ES2159997A1 - Mandos de vuelo con compensacion automatica. - Google Patents

Mandos de vuelo con compensacion automatica.

Info

Publication number
ES2159997A1
ES2159997A1 ES009800049A ES9800049A ES2159997A1 ES 2159997 A1 ES2159997 A1 ES 2159997A1 ES 009800049 A ES009800049 A ES 009800049A ES 9800049 A ES9800049 A ES 9800049A ES 2159997 A1 ES2159997 A1 ES 2159997A1
Authority
ES
Spain
Prior art keywords
aileron
flight controls
automatic balance
rotates
main part
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.)
Granted
Application number
ES009800049A
Other languages
English (en)
Other versions
ES2159997B1 (es
Inventor
Saiz Manuel Munoz
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to ES9800049A priority Critical patent/ES2159997B1/es
Priority to US09/139,524 priority patent/US6220551B1/en
Priority to EP98500281A priority patent/EP0937642A3/en
Publication of ES2159997A1 publication Critical patent/ES2159997A1/es
Application granted granted Critical
Publication of ES2159997B1 publication Critical patent/ES2159997B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/30—Balancing hinged surfaces, e.g. dynamically
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

Mandos de vuelo con compensación automática que consiste en alerones divididos en dos partes, los cuales a baja velocidad adoptan una forma de alerón convencional y giran en su totalidad con el mismo ángulo y a altas velocidades una porción gira o se extiende a un ángulo determinado movido por el actuador y el resto del alerón, que esta abisagrado o articulado a la porción principal del alerón, gira respecto a la porción principal en función de la presión del aire, oponiéndose a este giro por medio de unos muelles.
ES9800049A 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica. Expired - Fee Related ES2159997B1 (es)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES9800049A ES2159997B1 (es) 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica.
US09/139,524 US6220551B1 (en) 1998-01-14 1998-08-25 Flight controls with automatic balance
EP98500281A EP0937642A3 (en) 1998-01-14 1998-12-28 Flight controls with automatic balance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES9800049A ES2159997B1 (es) 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica.

Publications (2)

Publication Number Publication Date
ES2159997A1 true ES2159997A1 (es) 2001-10-16
ES2159997B1 ES2159997B1 (es) 2002-05-01

Family

ID=8302374

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9800049A Expired - Fee Related ES2159997B1 (es) 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica.

Country Status (2)

Country Link
EP (1) EP0937642A3 (es)
ES (1) ES2159997B1 (es)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPP646098A0 (en) * 1998-10-13 1998-11-05 Ladd, Paul Vincent Mr Directional control and aerofoil system for aircraft
CN107512384B (zh) * 2017-08-01 2020-04-21 中国航空工业集团公司西安飞机设计研究所 一种升降舵
EP3584153A1 (en) 2018-06-20 2019-12-25 Bombardier Inc. Variable camber system
EP3584156A1 (en) * 2018-06-20 2019-12-25 Bombardier Inc. Variable camber system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB267503A (es) * 1926-03-12 1928-02-09 Nieuport-Astra
GB360273A (es) * 1930-01-21 1931-11-05 Jacques Gerin
US5335886A (en) * 1992-01-30 1994-08-09 The United States Of America As Represented By The Seceretary Of The Navy Lift enhancement device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB267503A (es) * 1926-03-12 1928-02-09 Nieuport-Astra
GB360273A (es) * 1930-01-21 1931-11-05 Jacques Gerin
US5335886A (en) * 1992-01-30 1994-08-09 The United States Of America As Represented By The Seceretary Of The Navy Lift enhancement device

Also Published As

Publication number Publication date
EP0937642A3 (en) 2000-05-10
EP0937642A2 (en) 1999-08-25
ES2159997B1 (es) 2002-05-01

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