WO2003045777A1 - Aircraft monitoring system (ams) '3-d box' - Google Patents
Aircraft monitoring system (ams) '3-d box' Download PDFInfo
- Publication number
- WO2003045777A1 WO2003045777A1 PCT/AU2002/001613 AU0201613W WO03045777A1 WO 2003045777 A1 WO2003045777 A1 WO 2003045777A1 AU 0201613 W AU0201613 W AU 0201613W WO 03045777 A1 WO03045777 A1 WO 03045777A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- box
- section
- ground station
- video images
- Prior art date
Links
- 238000012544 monitoring process Methods 0.000 title abstract description 5
- 230000007935 neutral effect Effects 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 abstract description 3
- 238000004880 explosion Methods 0.000 abstract description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000029305 taxis Effects 0.000 description 1
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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0051—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft
- B64D45/0053—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by monitoring passengers or crew on aircraft using visual equipment, e.g. cameras
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0059—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by communicating emergency situations to ground control or between crew members
-
- 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
Definitions
- the inflight cameras will record and send, in the event of turbulence, factors such as behaviour of passengers and their safety and the behaviour of other items inside the aircraft itself.
- the cameras inside the cabin has the over ride function to focus and zoom in the direction of a sick patient for a doctor on the ground to inspect closely via the cameras.
- This project will create thousands of jobs and generate a huge revenue all over the world and on different networks, it will also assist the air traffic controllers all over the world.
- the ability to transmit video images can also be used on commercial basis such as inflight video phones.
- the aircraft can be controlled from Base Station/s.
- the controls of the aircraft can be over-ridden by the Ground Station in an Emergency or Hijack of the aircraft / Where the pilots are vulnerable.
- the hijackers take control of the aircraft, then, it can be over-ridden from Base Station/s by transmitting information and different parameters such as Heading, Course (Flight Path), Air Speed, etc to the AUTOPILOT COMMAND of the aircraft. In this way the aircraft can be controlled completely by the Base Station, simply by sending message/a to the AUTO PILOT receiver, by means of ENCRYPTION for total safety of hacking.
- this method of surveillance can also be used in transpor /s such as Buses, Trains, cars/Taxis, Trucks.
- the destination code will be input through 3-D Box, to the AUTO PIL T CONTROL SYSTEM.
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2002364766A AU2002364766A1 (en) | 2001-11-29 | 2002-11-28 | Aircraft monitoring system (ams) "3-d box" |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPR9191A AUPR919101A0 (en) | 2001-11-29 | 2001-11-29 | Aircraft monitoring system (ams) 3-d box |
AUPR9191 | 2001-11-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2003045777A1 true WO2003045777A1 (en) | 2003-06-05 |
Family
ID=3833000
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU2002/001613 WO2003045777A1 (en) | 2001-11-29 | 2002-11-28 | Aircraft monitoring system (ams) '3-d box' |
Country Status (2)
Country | Link |
---|---|
AU (1) | AUPR919101A0 (en) |
WO (1) | WO2003045777A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007002493A1 (en) * | 2007-01-17 | 2008-08-21 | Franz Butschek | Airplane control camera system has rotary cameras designed in aerodynamic manner and are responsible for nose landing gear or main landing gear and contain heated protective glass housing |
CN106034147A (en) * | 2015-03-16 | 2016-10-19 | 北京军懋国兴科技股份有限公司 | Multi-machine aircraft data real -time monitoring system |
CN113720676A (en) * | 2021-08-16 | 2021-11-30 | 中国飞机强度研究所 | Deformation damage detection system that interior cabin was patrolled and examined among aircraft structure fatigue test |
CN113740185A (en) * | 2021-08-16 | 2021-12-03 | 中国飞机强度研究所 | Structure is patrolled and examined to aircraft inner cabin structural damage among aircraft fatigue test |
CN113740185B (en) * | 2021-08-16 | 2024-05-03 | 中国飞机强度研究所 | Aircraft inner cabin structural damage inspection framework in aircraft fatigue test |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH092399A (en) * | 1995-06-22 | 1997-01-07 | Toshifumi Kadokawa | Aircraft emergency condition grasping and monitoring system |
JPH0920297A (en) * | 1995-07-05 | 1997-01-21 | Nippon Seigyo:Kk | Aircraft hijack settlement assisting device |
JPH0936791A (en) * | 1995-07-19 | 1997-02-07 | Toyo Commun Equip Co Ltd | Emergency communication equipment using satellite communication system |
JPH0993566A (en) * | 1995-09-20 | 1997-04-04 | Fujitsu General Ltd | In-aircraft monitor system |
US5742336A (en) * | 1996-12-16 | 1998-04-21 | Lee; Frederick A. | Aircraft surveillance and recording system |
US6092008A (en) * | 1997-06-13 | 2000-07-18 | Bateman; Wesley H. | Flight event record system |
US6173219B1 (en) * | 1996-06-07 | 2001-01-09 | Sextant Avionique | Method for automatically controlling a vehicle for the lateral avoidance of a fixed zone |
CA2305882A1 (en) * | 2000-04-19 | 2001-10-19 | Panahi Kaumarce | Flight & navigation control unit |
DE20116233U1 (en) * | 2001-10-02 | 2001-11-29 | Koch Rene | Anti-terrorism system |
-
2001
- 2001-11-29 AU AUPR9191A patent/AUPR919101A0/en not_active Abandoned
-
2002
- 2002-11-28 WO PCT/AU2002/001613 patent/WO2003045777A1/en not_active Application Discontinuation
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH092399A (en) * | 1995-06-22 | 1997-01-07 | Toshifumi Kadokawa | Aircraft emergency condition grasping and monitoring system |
JPH0920297A (en) * | 1995-07-05 | 1997-01-21 | Nippon Seigyo:Kk | Aircraft hijack settlement assisting device |
JPH0936791A (en) * | 1995-07-19 | 1997-02-07 | Toyo Commun Equip Co Ltd | Emergency communication equipment using satellite communication system |
JPH0993566A (en) * | 1995-09-20 | 1997-04-04 | Fujitsu General Ltd | In-aircraft monitor system |
US6173219B1 (en) * | 1996-06-07 | 2001-01-09 | Sextant Avionique | Method for automatically controlling a vehicle for the lateral avoidance of a fixed zone |
US5742336A (en) * | 1996-12-16 | 1998-04-21 | Lee; Frederick A. | Aircraft surveillance and recording system |
US6092008A (en) * | 1997-06-13 | 2000-07-18 | Bateman; Wesley H. | Flight event record system |
CA2305882A1 (en) * | 2000-04-19 | 2001-10-19 | Panahi Kaumarce | Flight & navigation control unit |
DE20116233U1 (en) * | 2001-10-02 | 2001-11-29 | Koch Rene | Anti-terrorism system |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007002493A1 (en) * | 2007-01-17 | 2008-08-21 | Franz Butschek | Airplane control camera system has rotary cameras designed in aerodynamic manner and are responsible for nose landing gear or main landing gear and contain heated protective glass housing |
DE102007002493B4 (en) * | 2007-01-17 | 2013-03-14 | Franz Butschek | Flight control camera system |
CN106034147A (en) * | 2015-03-16 | 2016-10-19 | 北京军懋国兴科技股份有限公司 | Multi-machine aircraft data real -time monitoring system |
CN113720676A (en) * | 2021-08-16 | 2021-11-30 | 中国飞机强度研究所 | Deformation damage detection system that interior cabin was patrolled and examined among aircraft structure fatigue test |
CN113740185A (en) * | 2021-08-16 | 2021-12-03 | 中国飞机强度研究所 | Structure is patrolled and examined to aircraft inner cabin structural damage among aircraft fatigue test |
CN113740185B (en) * | 2021-08-16 | 2024-05-03 | 中国飞机强度研究所 | Aircraft inner cabin structural damage inspection framework in aircraft fatigue test |
Also Published As
Publication number | Publication date |
---|---|
AUPR919101A0 (en) | 2001-12-20 |
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