IT967164B - Supporto raddoppiato per stabiliz zatore orizzontale di aeromobile - Google Patents

Supporto raddoppiato per stabiliz zatore orizzontale di aeromobile

Info

Publication number
IT967164B
IT967164B IT28838/72A IT2883872A IT967164B IT 967164 B IT967164 B IT 967164B IT 28838/72 A IT28838/72 A IT 28838/72A IT 2883872 A IT2883872 A IT 2883872A IT 967164 B IT967164 B IT 967164B
Authority
IT
Italy
Prior art keywords
horizontal stabilizer
double support
aircraft horizontal
aircraft
double
Prior art date
Application number
IT28838/72A
Other languages
English (en)
Italian (it)
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of IT967164B publication Critical patent/IT967164B/it

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
    • B64C2027/8263—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)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Earth Drilling (AREA)
IT28838/72A 1971-09-14 1972-09-06 Supporto raddoppiato per stabiliz zatore orizzontale di aeromobile IT967164B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US18029571A 1971-09-14 1971-09-14

Publications (1)

Publication Number Publication Date
IT967164B true IT967164B (it) 1974-02-28

Family

ID=22659927

Family Applications (1)

Application Number Title Priority Date Filing Date
IT28838/72A IT967164B (it) 1971-09-14 1972-09-06 Supporto raddoppiato per stabiliz zatore orizzontale di aeromobile

Country Status (6)

Country Link
US (1) US3706432A (OSRAM)
JP (1) JPS4862199A (OSRAM)
DE (1) DE2231010A1 (OSRAM)
FR (1) FR2152534A1 (OSRAM)
GB (1) GB1332620A (OSRAM)
IT (1) IT967164B (OSRAM)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4247061A (en) * 1978-07-12 1981-01-27 United Technologies Corporation Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency
DE3500454A1 (de) * 1985-01-09 1986-07-10 Valerij Vladimirovič Moskau/Moskva Archipov Ladetreppe
ES2279716B1 (es) * 2005-12-26 2008-08-16 Airbus España, S.L. Herraje de giro para un empenaje de una aeronave.
ES2345584B1 (es) * 2007-12-21 2011-07-18 Airbus Operations, S.L. Superficie de control de aeronave.
EP2878536B1 (en) 2013-11-29 2017-05-24 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Advanced pitch stabilizer
US20170106970A1 (en) * 2015-10-15 2017-04-20 The Boeing Company Composite failsafe torque tube
CN107745809B (zh) * 2017-10-14 2020-04-21 上海歌尔泰克机器人有限公司 飞行器
US12151811B2 (en) * 2019-08-13 2024-11-26 Textron Innovations Inc. Tilting wing rotorcrafts and wing rotation systems
US11685515B2 (en) * 2019-10-11 2023-06-27 Textron Innovations Inc. Active horizontal stabilizer for high speed rotorcraft
CN110697024B (zh) * 2019-10-14 2022-07-15 中国航空工业集团公司西安飞机设计研究所 一种飞机尾翼结构

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437330A (en) * 1944-01-24 1948-03-09 Alexander S Mullgardt Variable incidence wing control for aircraft of the rotaly wing or airplane sustained type
US2959373A (en) * 1954-12-10 1960-11-08 Daniel R Zuck Convertiplane

Also Published As

Publication number Publication date
JPS4862199A (OSRAM) 1973-08-30
GB1332620A (en) 1973-10-03
DE2231010A1 (de) 1973-03-22
FR2152534A1 (OSRAM) 1973-04-27
US3706432A (en) 1972-12-19

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