EP1187083A2 - Procédé et système pour surveiller les décollages et atterrissages des aéronefs - Google Patents

Procédé et système pour surveiller les décollages et atterrissages des aéronefs Download PDF

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Publication number
EP1187083A2
EP1187083A2 EP01121210A EP01121210A EP1187083A2 EP 1187083 A2 EP1187083 A2 EP 1187083A2 EP 01121210 A EP01121210 A EP 01121210A EP 01121210 A EP01121210 A EP 01121210A EP 1187083 A2 EP1187083 A2 EP 1187083A2
Authority
EP
European Patent Office
Prior art keywords
aircraft
video cameras
arrangement
image recordings
flames
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.)
Withdrawn
Application number
EP01121210A
Other languages
German (de)
English (en)
Other versions
EP1187083A3 (fr
Inventor
Hans Dipl.-Ing.; Pa Zapfe
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.)
ZAPFE HANS DIPL ING PA
Original Assignee
ZAPFE HANS DIPL ING PA
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 ZAPFE HANS DIPL ING PA filed Critical ZAPFE HANS DIPL ING PA
Publication of EP1187083A2 publication Critical patent/EP1187083A2/fr
Publication of EP1187083A3 publication Critical patent/EP1187083A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0043—Traffic management of multiple aircrafts from the ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0082—Surveillance aids for monitoring traffic from a ground station

Definitions

  • the invention relates to a method for monitoring starts and Landings of aircraft according to the preamble of the claim 1 and an arrangement according to the preamble of the claim 4th
  • DE 195 34 616 A1 is a tire pressure monitoring device known in the tire sensors and transmitters and antennas for the reception and transmission of the measured values (pressure and, if applicable, temperature) are assigned to a central evaluation device.
  • the capture from other defects, such as fires, which become much more severe to expand a disaster is not disclosed.
  • DE 41 215 A1 also only deals with radar monitoring Locating objects and obstacles as well as for detection and determination the rolling state of moving objects such as airplanes, ground vehicles et al Describing the acquisition of e.g. fallen engine parts.
  • Monitoring by row arrangements is also described of radar sensors with overlapping angular ranges from more than 90 degrees and the evaluation in a central station.
  • DE 36 88 660 T2 are airport surveillance, control and Fire fighting systems are known in which along the runways Rows of heat or infrared sensors are arranged through which Extinguishing devices assigned to runways, e.g. Hydrants, automatic can be activated to prevent aircraft fires and - in the event of collisions - combat broken aircraft parts. It can also be used to leave and burning fuel are extinguished. It is also possible to track, accompany and close a moving aircraft check if this is the row of overlapping sensor areas happens. It is also known to control a sensor tower feed in order to initiate the delete actions from there. A Image capture with high detail resolution is not disclosed.
  • EP 0 776 825 A1 is a navigation system for aircraft known in which there is a TV camera on board the aircraft. As a result, the track lighting should be used in poor visibility can be better grasped.
  • a display unit in the pilot's field of vision enables visualization of the corridors for taxiing, takeoff and landing. Monitoring of the outside of the aircraft is not provided.
  • the invention is therefore based on the object, a method and a Specify the arrangement, through the critical operating conditions as early as possible such as engine fires and spills from leaking fuel at takeoffs and / or landings can be identified after Possibility to cancel the start before the critical Speed is exceeded and / or the remaining length of the runway is no longer sufficient for an emergency stop or emergency landing.
  • video cameras are of particular importance as monitoring devices and their orientation towards the bottom of the aircraft including the engines since such cameras have high resolution and are bright even in daylight bright flames on a screen or monitor in high contrast reflect, right at the beginning of the damage. This stands in contrast to radar or heat and infrared sensors like this is indicated in the prior art.
  • Heat and infrared sensors also react to the hot,
  • the exhaust gases from the engines are barely visible during normal operation.
  • register Video cameras immediately the abnormality, and even if the Flames are still very small and they react instantly to enlargement of flames, so that immediately a damage report to the tower and / or the cockpit instrumentation can be passed around cancel the take-off early or initiate an emergency landing.
  • FIG. 1 In the figure is a runway 1 with boundary borders 2 and 3 shown.
  • An aircraft 4 is located on or just above the web 1 with engines 5 and undercarriages 6 two rows of video cameras 7 parallel to lane 1. These must be however, not arranged directly at the boundary borders 2 and 3 bejn, larger distances are quite possible. It can be seen that the video cameras 7 are aligned with the underside of the aircraft 4 are.
  • the “viewing angles” are indicated by dashed lines. This "perspective" should reach from the surface of the track to a height at which the critical aircraft parts while taxiing on the runway or move shortly after take off, so that an emergency stop or Emergency landing within the remaining length of runway 1 is possible. From this the most expedient placement of the video cameras 7 also results as well as their distances. However, it may also be appropriate to Set up video cameras 7 up to the end of a runway. So that's it less critical conditions possible, the crew and / or the Destination airport to give warnings if the takeoff is not canceled more is possible and / or a continuation flight at least up to one Nearby airport allowed for a stopover appears.
  • the tower staff can face critical conditions not perceive numerous aircraft parts or do not notice them in time; from the Bird's eye view and because of the distance of the tower the perception takes place of critical conditions on the underside of the aircraft - if at all - only with considerable delay, so that a transfer to the cockpit crew too late.
  • poor visibility e.g. through fog, rain or snowfall is the perception through that Tower staff additionally disabled or even impossible.
  • the cockpit crew even such perceptions are completely elusive.
  • the critical operating states include an unusual one Flames escaping from the engines also have flames coming from tanks exit, overheated brakes, flying sparks, thrown tire parts Etc.
  • the video cameras 7 can also be designed as infrared cameras. e.g. by using an infrared filter.
  • the "viewing angle" of the video cameras 7 can be determined by using remotely controlled zoom lenses can be changed. It is also possible through the use of known pan-tilt heads on the Video cameras 7 this the aircraft movement in horizontal and / or vertical direction and "zoom in" critical zones and track. This may allow the number of video cameras 7 be reduced.
  • the signal transmission can be done in a known manner by radio and / or - to fixed installations - by cable (glass fiber, metal) or the like.
  • a radio transmission sets appropriate transmitters and receiver ahead.
  • the video cameras 7 can be used in conjunction with corresponding data recordings and recording devices also for documentation used to record the black box supplement or replace.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Closed-Circuit Television Systems (AREA)
EP01121210A 2000-09-08 2001-09-05 Procédé et système pour surveiller les décollages et atterrissages des aéronefs Withdrawn EP1187083A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2000144365 DE10044365A1 (de) 2000-09-08 2000-09-08 Verfahren und Anordnung zum Überwachen von Starts und Landungen von Luftfahrzeugen
DE10044365 2000-09-08

Publications (2)

Publication Number Publication Date
EP1187083A2 true EP1187083A2 (fr) 2002-03-13
EP1187083A3 EP1187083A3 (fr) 2003-05-07

Family

ID=7655452

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01121210A Withdrawn EP1187083A3 (fr) 2000-09-08 2001-09-05 Procédé et système pour surveiller les décollages et atterrissages des aéronefs

Country Status (2)

Country Link
EP (1) EP1187083A3 (fr)
DE (1) DE10044365A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4845629A (en) * 1985-07-18 1989-07-04 General De Investigacion Y Desarrollo S.A. Airport surveillance systems
US4989084A (en) * 1989-11-24 1991-01-29 Wetzel Donald C Airport runway monitoring system
EP0744630A2 (fr) * 1995-05-26 1996-11-27 HE HOLDINGS, INC. dba HUGHES ELECTRONICS Système de surveillance pour aéroport et de signalisation d'incursion de piste
WO1997037336A1 (fr) * 1996-03-29 1997-10-09 Commonwealth Scientific And Industrial Research Organisation Systeme de detection d'avion

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4143215A1 (de) * 1991-12-30 1993-07-01 Deutsche Forsch Luft Raumfahrt System zur ortung von objekten und hindernissen sowie zur erfassung und bestimmung des rollzustands von beweglichen objekten, wie flugzeugen, bodenfahrzeugen u. ae.
RU2019472C1 (ru) * 1992-07-10 1994-09-15 Дмитрий Анатольевич Сафьян Телевизионная система для руления, взлета и посадки самолетов в сложных метеоусловиях
DE19516157A1 (de) * 1995-05-03 1996-11-07 Klaus Schaefer Verfahren und Löschanlage zur Brandbekämpfung
DE19534616B4 (de) * 1995-09-18 2007-01-11 Alpha-Beta Electronics Ag Reifendruck-Überwachungseinrichtung
DE19949737A1 (de) * 1999-10-15 2001-04-26 Apm Gmbh Airport Equipment Vorrichtung zur Führung von Luftfahrzeugen auf Landeplätzen

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4845629A (en) * 1985-07-18 1989-07-04 General De Investigacion Y Desarrollo S.A. Airport surveillance systems
US4989084A (en) * 1989-11-24 1991-01-29 Wetzel Donald C Airport runway monitoring system
EP0744630A2 (fr) * 1995-05-26 1996-11-27 HE HOLDINGS, INC. dba HUGHES ELECTRONICS Système de surveillance pour aéroport et de signalisation d'incursion de piste
WO1997037336A1 (fr) * 1996-03-29 1997-10-09 Commonwealth Scientific And Industrial Research Organisation Systeme de detection d'avion

Also Published As

Publication number Publication date
EP1187083A3 (fr) 2003-05-07
DE10044365A1 (de) 2002-04-04

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