WO2022186826A1 - Système de caméras embarquées dans un aéronef - Google Patents

Système de caméras embarquées dans un aéronef Download PDF

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Publication number
WO2022186826A1
WO2022186826A1 PCT/US2021/020467 US2021020467W WO2022186826A1 WO 2022186826 A1 WO2022186826 A1 WO 2022186826A1 US 2021020467 W US2021020467 W US 2021020467W WO 2022186826 A1 WO2022186826 A1 WO 2022186826A1
Authority
WO
WIPO (PCT)
Prior art keywords
cameras
aircraft
housing
wing
bulkhead
Prior art date
Application number
PCT/US2021/020467
Other languages
English (en)
Inventor
Miller Colson
Original Assignee
Miller Colson
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 Miller Colson filed Critical Miller Colson
Priority to PCT/US2021/020467 priority Critical patent/WO2022186826A1/fr
Publication of WO2022186826A1 publication Critical patent/WO2022186826A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N21/00—Selective content distribution, e.g. interactive television or video on demand [VOD]
    • H04N21/20—Servers specifically adapted for the distribution of content, e.g. VOD servers; Operations thereof
    • H04N21/21—Server components or server architectures
    • H04N21/218—Source of audio or video content, e.g. local disk arrays
    • H04N21/2187—Live feed
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50—Constructional details
    • H04N23/51—Housings
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/57—Mechanical or electrical details of cameras or camera modules specially adapted for being embedded in other devices
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/90—Arrangement of cameras or camera modules, e.g. multiple cameras in TV studios or sports stadiums
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00—Television systems
    • H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • H04N7/181—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources

Definitions

  • the present invention relates to a system of cameras onboard an aircraft and, more particularly, to a system of cameras onboard an aircraft that allows the pilots of an aircraft to continuously view a display of the exterior and interior of an aircraft allowing the pilots access to more information to aid them in the event of an emergency.
  • Applicant believes that a related reference corresponds to U.S. patent No. 2002/0093564 disclosing a digital camera network for a commercial aircraft. However, it differs from the present invention because the reference fails to address the issue of providing a constant display of the exterior and interior of an aircraft provided by the present invention.
  • the present invention addresses these issues by providing a plurality of cameras of the present invention is adapted to capture the left wing, left engine, left main landing gear, left slat/flaps; right wing, right engine, right main landing gear, right slats/flaps; left stabilizer, left view of rudder; right stabilizer, right review of rudder; nose, landing gear; cockpit interior and baggage compartment.
  • the plurality of cameras are connected to display panel located in the cockpit of a plane via a system of wires.
  • Figure 1 represents a top view of aircraft 60 wherein a plurality of cameras 22 located at or near bulkhead station 62, a left wing 66, a right wing 64, a rudder 72, left stabilizer 76, and a right stabilizer 74 may be viewed.
  • Figure 2 shows a front view of aircraft 60 wherein a plurality of cameras 22 located at a bulkhead station 62, a left main landing gear 66C, and a right main landing gear 64C may be observed.
  • Figure 3 illustrates a side view of aircraft 60 wherein a baggage compartment 70, and a rudder 72 may be viewed.
  • Figure 4 is a representation of the interior of a cockpit 68 within an aircraft 60 wherein a plurality of display units 44, and a video selector unit 46 may be observed.
  • Figure 5 represents a view of the aircraft 60 in flight within a maintenance control tower 78.
  • Figure 6 shows an isometric view of a camera of the plurality of cameras 22 in accordance to an embodiment of the present invention.
  • Figure 7 illustrates a side view of a camera of the plurality of cameras 22 mounted on aircraft 60 in accordance to an embodiment of the present invention.
  • Camera assembly 20 includes a plurality of cameras 22 that are mounted on the exterior and interior of an aircraft 60.
  • the plurality of cameras 22 may be placed on or near a bulkhead station 62, a left wing 66, and a right wing 64 of the exterior of aircraft 60.
  • the plurality of cameras 22 may be placed within a cockpit 68 and a baggage compartment 70 of the interior of the aircraft 60.
  • the camera placed within cockpit 68 is to be used only in the event of an emergency onboard the aircraft.
  • the present embodiment of the plurality of cameras 22 is observed to be located on the aforementioned locations, it should be understood that other embodiments placing the plurality of cameras 22 on different locations of the aircraft 60 may be interpreted by those skilled in the art.
  • a camera of the plurality of cameras 22 may be placed thereon.
  • the camera of the plurality of cameras 22 placed on the aforementioned location may be placed to capture a left wing 66, left slats 66A, left flaps 66B, a left main landing gear 66C, and a left engine 67.
  • a camera of the plurality of cameras 22 may be placed thereon.
  • the camera of the plurality of cameras 22 placed on the aforementioned location may be placed to capture a right wing 64, right slats 64A, right flaps 64B, a right main landing gear 64C, and a right engine 65.
  • a camera of the plurality of cameras 22 may be placed inside the nose wheel weld area.
  • the camera of the plurality of cameras 22 placed on the aforementioned location may be placed to capture a nose landing gear 63.
  • Figure 6 depicts an embodiment of one of plurality of cameras 22.
  • the camera includes a housing which has a triangular shape with rounded edges. Further, the housing includes a top portion which protrudes outwardly from a top end of the housing. The top portion houses a camera lens and begins along a lateral edge of the housing. The top portion then partially extends towards an inner area of the top of the housing. It should be understood that the camera lens is in constant exposure from the top portion in order to constantly provide a pilot with a view of the outside of the aircraft during flight.
  • a camera of the plurality of cameras 22 may also be placed on the top of left wing 66 tip at or near the navigation lights assembly of left wing 66 of aircraft 60.
  • the camera of the plurality of cameras 22 placed on the aforementioned location may be placed to capture the left side of a rudder 72, a left stabilizer 76 and the left side of an AFT. fuselage 79.
  • a camera of the plurality of cameras 22 may also be placed on the top of right wing 64 tip at or near the navigation lights assembly of right wing 64 of aircraft 60 on the distal end of right wing 64 of aircraft 60.
  • the camera of the plurality of cameras 22 may be placed to capture the right side of the rudder 72 a right stabilizer 74, and the right side of an AFT. fuselage 79.
  • other embodiments of the plurality of cameras 22 placed on the left wing 66 and the top of right wing 64 tip at or near the navigation light assembly capturing other sections of the exterior of aircraft 60 may be interpreted.
  • a camera of the plurality of cameras 22 may also be placed within the cockpit 68 of the interior of aircraft 60.
  • the camera of the plurality of cameras 22 placed within the cockpit 68 may capture the pilots of aircraft 60 as well as the interior of the cockpit. This camera will only be activated when aircraft 60 experiences a true emergency.
  • a camera of the plurality of the cameras 22 may be placed within the baggage compartment 70 of the aircraft 60 to capture the interior of the baggage compartment.
  • Camera assembly 20 also comprises wires 24 located within the interior of aircraft 60. Wires 24 are used to communicably attach a plurality of cameras 22 to the video data management assembly 40.
  • Video data management assembly 40 includes a video data management computer 42, a plurality of display units 44, and a video selector unit 46. Video data management computer 42 is used to process and store the information being streamed from a plurality of cameras 22. Video data management computer 42 are communicably attached to the plurality of display units 44 located within the cockpit 68 of aircraft 60. Plurality of display units 44 is adapted to constantly stream the capture of the plurality of cameras 22.
  • video selector unit 46 When a pilot selects the desired view of an aircraft surface by using the video selector unit 46 it is communicably attached to a plurality of display units 44. Additionally, video selector unit 46 is adapted to allow the pilots to switch the capture of the plurality of cameras 22 on the plurality of display units 44.
  • video data management assembly 40 is adapted to stream the capture of a camera of the plurality cameras 22 inside the cockpit 68 to a maintenance control tower 78 in the event of an emergency.
  • the maintenance control tower 78 may be able to assist the pilots of aircraft 60 utilizing the information being streamed to the maintenance control tower 78.
  • the system of cameras onboard an aircraft has several implementations for industrial applicability.
  • the system of cameras onboard an aircraft is provided on commercial aircrafts to allow pilots to better observe different parts of the aircraft to ensure the safety of everyone onboard.
  • the system is beneficial in that it provides a continuous stream of visuals of the exterior and interior of said aircraft to the pilots in the cockpit in order to increase the safety of the aircraft.
  • the system can record and store the data gathered by the cameras on a computer thereby providing more information in the event of an emergency.
  • the system can also provide maintenance control of said aircraft a live video stream of the pilots inside the cockpit.
  • the system for cameras onboard an aircraft includes a video data management computer that is modified to record and store the date being streamed from the cameras located on the aircraft to a computer. Additionally, a video selector unit is adapted to allow the pilots to switch between different views of the cameras. Furthermore, the video data management computer will stream the video feed of the cockpit camera to maintenance control of the aircraft in the event of an emergency.

Abstract

L'invention concerne un système de caméras embarquées dans un aéronef comprenant un ensemble caméra et un ensemble de gestion de données vidéo. L'ensemble caméra est modifié pour aider les pilotes d'un aéronef en fournissant un flux visuel continu de différentes sections de l'aéronef. L'aide visuelle fournie aux pilotes à partir de l'ensemble caméra aide les pilotes à identifier des problèmes et des solutions en cas d'urgence. Le système pour caméras embarquées dans un aéronef comprend en outre un ordinateur de gestion de données vidéo qui est modifié pour enregistrer et stocker la date qui est diffusée en continu à partir des caméras situées sur l'aéronef vers un ordinateur. De plus, l'unité de sélection vidéo est conçue pour permettre aux pilotes de commuter entre différentes vues des caméras. En outre, l'ordinateur de gestion de données vidéo diffuse le flux vidéo de la caméra de poste de pilotage à la commande de maintenance de l'aéronef en cas d'urgence.
PCT/US2021/020467 2021-03-02 2021-03-02 Système de caméras embarquées dans un aéronef WO2022186826A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/US2021/020467 WO2022186826A1 (fr) 2021-03-02 2021-03-02 Système de caméras embarquées dans un aéronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2021/020467 WO2022186826A1 (fr) 2021-03-02 2021-03-02 Système de caméras embarquées dans un aéronef

Publications (1)

Publication Number Publication Date
WO2022186826A1 true WO2022186826A1 (fr) 2022-09-09

Family

ID=83155160

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2021/020467 WO2022186826A1 (fr) 2021-03-02 2021-03-02 Système de caméras embarquées dans un aéronef

Country Status (1)

Country Link
WO (1) WO2022186826A1 (fr)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020004695A1 (en) * 2000-02-03 2002-01-10 Glenn Matthew H. Event based aircraft image and data recording system
US20020093564A1 (en) * 2001-01-12 2002-07-18 Danny Israel Digital camera network for commercial aircraft
US20040008253A1 (en) * 2002-07-10 2004-01-15 Monroe David A. Comprehensive multi-media surveillance and response system for aircraft, operations centers, airports and other commercial transports, centers and terminals
US20070215746A1 (en) * 2004-03-29 2007-09-20 Rieken William D Aircraft Having A Ring-Shaped Wing Structure
US20160014443A1 (en) * 2014-07-08 2016-01-14 Umm Al-Qura University Broadcasting of land, water, and air cameras
US20200307825A1 (en) * 2019-03-28 2020-10-01 Airbus Operations Gmbh Camera module and system for surveillance of a passenger cabin of an aircraft, and aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020004695A1 (en) * 2000-02-03 2002-01-10 Glenn Matthew H. Event based aircraft image and data recording system
US20020093564A1 (en) * 2001-01-12 2002-07-18 Danny Israel Digital camera network for commercial aircraft
US20040008253A1 (en) * 2002-07-10 2004-01-15 Monroe David A. Comprehensive multi-media surveillance and response system for aircraft, operations centers, airports and other commercial transports, centers and terminals
US20070215746A1 (en) * 2004-03-29 2007-09-20 Rieken William D Aircraft Having A Ring-Shaped Wing Structure
US20160014443A1 (en) * 2014-07-08 2016-01-14 Umm Al-Qura University Broadcasting of land, water, and air cameras
US20200307825A1 (en) * 2019-03-28 2020-10-01 Airbus Operations Gmbh Camera module and system for surveillance of a passenger cabin of an aircraft, and aircraft

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