PL447533A1 - Podwozie samolotu - Google Patents

Podwozie samolotu Download PDF

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Publication number
PL447533A1
PL447533A1 PL447533A PL44753324A PL447533A1 PL 447533 A1 PL447533 A1 PL 447533A1 PL 447533 A PL447533 A PL 447533A PL 44753324 A PL44753324 A PL 44753324A PL 447533 A1 PL447533 A1 PL 447533A1
Authority
PL
Poland
Prior art keywords
attached
leg
landing gear
aircraft landing
actuator
Prior art date
Application number
PL447533A
Other languages
English (en)
Other versions
PL246784B1 (pl
Inventor
Łukasz Puzio
Jarosław Pytka
Adrian Nafalski
Original Assignee
Politechnika Lubelska
Państwowa Akademia Nauk Stosowanych W Chełmie
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 Politechnika Lubelska, Państwowa Akademia Nauk Stosowanych W Chełmie filed Critical Politechnika Lubelska
Priority to PL447533A priority Critical patent/PL246784B1/pl
Publication of PL447533A1 publication Critical patent/PL447533A1/pl
Publication of PL246784B1 publication Critical patent/PL246784B1/pl

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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 
    • B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • B64C25/36—Arrangements or adaptations of wheels, tyres or axles in general
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Body Structure For Vehicles (AREA)
  • Toys (AREA)

Abstract

Podwozie samolotu, w którym oś koła (1) jezdnego zamocowana jest poprzez goleń (2) do kadłuba (3), charakteryzuje się tym, że do goleni (2) zamocowany jest pierwszym końcem za pomocą zawiasu (4) wahacz (5), do którego drugiego końca zamocowany jest za pomocą tulei wał (6) koła wspomagającego (7), połączonego z silnikiem elektrycznym. Wał (6) zamocowany jest obrotowo do goleni (2). Pomiędzy golenią (2) a drugim końcem wahacza (5) zamocowany jest siłownik (9). Z kołem wspomagającym (7) sprzężony jest czujnik jego prędkości obrotowej (10), który połączony jest elektrycznie z modułem sterującym, połączonym linią sterującą do zasilania silnika elektrycznego oraz do siłownika (9).
PL447533A 2024-01-17 2024-01-17 Podwozie samolotu PL246784B1 (pl)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL447533A PL246784B1 (pl) 2024-01-17 2024-01-17 Podwozie samolotu

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL447533A PL246784B1 (pl) 2024-01-17 2024-01-17 Podwozie samolotu

Publications (2)

Publication Number Publication Date
PL447533A1 true PL447533A1 (pl) 2024-08-12
PL246784B1 PL246784B1 (pl) 2025-03-10

Family

ID=92264352

Family Applications (1)

Application Number Title Priority Date Filing Date
PL447533A PL246784B1 (pl) 2024-01-17 2024-01-17 Podwozie samolotu

Country Status (1)

Country Link
PL (1) PL246784B1 (pl)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6698689B1 (en) * 1999-12-08 2004-03-02 Aerospatiale Matra Airbus Auxiliary nose landing gear for aircraft
US20130140399A1 (en) * 2010-06-16 2013-06-06 Messier-Bugatti-Dowty Main landing gear of an aircraft, comprising two walking beams and a deformable parallelogram structure
US20150266592A1 (en) * 2011-02-21 2015-09-24 The Boeing Company Air-ground detection system for semi-levered landing gear
US20210253228A1 (en) * 2020-02-18 2021-08-19 Airbus Operations Limited Modular landing gear

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6698689B1 (en) * 1999-12-08 2004-03-02 Aerospatiale Matra Airbus Auxiliary nose landing gear for aircraft
US20130140399A1 (en) * 2010-06-16 2013-06-06 Messier-Bugatti-Dowty Main landing gear of an aircraft, comprising two walking beams and a deformable parallelogram structure
US20150266592A1 (en) * 2011-02-21 2015-09-24 The Boeing Company Air-ground detection system for semi-levered landing gear
US20210253228A1 (en) * 2020-02-18 2021-08-19 Airbus Operations Limited Modular landing gear

Also Published As

Publication number Publication date
PL246784B1 (pl) 2025-03-10

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