FR2554082B1 - Commande d'helice anticouple d'helicoptere - Google Patents

Commande d'helice anticouple d'helicoptere

Info

Publication number
FR2554082B1
FR2554082B1 FR8416308A FR8416308A FR2554082B1 FR 2554082 B1 FR2554082 B1 FR 2554082B1 FR 8416308 A FR8416308 A FR 8416308A FR 8416308 A FR8416308 A FR 8416308A FR 2554082 B1 FR2554082 B1 FR 2554082B1
Authority
FR
France
Prior art keywords
torple
propeller
order
helicopter anti
helicopter
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
Application number
FR8416308A
Other languages
English (en)
Other versions
FR2554082A1 (fr
Inventor
Santino Pancotti
Ivan Pergetti
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Agusta SpA
Original Assignee
Costruzioni Aeronautiche Giovanni Augusta SpA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Costruzioni Aeronautiche Giovanni Augusta SpA filed Critical Costruzioni Aeronautiche Giovanni Augusta SpA
Publication of FR2554082A1 publication Critical patent/FR2554082A1/fr
Application granted granted Critical
Publication of FR2554082B1 publication Critical patent/FR2554082B1/fr
Expired legal-status Critical Current

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
    • B64C27/64—Transmitting means, e.g. interrelated with initiating means or means acting on blades using fluid pressure, e.g. having fluid power amplification
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Accessories For Mixers (AREA)
  • Retarders (AREA)
  • Pulleys (AREA)
  • Toys (AREA)
  • Sliding-Contact Bearings (AREA)
FR8416308A 1983-10-26 1984-10-24 Commande d'helice anticouple d'helicoptere Expired FR2554082B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT68108/83A IT1161530B (it) 1983-10-26 1983-10-26 Trasmissione per rotore anticoppia di elicotteri

Publications (2)

Publication Number Publication Date
FR2554082A1 FR2554082A1 (fr) 1985-05-03
FR2554082B1 true FR2554082B1 (fr) 1987-01-23

Family

ID=11307904

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8416308A Expired FR2554082B1 (fr) 1983-10-26 1984-10-24 Commande d'helice anticouple d'helicoptere

Country Status (5)

Country Link
JP (1) JPS60166595A (fr)
DE (1) DE3437582A1 (fr)
FR (1) FR2554082B1 (fr)
GB (1) GB2148818A (fr)
IT (1) IT1161530B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL102698A (en) * 1991-08-02 1996-11-14 Boeing Co Pitch control and fan with ducts for rotor of tail vessel of air vessel with rotary tail
IL102700A (en) * 1991-08-02 1996-10-16 Boeing Co Tail rotor with ducts for air vessels with rotary wing that provides Turk response and Liu reference control
GB2488142B (en) 2011-02-17 2017-11-01 Agustawestland Ltd Tail rotor gearbox lubrication
CN105035315B (zh) * 2015-08-03 2016-11-02 深圳供电局有限公司 一种基于镭射光精确落线巡检的多旋翼无人机及操作方法
CH717147A2 (de) * 2020-02-18 2021-08-31 Marenco Ag Hydraulischer Servo-Aktuator.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB601952A (en) * 1942-12-05 1948-05-14 Andre Aime Lucien Bruel Improvements in aircraft with sustaining airscrews
GB628861A (en) * 1946-04-17 1949-09-06 Firestone Tire & Rubber Co Improvements in or relating to torque counteracting rotors for helicopters
GB615156A (en) * 1946-07-30 1949-01-03 Cierva Autogiro Co Ltd Improvements in and relating to aircraft with rotary-wings
US2581923A (en) * 1947-11-25 1952-01-08 Firestone Tire & Rubber Co Auxiliary rotor for helicopters
GB734888A (en) * 1953-04-30 1955-08-10 Short Brothers & Harland Ltd An improved helicopter rotor hub
GB777076A (en) * 1954-02-19 1957-06-19 United Aircraft Corp Improvements in and relating to helicopter rotors

Also Published As

Publication number Publication date
DE3437582A1 (de) 1985-05-09
GB2148818A (en) 1985-06-05
FR2554082A1 (fr) 1985-05-03
IT1161530B (it) 1987-03-18
JPS60166595A (ja) 1985-08-29
GB8426451D0 (en) 1984-11-28
IT8368108A0 (it) 1983-10-26

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property