PL399836A1 - Dynamic landing gear suspension - Google Patents

Dynamic landing gear suspension

Info

Publication number
PL399836A1
PL399836A1 PL399836A PL39983612A PL399836A1 PL 399836 A1 PL399836 A1 PL 399836A1 PL 399836 A PL399836 A PL 399836A PL 39983612 A PL39983612 A PL 39983612A PL 399836 A1 PL399836 A1 PL 399836A1
Authority
PL
Poland
Prior art keywords
kinetic energy
flail
gears
rotor
chassis
Prior art date
Application number
PL399836A
Other languages
Polish (pl)
Inventor
Przemyslaw Lagiewka
Stanisław Gumuła
Mariusz Wszendybył
Original Assignee
Centrum Badawczo-Rozwojowe Epar Spólka Z Ograniczona Odpowiedzialnoscia
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 Centrum Badawczo-Rozwojowe Epar Spólka Z Ograniczona Odpowiedzialnoscia filed Critical Centrum Badawczo-Rozwojowe Epar Spólka Z Ograniczona Odpowiedzialnoscia
Priority to PL399836A priority Critical patent/PL399836A1/en
Publication of PL399836A1 publication Critical patent/PL399836A1/en

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Abstract

Dynamiczny uklad amortyzacji podwozia samolotu zawiera uklad jezdny (103) mocowalny do podwozia (102) za posrednictwem wirnikowego urzadzenia do przejmowania i rozpraszania energii zderzenia, przy czym wirnikowe urzadzenie do przejmowania i rozpraszania energii zderzenia zawiera przymocowany do ukladu jezdnego (103) element bijakowy (1) sprzezony suwliwie za pomoca bijakowych prowadnic z bocznymi scianami plyty korpusowej (13) mocowalnej do plyty podwozia (102) samolotu, który wspólpracuje z co najmniej dwiema sprzezonymi szeregowo zebatkami (2, 3, 4) osadzonymi suwliwie na prowadnicy przymocowanej do plyty korpusowej (13) i napedzajacymi kola zebate (9), wirnikowych akumulatorów energii kinetycznej (10, 11, 12), przy czym pomiedzy elementem bijakowym (1) i pierwsza zebatka (2) oraz pomiedzy zebatkami (2, 3, 4) utworzone sa odstepy zapewniajace dzialanie elementów amortyzujacych (8) i umozliwiajace przesuw elementu bijakowego (1) wzgledem zebatek (2, 3, 4) jak równiez przesuw tych zebatek (2, 3, 4) wzgledem siebie, tak aby przesuwajacy sie element bijakowy (1) przekazywal energie kinetyczna ruchu postepowego do wirnikowych akumulatorów energii kinetycznej (10, 11, 12) w celu jej przetworzenia na energie kinetyczna ruchu obrotowego.The dynamic suspension system of the aircraft chassis comprises a running gear (103) fastened to the chassis (102) via a rotor device for absorbing and dissipating collision energy, the rotor device for absorbing and dissipating collision energy comprising a flail element attached to the running gear (103) ) slidably coupled by means of flail guides with side walls of the body plate (13) fixed to the chassis plate (102) of the aircraft, which cooperates with at least two in-line teeth (2, 3, 4) mounted slidably on a guide attached to the body plate (13 ) and driving gears (9), rotor accumulators of kinetic energy (10, 11, 12), with spacing between the beater element (1) and the first gear (2) and between the gears (2, 3, 4) shock absorbing elements (8) and enabling the flail element (1) to move relative to the teeth (2, 3, 4) as well as gears (2, 3, 4) in relation to each other, so that the moving flail element (1) transmits the kinetic energy of the progressive motion to the rotor accumulators of kinetic energy (10, 11, 12) in order to convert it into the kinetic energy of the rotational motion.

PL399836A 2012-07-05 2012-07-05 Dynamic landing gear suspension PL399836A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL399836A PL399836A1 (en) 2012-07-05 2012-07-05 Dynamic landing gear suspension

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL399836A PL399836A1 (en) 2012-07-05 2012-07-05 Dynamic landing gear suspension

Publications (1)

Publication Number Publication Date
PL399836A1 true PL399836A1 (en) 2014-01-07

Family

ID=49877274

Family Applications (1)

Application Number Title Priority Date Filing Date
PL399836A PL399836A1 (en) 2012-07-05 2012-07-05 Dynamic landing gear suspension

Country Status (1)

Country Link
PL (1) PL399836A1 (en)

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