DE20013599U1 - Protective device for aircraft wheels - Google Patents

Protective device for aircraft wheels

Info

Publication number
DE20013599U1
DE20013599U1 DE20013599U DE20013599U DE20013599U1 DE 20013599 U1 DE20013599 U1 DE 20013599U1 DE 20013599 U DE20013599 U DE 20013599U DE 20013599 U DE20013599 U DE 20013599U DE 20013599 U1 DE20013599 U1 DE 20013599U1
Authority
DE
Germany
Prior art keywords
protection device
mudguard
wheels
aircraft
fender
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
DE20013599U
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.)
MAE AUTODESIGN GmbH
Original Assignee
MAE AUTODESIGN GmbH
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 MAE AUTODESIGN GmbH filed Critical MAE AUTODESIGN GmbH
Priority to DE20013599U priority Critical patent/DE20013599U1/en
Publication of DE20013599U1 publication Critical patent/DE20013599U1/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 
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Description

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßt The description text was not recorded electronically  

Der Beschreibungstext wurde nicht elektronisch erfaßtThe description text was not recorded electronically

Claims (9)

1. Schutzeinrichtung für Flugzeuglaufräder umfassend mindestens ein Schutzblech (16), das zumindest entlang eines Teilumfangs der Flugzeuglaufräder (10) um den oberen Teil einer Lauffläche (14) der Flugzeuglaufräder (10) herumgeführt ist und diese abdeckt und mindestens eine Halteeinrichtung (17) zum Befestigen des mindestens einen Schutzblechs (16) an starren Fahrwerksteilen (32) eines die Laufräder (10) umfassenden Fahrwerks (32) und/oder mindestens eine Radachse (18) mindestens eines Flugzeuglaufrades (10).1. Protection device for aircraft wheels comprising at least one protective plate ( 16 ) which is guided around at least along a partial circumference of the aircraft wheels ( 10 ) around the upper part of a tread ( 14 ) of the aircraft wheels ( 10 ) and covers them and at least one holding device ( 17 ) for attaching the at least one protective sheet (16) to the rigid chassis parts (32) of the impellers (10) comprising running gear (32) and / or at least one wheel axle (18) of at least one aircraft wheel (10). 2. Schutzeinrichtung nach Anspruch 1, wobei das Schutzblech (16) mindestens einen Teilumfang der Laufräder (10) im Bereich des oberen hinteren Teils des Flugzeuglaufrades (10) überdeckt.2. Protection device according to claim 1, wherein the mudguard ( 16 ) covers at least a partial circumference of the wheels ( 10 ) in the region of the upper rear part of the aircraft wheel ( 10 ). 3. Schutzeinrichtung nach Anspruch 1 oder 2, wobei jedes Laufrad (10) ein separates Schutzblech (16) aufweist.3. Protection device according to claim 1 or 2, wherein each impeller ( 10 ) has a separate protective plate ( 16 ). 4. Schutzeinrichtung nach Anspruch 1 oder 2, wobei jeweils zwei gleichseitige bzw. die zwei vorderen und/oder die zwei hinteren Laufräder (10) ein gemeinsames Schutzblech (16) aufweisen.4. Protection device according to claim 1 or 2, wherein in each case two equilateral or the two front and / or the two rear wheels ( 10 ) have a common mudguard ( 16 ). 5. Schutzeinrichtung nach Anspruch 1 oder 2, wobei alle Laufräder (10) des Fahrwerks (32) durch ein gemeinsames Schutzblech (16) abgedeckt sind.5. Protection device according to claim 1 or 2, wherein all the wheels ( 10 ) of the chassis ( 32 ) are covered by a common mudguard ( 16 ). 6. Schutzeinrichtung nach einem oder mehreren der Ansprüche 1 bis 5, wobei das mindestens eine Schutzblech (16) im wesentlichen nur die Lauffläche (14) der Laufräder (10) überspannt.6. Protection device according to one or more of claims 1 to 5, wherein the at least one mudguard ( 16 ) spans essentially only the tread ( 14 ) of the wheels ( 10 ). 7. Schutzeinrichtung nach einem oder mehreren der Ansprüche 1 bis 6, wobei das Schutzblech (16) aus einem dünnen Stahl-, Aluminium- und/oder Titanblech und/oder einem hochfesten Kunststoff- Verbundmaterial besteht.7. Protection device according to one or more of claims 1 to 6, wherein the fender ( 16 ) consists of a thin steel, aluminum and / or titanium sheet and / or a high-strength plastic composite material. 8. Schutzeinrichtung nach einem oder mehreren der Ansprüche 1 bis 7, wobei das mindestens eine Schutzblech (16) gelocht, geschlitzt, strukturiert und/oder aus verschiedenen Materialschichten aufgebaut ist.8. Protection device according to one or more of claims 1 to 7, wherein the at least one mudguard ( 16 ) is perforated, slotted, structured and / or constructed from different material layers. 9. Schutzeinrichtung nach einem oder mehreren der Ansprüche 1 bis 8, wobei das Schutzblech (16) an seiner bei Vorwärtsfahrt des Flugzeugs vorne liegenden Kante so ausgebildet ist, daß Luft durch die Vorwärtsbewegung des Flugzeugs zwischen dem Laufrad (10) und dem Schutzblech (16) eintritt und an der gegenüberliegenden Schutzblechkante (39) bzw. durch Schlitze (38) im Schutzblech (16) im hinteren Laufradbereich wieder austritt.9. Protection device according to one or more of claims 1 to 8, wherein the mudguard ( 16 ) is formed on its front edge when the aircraft is moving forward so that air is caused by the forward movement of the aircraft between the impeller ( 10 ) and the mudguard ( 16 ) enters and exits at the opposite fender edge ( 39 ) or through slots ( 38 ) in the fender ( 16 ) in the rear impeller area.
DE20013599U 2000-08-03 2000-08-03 Protective device for aircraft wheels Expired - Lifetime DE20013599U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE20013599U DE20013599U1 (en) 2000-08-03 2000-08-03 Protective device for aircraft wheels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE20013599U DE20013599U1 (en) 2000-08-03 2000-08-03 Protective device for aircraft wheels

Publications (1)

Publication Number Publication Date
DE20013599U1 true DE20013599U1 (en) 2001-12-13

Family

ID=7944888

Family Applications (1)

Application Number Title Priority Date Filing Date
DE20013599U Expired - Lifetime DE20013599U1 (en) 2000-08-03 2000-08-03 Protective device for aircraft wheels

Country Status (1)

Country Link
DE (1) DE20013599U1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2436685A (en) * 2005-10-31 2007-10-03 Boeing Co Mesh fender for protecting an aircraft against foreign object damage
FR2903381A1 (en) * 2006-07-10 2008-01-11 Airbus France Sas AIRCRAFT PROTECTED FROM PROJECTIONS OF PNEUMATIC DEBRIS

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572342A (en) * 1946-09-03 1951-10-23 James C Huett Aircraft mudguard
DE4012277A1 (en) * 1990-04-17 1991-10-24 Warth Adolf G Dipl Ing Fh Drag reduction air channel - is shaped to accommodate gas, air or fluid medium accelerated to twice vehicle speed

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572342A (en) * 1946-09-03 1951-10-23 James C Huett Aircraft mudguard
DE4012277A1 (en) * 1990-04-17 1991-10-24 Warth Adolf G Dipl Ing Fh Drag reduction air channel - is shaped to accommodate gas, air or fluid medium accelerated to twice vehicle speed

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Aviation Week & Space Technology, H.17.3.69, S.54 *
KENS,Karlheinz, NOWARRA,Heinz J.: Die deutschen Flugzeuge 1933-1945, J.F. Lehmanns Verlag, München, 3.Aufl., S.682,683,692,693,709 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2436685A (en) * 2005-10-31 2007-10-03 Boeing Co Mesh fender for protecting an aircraft against foreign object damage
GB2436685B (en) * 2005-10-31 2008-04-09 Boeing Co A mesh fender for protecting an aircraft against damage from foreign objects
FR2903381A1 (en) * 2006-07-10 2008-01-11 Airbus France Sas AIRCRAFT PROTECTED FROM PROJECTIONS OF PNEUMATIC DEBRIS
US7669798B2 (en) 2006-07-10 2010-03-02 Airbus France Airplane protected against projections of tire debris

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Legal Events

Date Code Title Description
R163 Identified publications notified
R207 Utility model specification

Effective date: 20020124

R156 Lapse of ip right after 3 years

Effective date: 20040302