à la commande de direction et à la compensation anticoupleInfo
- Publication number
- FR1484732A FR1484732A FR67008584A FR67008584A FR1484732A FR 1484732 A FR1484732 A FR 1484732A FR 67008584 A FR67008584 A FR 67008584A FR 67008584 A FR67008584 A FR 67008584A FR 1484732 A FR1484732 A FR 1484732A
- Authority
- FR
- France
- Prior art keywords
- helicopter
- propulsion
- steering control
- system arranged
- rotor system
- 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
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
- B64C27/82—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
- B64C2027/8236—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 including pusher propellers
-
- 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
- B64C2027/8263—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 comprising in addition rudders, tails, fins, or the like
- B64C2027/8272—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 comprising in addition rudders, tails, fins, or the like comprising fins, or movable rudders
-
- 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
- B64C2027/8263—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 comprising in addition rudders, tails, fins, or the like
- B64C2027/8281—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 comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED47084A DE1272729B (de) | 1965-04-22 | 1965-04-22 | Kombinationsflugschrauber mit einem am Heck angeordneten Rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1484732A true FR1484732A (fr) | 1967-06-16 |
Family
ID=7050180
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR67008584A Expired FR1484732A (fr) | 1965-04-22 | 1966-04-22 | Hélicoptère avec un système à rotor disposé à l'arrière et servant à la propulsion, à la commande de direction et à la compensation anticouple |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1272729B (fr) |
FR (1) | FR1484732A (fr) |
GB (1) | GB1118117A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2407377A1 (fr) * | 2010-07-13 | 2012-01-18 | Eurocopter | Procède et aèronef muni d`un rotor arrière basculant |
FR3014838A1 (fr) * | 2013-12-17 | 2015-06-19 | Eurocopter France | Giravion equipe d'un rotor arriere anti couple participant selectivement a la sustentation et a la propulsion en translation du giravion |
FR3014837A1 (fr) * | 2013-12-17 | 2015-06-19 | Eurocopter France | Giravion equipe d'un rotor arriere anticouple participant a la sustentation du giravion par variation cyclique du pas des pales dudit rotor arriere |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2197276B (en) * | 1986-09-26 | 1990-04-04 | Airship Ind | Improvements in airships |
GB8927784D0 (en) * | 1989-12-08 | 1990-05-30 | Westland Helicopters | Helicopters |
DE202009001355U1 (de) | 2009-02-04 | 2009-05-20 | RÖHR, Ulrich | Modellflugkörpersteuer- und Empfangseinrichtung |
DE102012003910A1 (de) | 2011-04-15 | 2012-10-18 | Ulrich Röhr | System zur drahtlosen Steuerung eines RC-Modells, Sendeeinrichtung, Empfangseinrichtung sowie Verfahren |
WO2016126304A1 (fr) * | 2015-02-04 | 2016-08-11 | Sikorsky Aircraft Corporation | Commande de direction améliorée pour engin à voilure rotative coaxiale |
WO2016200458A2 (fr) * | 2015-05-20 | 2016-12-15 | Sikorsky Aircraft Corporation | Plateau cyclique à commande monocyclique |
CN112089533A (zh) * | 2020-10-13 | 2020-12-18 | 航宇救生装备有限公司 | 直升机吊装防旋担架 |
CN113086165B (zh) * | 2021-04-20 | 2022-11-04 | 中国直升机设计研究所 | 一种主旋翼与尾桨间距可变的直升机 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2479549A (en) * | 1943-11-10 | 1949-08-23 | Sperry Corp | Automatic pilot for helicopters |
DE1144116B (de) * | 1959-11-06 | 1963-02-21 | Boelkow Entwicklungen Kg | Drehfluegelflugzeug mit einem Heckrotor und einem Seitenleitwerk |
DE1136580B (de) * | 1960-10-01 | 1962-09-13 | Boelkow Entwicklungen Kg | Drehfluegelflugzeug |
US3138349A (en) * | 1962-01-15 | 1964-06-23 | Piasecki Aircraft Corp | Rotary wing aircraft tail assembly and controls |
-
1965
- 1965-04-22 GB GB1770666A patent/GB1118117A/en not_active Expired
- 1965-04-22 DE DED47084A patent/DE1272729B/de active Pending
-
1966
- 1966-04-22 FR FR67008584A patent/FR1484732A/fr not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2407377A1 (fr) * | 2010-07-13 | 2012-01-18 | Eurocopter | Procède et aèronef muni d`un rotor arrière basculant |
FR2962713A1 (fr) * | 2010-07-13 | 2012-01-20 | Eurocopter France | Procede et aeronef muni d'un rotor arriere basculant |
US8777152B2 (en) | 2010-07-13 | 2014-07-15 | Airbus Helicopters | Method and an aircraft provided with a swiveling tail rotor |
FR3014838A1 (fr) * | 2013-12-17 | 2015-06-19 | Eurocopter France | Giravion equipe d'un rotor arriere anti couple participant selectivement a la sustentation et a la propulsion en translation du giravion |
FR3014837A1 (fr) * | 2013-12-17 | 2015-06-19 | Eurocopter France | Giravion equipe d'un rotor arriere anticouple participant a la sustentation du giravion par variation cyclique du pas des pales dudit rotor arriere |
EP2886459A1 (fr) | 2013-12-17 | 2015-06-24 | Airbus Helicopters | Giravion équipé d'un rotor arrière anti-couple participant sélectivement à la sustentation et à la propulsion en translation du giravion |
JP2015117018A (ja) * | 2013-12-17 | 2015-06-25 | エアバス ヘリコプターズ | 回転翼航空機への揚力及び並進推進力の提供に選択的に寄与する反トルク尾部ロータが装着された回転翼航空機 |
US9365289B2 (en) | 2013-12-17 | 2016-06-14 | Airbus Helicopters | Rotorcraft fitted with an anti-torque tail rotor that contributes selectively to providing the rotorcraft with lift and with propulsion in translation |
Also Published As
Publication number | Publication date |
---|---|
DE1272729B (de) | 1968-07-11 |
GB1118117A (en) | 1968-06-26 |
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