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ES2183672A1 - System for adjusting the speed of aircraft landing wheels - Google Patents

System for adjusting the speed of aircraft landing wheels

Info

Publication number
ES2183672A1
ES2183672A1 ES200000218A ES200000218A ES2183672A1 ES 2183672 A1 ES2183672 A1 ES 2183672A1 ES 200000218 A ES200000218 A ES 200000218A ES 200000218 A ES200000218 A ES 200000218A ES 2183672 A1 ES2183672 A1 ES 2183672A1
Authority
ES
Spain
Prior art keywords
wheels
speed
aircraft
wheel
landing
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
ES200000218A
Other languages
Spanish (es)
Other versions
ES2183672B1 (en
Inventor
Carrete Mireia Piera
Piera Jose Maria Martinez-Val
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.)
3 14 Era S L
Original Assignee
3 14 Era S L
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 3 14 Era S L filed Critical 3 14 Era S L
Priority to ES200000218A priority Critical patent/ES2183672B1/en
Publication of ES2183672A1 publication Critical patent/ES2183672A1/en
Application granted granted Critical
Publication of ES2183672B1 publication Critical patent/ES2183672B1/en
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
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface  the elements being rotated before touch-down

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

System for adjusting the speed of aircraft landing wheels, characterised in that the wheels acquire a relevant rotation speed before contact is made with the landing strip, thus obtaining a better touch-down of the aircraft and a substantial and great reduction of the friction of the first contact, which normally provokes significant deterioration in the reversal band of the wheels with a risk of excessive local wear and tear the appropriate rate of wheel rotation is obtained before the first landing contact thanks to a very aerodynamic device, either electro-mechanical, or mixed, that accelerates the wheels, from its initial standby mode, to a speed close to that which the wheel would have if it were rotating exactly at the same linear speed of the aircraft, said device is implemented next to the rim of each wheel.
ES200000218A 2000-02-02 2000-02-02 SYSTEM OF ADEQUACY OF THE SPEED OF THE AIRCRAFT LANDING WHEELS. Expired - Fee Related ES2183672B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES200000218A ES2183672B1 (en) 2000-02-02 2000-02-02 SYSTEM OF ADEQUACY OF THE SPEED OF THE AIRCRAFT LANDING WHEELS.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200000218A ES2183672B1 (en) 2000-02-02 2000-02-02 SYSTEM OF ADEQUACY OF THE SPEED OF THE AIRCRAFT LANDING WHEELS.

Publications (2)

Publication Number Publication Date
ES2183672A1 true ES2183672A1 (en) 2003-03-16
ES2183672B1 ES2183672B1 (en) 2004-06-16

Family

ID=8492138

Family Applications (1)

Application Number Title Priority Date Filing Date
ES200000218A Expired - Fee Related ES2183672B1 (en) 2000-02-02 2000-02-02 SYSTEM OF ADEQUACY OF THE SPEED OF THE AIRCRAFT LANDING WHEELS.

Country Status (1)

Country Link
ES (1) ES2183672B1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004014727A1 (en) * 2002-08-05 2004-02-19 Martin Huete Jane Rim for aircraft landing gear wheels
US8684300B2 (en) 2009-08-28 2014-04-01 Airbus Operations Limited Aircraft landing gear
ES2529512A1 (en) * 2013-08-20 2015-02-20 Joaquín ALONSO CERQUEIRA Aerodynamic turning accelerator set for aircraft wheels (Machine-translation by Google Translate, not legally binding)
ES2916749A1 (en) * 2021-01-04 2022-07-05 Sisini Cristian Miguel Alonso Covers and automatic turn tires for aircraft (Machine-translation by Google Translate, not legally binding)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430163A (en) * 1944-09-25 1947-11-04 Otto E Dever Motor wheel
US2505770A (en) * 1945-12-07 1950-05-02 Herbert G Hill Drive for airplane wheels
ES359142A1 (en) * 1968-10-14 1970-05-16 Somme Procedure to avoid the efforts produced by the reaction of the inertia of the wheels of the aircraft. (Machine-translation by Google Translate, not legally binding)
US3814354A (en) * 1973-05-14 1974-06-04 Oldrich Drake Landing wheel rotating device for aircraft
WO1992015483A1 (en) * 1991-03-05 1992-09-17 Julian Pasqua Aircraft wheel prerotation apparatus
ES1032378U (en) * 1995-10-30 1996-04-16 Pascual Laureano Medina Device promoter wheelspin landing gear for aircraft. (Machine-translation by Google Translate, not legally binding)

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430163A (en) * 1944-09-25 1947-11-04 Otto E Dever Motor wheel
US2505770A (en) * 1945-12-07 1950-05-02 Herbert G Hill Drive for airplane wheels
ES359142A1 (en) * 1968-10-14 1970-05-16 Somme Procedure to avoid the efforts produced by the reaction of the inertia of the wheels of the aircraft. (Machine-translation by Google Translate, not legally binding)
US3814354A (en) * 1973-05-14 1974-06-04 Oldrich Drake Landing wheel rotating device for aircraft
WO1992015483A1 (en) * 1991-03-05 1992-09-17 Julian Pasqua Aircraft wheel prerotation apparatus
ES1032378U (en) * 1995-10-30 1996-04-16 Pascual Laureano Medina Device promoter wheelspin landing gear for aircraft. (Machine-translation by Google Translate, not legally binding)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004014727A1 (en) * 2002-08-05 2004-02-19 Martin Huete Jane Rim for aircraft landing gear wheels
ES2246607A1 (en) * 2002-08-05 2006-02-16 Martin Huete Jane Rim for aircraft landing gear wheels
ES2246607B1 (en) * 2002-08-05 2007-04-01 Martin Huete Jane RIM FOR WHEELS OF AIRCRAFT LANDING TRAINS.
US8684300B2 (en) 2009-08-28 2014-04-01 Airbus Operations Limited Aircraft landing gear
US9428266B2 (en) 2009-08-28 2016-08-30 Airbus Operations Limited Aircraft landing gear
US10562615B2 (en) 2009-08-28 2020-02-18 Airbus Operations Limited Aircraft landing gear
US11628931B2 (en) 2009-08-28 2023-04-18 Airbus Operations Limited Aircraft landing gear with pivoting drive transmission
ES2529512A1 (en) * 2013-08-20 2015-02-20 Joaquín ALONSO CERQUEIRA Aerodynamic turning accelerator set for aircraft wheels (Machine-translation by Google Translate, not legally binding)
ES2916749A1 (en) * 2021-01-04 2022-07-05 Sisini Cristian Miguel Alonso Covers and automatic turn tires for aircraft (Machine-translation by Google Translate, not legally binding)

Also Published As

Publication number Publication date
ES2183672B1 (en) 2004-06-16

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