IL102698A - Pitch control and fan with ducts for rotor of tail vessel of air vessel with rotary tail - Google Patents
Pitch control and fan with ducts for rotor of tail vessel of air vessel with rotary tailInfo
- Publication number
- IL102698A IL102698A IL10269892A IL10269892A IL102698A IL 102698 A IL102698 A IL 102698A IL 10269892 A IL10269892 A IL 10269892A IL 10269892 A IL10269892 A IL 10269892A IL 102698 A IL102698 A IL 102698A
- Authority
- IL
- Israel
- Prior art keywords
- pitch
- rotor
- axis
- shaft
- supporting
- 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
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
- B64C27/45—Rotors having articulated joints with a feathering hinge only
-
- 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
- B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US73949891A | 1991-08-02 | 1991-08-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
IL102698A0 IL102698A0 (en) | 1993-02-21 |
IL102698A true IL102698A (en) | 1996-11-14 |
Family
ID=24972582
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL10269892A IL102698A (en) | 1991-08-02 | 1992-07-31 | Pitch control and fan with ducts for rotor of tail vessel of air vessel with rotary tail |
Country Status (9)
Country | Link |
---|---|
US (1) | US5478204A (es) |
EP (1) | EP0597038B1 (es) |
JP (1) | JP2768826B2 (es) |
AU (1) | AU2467992A (es) |
CA (1) | CA2113719C (es) |
DE (1) | DE69228246T2 (es) |
ES (1) | ES2126600T3 (es) |
IL (1) | IL102698A (es) |
WO (1) | WO1993002916A1 (es) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2725420B1 (fr) * | 1994-10-11 | 1996-12-13 | Eurocopter France | Dispositif de commande de pas pour rotor sans articulation |
US5607122A (en) * | 1994-12-22 | 1997-03-04 | Bell Helicopter Textron Inc. | Tail rotor authority control for a helicopter |
FR2764578B1 (fr) * | 1997-06-13 | 1999-09-10 | Eurocopter France | Rotor de giravion a moyeu bi-plateau et commande de pas partiellement externe |
FR2775951B1 (fr) * | 1998-03-16 | 2001-09-07 | Rene Mouille | Pale de rotor, notamment pour le rotor arriere anticouple d'un helicoptere |
US7194913B2 (en) | 2002-08-26 | 2007-03-27 | Shell Oil Company | Apparatuses and methods for monitoring stress in steel catenary risers |
BRPI0517922A (pt) | 2004-11-03 | 2008-10-21 | Shell Int Research | sistema para retroativamente equipar um sensor e sistema de comunicação de sensor para monitorar um elemento estrutural instalado, e, método para monitorar mudanças fìsicas em um elemento submarino |
CN101583535B (zh) * | 2006-01-13 | 2013-11-06 | 贝尔直升机泰克斯特龙公司 | 硬共面的、装有万向架的斜旋翼毂 |
US20100019082A1 (en) * | 2008-07-25 | 2010-01-28 | Tsc, Llc | Composite Flight Control Cables |
PL2154065T3 (pl) * | 2008-08-14 | 2011-11-30 | Agustawestland Spa | Śmigło helikoptera |
US8122586B2 (en) * | 2008-11-18 | 2012-02-28 | The Boeing Company | Method for connecting a tension-torsion strap |
WO2010068209A1 (en) * | 2008-12-11 | 2010-06-17 | Sikorsky Aircraft Corporation | Elastomeric bearing system motion limiter |
GB2511668A (en) * | 2012-04-12 | 2014-09-10 | Supercell Oy | System and method for controlling technical processes |
FR2991294B1 (fr) * | 2012-06-04 | 2015-02-13 | Etienne Jean Rampal | Ensemble rotor bi-plateaux d'aeronefs avec logement interne des commandes de pas et adaptateurs de frequence |
US9441495B2 (en) | 2013-02-27 | 2016-09-13 | Sikorsky Aircraft Corporation | Rotary wing aircraft pitch beam attachment with anti-rotation plate design |
RU2538497C1 (ru) * | 2013-12-03 | 2015-01-10 | Открытое акционерное общество "Камов" | Рулевой винт вертолета, установленный в туннеле |
WO2016028762A1 (en) | 2014-08-20 | 2016-02-25 | Sikorsky Aircraft Corporation | Rotor blade pitch horn assembly |
FR3031497B1 (fr) | 2015-01-08 | 2017-01-06 | Airbus Helicopters | Rotor de giravion comportant un moyeu en materiaux composites issus de tissus de fibres de carbone poudrees d'une resine thermoplastique |
US20180002002A1 (en) * | 2016-02-22 | 2018-01-04 | Sikorsky Aircraft Corporation | Rotor assembly including a one piece molding rotor hub |
EP3366584B1 (en) * | 2017-02-27 | 2019-04-17 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Pitch control device for a ducted tail rotor of a rotorcraft |
EP3434590B1 (en) * | 2017-07-27 | 2019-11-27 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A control transfer member for a pitch control device of a ducted rotorcraft tail rotor |
FR3072939B1 (fr) * | 2017-10-31 | 2021-11-26 | Airbus Helicopters | Rotor a pas collectif variable et aeronef |
KR102153511B1 (ko) * | 2019-01-08 | 2020-09-10 | 에어버스 헬리콥터스 도이칠란트 게엠베하 | 덕트된 회전익기 테일 로터의 피치 제어 장치용 제어 이동 부재 |
US11034440B2 (en) * | 2019-03-01 | 2021-06-15 | Textron Innovations Inc. | Tail rotor gearbox support assemblies for helicopters |
US10988243B2 (en) * | 2019-03-15 | 2021-04-27 | Bell Textron Inc. | Tension-torsion strap |
EP3753850B1 (en) * | 2019-06-17 | 2021-08-04 | LEONARDO S.p.A. | Anti-torque rotor for a helicopter |
EP3753848B1 (en) * | 2019-06-17 | 2021-08-04 | LEONARDO S.p.A. | Anti-torque rotor for a helicopter |
CH717386A1 (de) * | 2020-05-06 | 2021-11-15 | Kopter Group Ag | Lösbare Verbindung zwischen einem Blattsteuereinheitsarm und einem Blattverstellhebel. |
CN114537655B (zh) * | 2022-01-28 | 2023-07-28 | 南京航空航天大学 | 旋翼机构 |
CN117419885B (zh) * | 2023-12-19 | 2024-03-19 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种剪刀式尾桨风洞试验台 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2499314A (en) * | 1947-09-12 | 1950-02-28 | United Aircraft Corp | Two-bladed tail rotor on common hinge |
US3450208A (en) * | 1967-04-07 | 1969-06-17 | Barton R E | Dual drive mechanism |
US3518025A (en) * | 1968-05-06 | 1970-06-30 | Lockheed Aircraft Corp | Helicopter rotor system |
FR1593008A (es) * | 1968-07-11 | 1970-05-25 | ||
US3637321A (en) * | 1968-12-04 | 1972-01-25 | Andrei Vladimirovich Nekrasov | Tail rotor of a helicopter |
US3768334A (en) * | 1972-06-26 | 1973-10-30 | Bendix Corp | Load equalized tension torsion tie bar |
US3790302A (en) * | 1972-10-10 | 1974-02-05 | Textron Inc | Tail rotor mounting for coning relief |
FR2397326A2 (fr) * | 1977-07-13 | 1979-02-09 | Aerospatiale | Rotor sans articulations, en particulier pour un giravion |
FR2430354A1 (fr) * | 1978-07-07 | 1980-02-01 | Aerospatiale | Helice multipale a pas variable d'un type simplifie |
FR2534222A1 (fr) * | 1982-10-06 | 1984-04-13 | Aerospatiale | Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement |
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 |
IT1161530B (it) * | 1983-10-26 | 1987-03-18 | Agusta Aeronaut Costr | Trasmissione per rotore anticoppia di elicotteri |
IT1161531B (it) * | 1983-10-26 | 1987-03-18 | Agusta Aeronaut Costr | Assieme di rotore anticoppia per elicotteri |
SE458293B (sv) * | 1987-09-15 | 1989-03-13 | Svenning Konsult Ab S | Regleranordning foer konstanthaallning av varvtalet vid turbiner |
-
1992
- 1992-07-31 JP JP5503786A patent/JP2768826B2/ja not_active Expired - Lifetime
- 1992-07-31 CA CA002113719A patent/CA2113719C/en not_active Expired - Fee Related
- 1992-07-31 AU AU24679/92A patent/AU2467992A/en not_active Abandoned
- 1992-07-31 DE DE69228246T patent/DE69228246T2/de not_active Expired - Fee Related
- 1992-07-31 WO PCT/US1992/006441 patent/WO1993002916A1/en active IP Right Grant
- 1992-07-31 EP EP92918217A patent/EP0597038B1/en not_active Expired - Lifetime
- 1992-07-31 IL IL10269892A patent/IL102698A/en not_active IP Right Cessation
- 1992-07-31 ES ES92918217T patent/ES2126600T3/es not_active Expired - Lifetime
-
1994
- 1994-07-11 US US08/272,448 patent/US5478204A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
IL102698A0 (en) | 1993-02-21 |
AU2467992A (en) | 1993-03-02 |
CA2113719C (en) | 1999-11-02 |
EP0597038A1 (en) | 1994-05-18 |
DE69228246D1 (de) | 1999-03-04 |
ES2126600T3 (es) | 1999-04-01 |
WO1993002916A1 (en) | 1993-02-18 |
CA2113719A1 (en) | 1993-02-18 |
US5478204A (en) | 1995-12-26 |
EP0597038B1 (en) | 1999-01-20 |
JP2768826B2 (ja) | 1998-06-25 |
DE69228246T2 (de) | 1999-08-19 |
JPH06509765A (ja) | 1994-11-02 |
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Legal Events
Date | Code | Title | Description |
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FF | Patent granted | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
EXP | Patent expired |