PL437565A1 - Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed - Google Patents

Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed

Info

Publication number
PL437565A1
PL437565A1 PL437565A PL43756521A PL437565A1 PL 437565 A1 PL437565 A1 PL 437565A1 PL 437565 A PL437565 A PL 437565A PL 43756521 A PL43756521 A PL 43756521A PL 437565 A1 PL437565 A1 PL 437565A1
Authority
PL
Poland
Prior art keywords
ring
disc
rotational speed
gear wheel
touchdown
Prior art date
Application number
PL437565A
Other languages
Polish (pl)
Inventor
Andrzej Jerzy Szymysł
Krystian Jakub Szymysł
Original Assignee
Andrzej Jerzy Szymysł
Krystian Jakub Szymysł
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 Andrzej Jerzy Szymysł, Krystian Jakub Szymysł filed Critical Andrzej Jerzy Szymysł
Priority to PL437565A priority Critical patent/PL437565A1/en
Publication of PL437565A1 publication Critical patent/PL437565A1/en

Links

Landscapes

  • Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)

Abstract

Sposób bezpośredniego napędzania kół podwozia samolotu podczas lądowania do prędkości obrotowej odpowiadającej prędkości przyziemienia oraz wspomagania hamowania na dobiegu polegający na zastosowaniu silnika pierścieniowego, dyskowego lub pierścieniowo-dyskowego zabudowanego w zewnętrznej części obręczy koła w ten sposób, że rotor silnika (1) z magnesami trwałymi jest połączony z krawędzią obręczy oraz jego tarcza jest połączona z wirującą piastą natomiast stojan silnika z cewką jest umieszczony wewnątrz pierścieni rotora lub równolegle do jego dysku, a tarcza stojana jest trwale osadzona na nieruchomej osi piasty koła (III).The method of direct drive of the landing gear wheels to the rotational speed corresponding to the touchdown speed and to assist the braking during the roll-out, consisting in the use of a ring, disc or ring-disc motor installed in the outer part of the wheel rim in such a way that the rotor of the motor (1) with permanent magnets is connected to the rim edge and its disc is connected to the rotating hub, while the stator of the motor with the coil is placed inside the rotor rings or parallel to its disc, and the stator disc is permanently mounted on the stationary axis of the wheel hub (III).

PL437565A 2021-04-09 2021-04-09 Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed PL437565A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL437565A PL437565A1 (en) 2021-04-09 2021-04-09 Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL437565A PL437565A1 (en) 2021-04-09 2021-04-09 Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed

Publications (1)

Publication Number Publication Date
PL437565A1 true PL437565A1 (en) 2022-10-10

Family

ID=83724405

Family Applications (1)

Application Number Title Priority Date Filing Date
PL437565A PL437565A1 (en) 2021-04-09 2021-04-09 Method of directly propelling an airplane landing gear wheel by a ring/disc motor during landing to impart rotational speed consistent with touchdown speed

Country Status (1)

Country Link
PL (1) PL437565A1 (en)

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