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DE20218569U1 - Tire acceleration system for aircraft landing gear has paddle or motor drive - Google Patents

Tire acceleration system for aircraft landing gear has paddle or motor drive

Info

Publication number
DE20218569U1
DE20218569U1 DE20218569U DE20218569U DE20218569U1 DE 20218569 U1 DE20218569 U1 DE 20218569U1 DE 20218569 U DE20218569 U DE 20218569U DE 20218569 U DE20218569 U DE 20218569U DE 20218569 U1 DE20218569 U1 DE 20218569U1
Authority
DE
Germany
Prior art keywords
landing
landing gear
paddle
motor drive
aircraft 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.)
Expired - Lifetime
Application number
DE20218569U
Other languages
German (de)
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.)
WOZNY ANDREAS
Original Assignee
WOZNY ANDREAS
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 WOZNY ANDREAS filed Critical WOZNY ANDREAS
Priority to DE20218569U priority Critical patent/DE20218569U1/en
Publication of DE20218569U1 publication Critical patent/DE20218569U1/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

The tire acceleration landing system accelerates the tire using pilot operated freewheel coupled electric motor or wind force driven wheel fixed paddle to match landing speed.

Description

BeschreibungDescription

Bei der Erfindung handelt es sich um eine Erfindung aus dem Bereich Flugzeugtechnik / Flugzeugbau.The invention is an invention from the field of aircraft technology / aircraft construction.

Die Erfindung kann an allen Flugzeugen mit Fahrwerk unabhängig von Größe und Bauart eingesetzt werden.The invention can be used on all aircraft with landing gear, regardless of size and design.

Die Erfindung reduziert den Reifenverschleiß an Flugzeugreifen bei der Landung. Bisher werden beim Landen bzw. Aufsetzen des Flugzeugs auf die Landebahn die Reifen von Geschwindigkeit Null auf Landegeschwindigkeit (ca. 200 km/h und mehr) beschleunigt, was zu erheblichem Reifenverschleiß führt.The invention reduces tire wear on aircraft tires during landing. Until now, when the aircraft lands or touches down on the runway, the tires are accelerated from zero speed to landing speed (approx. 200 km/h and more), which leads to considerable tire wear.

Meine Problemlösung ist, dass sich die Fahrwerksreifen schon kurz vor dem Aufsetzen auf die Landebahn mit Landegeschwindigkeit drehen (ca. 200 km/h).My solution to the problem is that the landing gear tires rotate at landing speed (approx. 200 km/h) shortly before touching down on the runway.

Die Landegeschwindigkeit variiert und ist von vielen Faktoren abhängig, aus diesem Grund dürfen die Fahrwerksreifen nur mit der niedrigsten Landegeschwindigkeit drehen.Landing speed varies and depends on many factors, which is why the landing gear tires must only rotate at the lowest landing speed.

Das Drehen der Fahrwerksreifen kann durch zwei verschiedene Arten erfolgen:Rotating the chassis tires can be done in two different ways:

An den einzelnen Fahrwerksrädern sind beschaufelte Radscheiben, ähnlich einer Laufschaufelreihe einer Turbine angebracht, welche alle Fahrwerksräder durch den Fahrtwind in Drehung bringen, nachdem das Fahrgestell im Landeanflug ausgefahren wurde.Bladed wheel disks, similar to a row of turbine blades, are attached to the individual landing gear wheels, which cause all the landing gear wheels to rotate using the airflow after the landing gear has been extended during the landing approach.

Diese beschaufelten Radscheiben sind vom Durchmesser kleiner als die Reifen, aber mit den Rädern kraftschlüssig verbunden.These bladed wheel discs are smaller in diameter than the tires, but are frictionally connected to the wheels.

Die Bauart der beschaufelten Radscheiben muss dem einzelnen Flugzeugtyp angepasst sein.The design of the bladed wheel discs must be adapted to the individual aircraft type.

Sinngemäß wie unter Punkt 1. werden die Fahrwerksräder aber durch Elektromotoren angetrieben bis die Fahrwerkräder auf Landegeschwindigkeit drehen, was vom Piloten vorgegeben werden kann.As in point 1, the landing gear wheels are driven by electric motors until the landing gear wheels rotate to landing speed, which can be specified by the pilot.

Dadurch können für alle Landegeschwindigkeiten die optimalen Voraussetzungen erreicht werden.This allows optimal conditions to be achieved for all landing speeds.

Der Bremsvorgang unmittelbar nach der Landung erfolgt wie bisher mittels Umkehrschub der Triebwerke bei großen Flugzeugen und der Bremsen.The braking process immediately after landing is carried out as before by means of reverse thrust of the engines in large aircraft and the brakes.

Claims (1)

Reifen-Beschleunigungs-Landungs-System, dadurch gekennzeichnet, dass dieses aus beschaufelten Fahrwerksrädern besteht, die vor der Landung durch die Kraft des Windes oder mittels Elektromtoren mit Freilaufeinrichtung auf Landegeschwindigkeit beschleunigbar sind. Tire acceleration landing system, characterized in that it consists of bladed landing gear wheels which can be accelerated to landing speed before landing by the force of the wind or by means of electric motors with freewheel device.
DE20218569U 2002-11-29 2002-11-29 Tire acceleration system for aircraft landing gear has paddle or motor drive Expired - Lifetime DE20218569U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE20218569U DE20218569U1 (en) 2002-11-29 2002-11-29 Tire acceleration system for aircraft landing gear has paddle or motor drive

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE20218569U DE20218569U1 (en) 2002-11-29 2002-11-29 Tire acceleration system for aircraft landing gear has paddle or motor drive

Publications (1)

Publication Number Publication Date
DE20218569U1 true DE20218569U1 (en) 2003-06-12

Family

ID=7977489

Family Applications (1)

Application Number Title Priority Date Filing Date
DE20218569U Expired - Lifetime DE20218569U1 (en) 2002-11-29 2002-11-29 Tire acceleration system for aircraft landing gear has paddle or motor drive

Country Status (1)

Country Link
DE (1) DE20218569U1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8684300B2 (en) 2009-08-28 2014-04-01 Airbus Operations Limited Aircraft landing gear

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

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Legal Events

Date Code Title Description
R086 Non-binding declaration of licensing interest
R207 Utility model specification

Effective date: 20030717

R156 Lapse of ip right after 3 years

Effective date: 20060601