AU2001288375A1 - Audio feedback regarding aircraft operation - Google Patents
Audio feedback regarding aircraft operationInfo
- Publication number
- AU2001288375A1 AU2001288375A1 AU2001288375A AU8837501A AU2001288375A1 AU 2001288375 A1 AU2001288375 A1 AU 2001288375A1 AU 2001288375 A AU2001288375 A AU 2001288375A AU 8837501 A AU8837501 A AU 8837501A AU 2001288375 A1 AU2001288375 A1 AU 2001288375A1
- Authority
- AU
- Australia
- Prior art keywords
- aircraft
- feedback regarding
- audio feedback
- aircraft operation
- pilot
- 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.)
- Abandoned
Links
Classifications
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C3/00—Registering or indicating the condition or the working of machines or other apparatus, other than vehicles
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Circuit For Audible Band Transducer (AREA)
- Radio Relay Systems (AREA)
- Electrophonic Musical Instruments (AREA)
- Push-Button Switches (AREA)
Abstract
A method, system, and apparatus, for providing audio feedback regarding the operation of an aircraft. In one aspect, microphones are placed next to sound sources, which could be components of the aircraft. Audio inputs are received from the microphone and analyzed based on a psycho-acoustic model to provide settings, such as level, pan, and equalization, to an automatic mixer. The automatic mixer mixes the sounds based on the settings and provides audio output to the pilot of the aircraft. The pilot can then use the audio output to more effectively monitor the operations of the aircraft components, which might otherwise be difficult or impossible to hear.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/644,752 | 2000-08-23 | ||
US09/644,752 US7181020B1 (en) | 2000-08-23 | 2000-08-23 | Audio feedback regarding aircraft operation |
PCT/US2001/026425 WO2002016202A2 (en) | 2000-08-23 | 2001-08-23 | Audio feedback regarding aircraft operation |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2001288375A1 true AU2001288375A1 (en) | 2002-03-04 |
Family
ID=24586189
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2001288375A Abandoned AU2001288375A1 (en) | 2000-08-23 | 2001-08-23 | Audio feedback regarding aircraft operation |
Country Status (6)
Country | Link |
---|---|
US (1) | US7181020B1 (en) |
EP (1) | EP1373070B1 (en) |
AT (1) | ATE312755T1 (en) |
AU (1) | AU2001288375A1 (en) |
DE (1) | DE60115961T2 (en) |
WO (1) | WO2002016202A2 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005047274A1 (en) * | 2003-11-12 | 2005-05-26 | Dr. Reddy's Laboratories, Inc. | Preparation of escitalopram |
JP4491586B2 (en) * | 2004-08-06 | 2010-06-30 | 独立行政法人 宇宙航空研究開発機構 | Low noise flight support system |
DE102005001345B4 (en) * | 2004-11-10 | 2013-01-31 | Ask Industries Gmbh | Method and device for processing and reproducing audio signals |
US20060283190A1 (en) * | 2005-06-16 | 2006-12-21 | Pratt & Whitney Canada Corp. | Engine status detection with external microphone |
US8670573B2 (en) * | 2008-07-07 | 2014-03-11 | Robert Bosch Gmbh | Low latency ultra wideband communications headset and operating method therefor |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2748372A (en) | 1953-10-16 | 1956-05-29 | Northrop Aircraft Inc | Stall warning device |
US4538777A (en) | 1981-03-02 | 1985-09-03 | Hall Sherman E | Low thrust detection system for aircraft engines |
DE3327076A1 (en) | 1983-07-19 | 1985-01-31 | Klaus 5000 Köln Ebinger | Circuit arrangement for the acoustic and/or visual monitoring of the cabin and of the cockpit of an aircraft |
US4941187A (en) * | 1984-02-03 | 1990-07-10 | Slater Robert W | Intercom apparatus for integrating disparate audio sources for use in light aircraft or similar high noise environments |
US4952931A (en) | 1987-01-27 | 1990-08-28 | Serageldin Ahmedelhadi Y | Signal adaptive processor |
US4831438A (en) * | 1987-02-25 | 1989-05-16 | Household Data Services | Electronic surveillance system |
GB8902645D0 (en) | 1989-02-07 | 1989-03-30 | Smiths Industries Plc | Monitoring |
CA2067414A1 (en) | 1991-05-03 | 1992-11-04 | Bill Sacks | Psycho acoustic pseudo stereo foldback system |
US5406487A (en) * | 1991-10-11 | 1995-04-11 | Tanis; Peter G. | Aircraft altitude approach control device |
US5228093A (en) | 1991-10-24 | 1993-07-13 | Agnello Anthony M | Method for mixing source audio signals and an audio signal mixing system |
DE69523056T2 (en) * | 1994-07-28 | 2002-02-07 | Boeing Co | ACTIVE CONTROL OF BLOWER NOISE IN GAS TURBINE CHANNELS |
GB2314542A (en) | 1996-06-25 | 1998-01-07 | Trevor Henry | Pilot flight safety advisor and flight/mission controller |
US5798458A (en) * | 1996-10-11 | 1998-08-25 | Raytheon Ti Systems, Inc. | Acoustic catastrophic event detection and data capture and retrieval system for aircraft |
US6366311B1 (en) * | 1996-10-11 | 2002-04-02 | David A. Monroe | Record and playback system for aircraft |
US5864820A (en) | 1996-12-20 | 1999-01-26 | U S West, Inc. | Method, system and product for mixing of encoded audio signals |
US5894285A (en) | 1997-08-29 | 1999-04-13 | Motorola, Inc. | Method and apparatus to sense aircraft pilot ejection for rescue radio actuation |
US6275590B1 (en) * | 1998-09-17 | 2001-08-14 | Robert S. Prus | Engine noise simulating novelty device |
US6012426A (en) | 1998-11-02 | 2000-01-11 | Ford Global Technologies, Inc. | Automated psychoacoustic based method for detecting borderline spark knock |
IT1306612B1 (en) * | 1998-11-11 | 2001-06-18 | Marco Testi | INTERFACE METHOD BETWEEN A PILOT AND THE SURFACES OF AN AIRCRAFT, INTERFACE EQUIPMENT TO IMPLEMENT SUCH METHOD AND SENSORS |
US6545601B1 (en) * | 1999-02-25 | 2003-04-08 | David A. Monroe | Ground based security surveillance system for aircraft and other commercial vehicles |
US6366862B1 (en) * | 2000-04-19 | 2002-04-02 | National Instruments Corporation | System and method for analyzing signals generated by rotating machines |
-
2000
- 2000-08-23 US US09/644,752 patent/US7181020B1/en not_active Expired - Fee Related
-
2001
- 2001-08-23 AU AU2001288375A patent/AU2001288375A1/en not_active Abandoned
- 2001-08-23 WO PCT/US2001/026425 patent/WO2002016202A2/en active IP Right Grant
- 2001-08-23 AT AT01968100T patent/ATE312755T1/en not_active IP Right Cessation
- 2001-08-23 EP EP01968100A patent/EP1373070B1/en not_active Expired - Lifetime
- 2001-08-23 DE DE60115961T patent/DE60115961T2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO2002016202A2 (en) | 2002-02-28 |
DE60115961D1 (en) | 2006-01-19 |
ATE312755T1 (en) | 2005-12-15 |
DE60115961T2 (en) | 2006-08-03 |
EP1373070B1 (en) | 2005-12-14 |
EP1373070A2 (en) | 2004-01-02 |
US7181020B1 (en) | 2007-02-20 |
WO2002016202A3 (en) | 2003-10-09 |
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