IT8448340A0 - Sistema per avvisare il pilota di un aereo ad ala rotante di velocita' discensionale eccessiva - Google Patents
Sistema per avvisare il pilota di un aereo ad ala rotante di velocita' discensionale eccessivaInfo
- Publication number
- IT8448340A0 IT8448340A0 IT8448340A IT4834084A IT8448340A0 IT 8448340 A0 IT8448340 A0 IT 8448340A0 IT 8448340 A IT8448340 A IT 8448340A IT 4834084 A IT4834084 A IT 4834084A IT 8448340 A0 IT8448340 A0 IT 8448340A0
- Authority
- IT
- Italy
- Prior art keywords
- descental
- warn
- pilot
- excessive
- speed
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
- G01C5/005—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Emergency Alarm Devices (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Alarm Systems (AREA)
- Retarders (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/503,218 US4551723A (en) | 1983-06-10 | 1983-06-10 | Excessive descent rate warning system for rotary wing aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8448340A0 true IT8448340A0 (it) | 1984-06-07 |
IT1208683B IT1208683B (it) | 1989-07-10 |
Family
ID=24001197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8448340A IT1208683B (it) | 1983-06-10 | 1984-06-07 | Sistema per avvisare il pilota di un aereo ad ala rotante di velocita' discensionale eccessiva |
Country Status (15)
Country | Link |
---|---|
US (1) | US4551723A (it) |
JP (1) | JPS608194A (it) |
AU (1) | AU548328B2 (it) |
BE (1) | BE899878A (it) |
CA (1) | CA1213013A (it) |
CH (1) | CH660157A5 (it) |
DE (1) | DE3417834A1 (it) |
FI (1) | FI841929A (it) |
FR (1) | FR2547276B1 (it) |
GB (3) | GB2141086B (it) |
GR (1) | GR82108B (it) |
IL (1) | IL71604A (it) |
IT (1) | IT1208683B (it) |
NL (1) | NL8401854A (it) |
SE (1) | SE460282B (it) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4639730A (en) * | 1983-05-13 | 1987-01-27 | Sundstrand Data Control, Inc. | Excessive terrain closure warning system |
US5001476A (en) * | 1983-05-13 | 1991-03-19 | Sundstrand Data Control, Inc. | Warning system for tactical aircraft |
US4980684A (en) * | 1983-06-10 | 1990-12-25 | Sundstrand Data Controls, Inc. | Warning system for tactical rotary wing aircraft |
US4769645A (en) * | 1983-06-10 | 1988-09-06 | Sundstrand Data Control, Inc. | Excessive pitch attitude warning system for rotary wing aircraft |
CA1243119A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain warning system with configuration modified warning and improved mode switching |
CA1243118A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain closure warning system with descent rate based envelope modification |
US5187478A (en) * | 1985-02-22 | 1993-02-16 | Sundstrand Corporation | Configuration responsive descent rate warning system for aircraft |
CA1243405A (en) * | 1985-02-22 | 1988-10-18 | Michael M. Grove | Configuration responsive descent rate warning system for aircraft |
US4728951A (en) * | 1985-10-16 | 1988-03-01 | Honeywell Inc. | Vertical windshear detection for aircraft |
US4857923A (en) * | 1986-07-15 | 1989-08-15 | Sundstrand Data Control, Inc. | Ground proximity warning system for an excessive descent rate over undulating terrain |
US5260702A (en) * | 1989-12-27 | 1993-11-09 | Thompson Keith P | Aircraft information system |
US5406487A (en) * | 1991-10-11 | 1995-04-11 | Tanis; Peter G. | Aircraft altitude approach control device |
US5666110A (en) * | 1995-03-09 | 1997-09-09 | Paterson; Noel S. | Helicopter enhanced descent after take-off warning for GPWS |
US6043759A (en) * | 1996-07-29 | 2000-03-28 | Alliedsignal | Air-ground logic system and method for rotary wing aircraft |
US5781126A (en) * | 1996-07-29 | 1998-07-14 | Alliedsignal Inc. | Ground proximity warning system and methods for rotary wing aircraft |
US6012001A (en) * | 1997-12-30 | 2000-01-04 | Scully; Robert L. | Method and apparatus for determining aircraft-to-ground distances and descent rates during landing |
JP4551562B2 (ja) | 1998-10-16 | 2010-09-29 | ユニバーサル エイビーアニクス システムズ コーポレイション | 飛行計画目的警報システムおよび方法 |
US6833797B2 (en) | 2000-05-26 | 2004-12-21 | Honeywell International Inc. | Method, apparatus and computer program product for displaying terrain in rotary wing aircraft |
WO2002023125A1 (en) | 2000-09-14 | 2002-03-21 | Honeywell International Inc. | Method, apparatus and computer program product for helicopter tail strike warning |
US7126496B2 (en) * | 2004-09-30 | 2006-10-24 | Safe Flight Instrument Corporation | Tactile cueing system and method for aiding a helicopter pilot in making landings |
US7626514B2 (en) | 2006-06-23 | 2009-12-01 | Honeywell International Inc. | Systems and methods for reducing nuisance alerts for helicopter enhanced ground proximity warning systems |
US20080173753A1 (en) * | 2007-01-22 | 2008-07-24 | Honeywell International Inc. | Methods and systems for monitoring approach of rotary wing aircraft |
US8042765B1 (en) * | 2008-05-20 | 2011-10-25 | Nance C Kirk | Aircraft landing gear compression rate monitor |
US8116923B2 (en) * | 2009-11-19 | 2012-02-14 | Honeywell International | Stabilized approach monitor |
FR2956512B1 (fr) * | 2010-02-16 | 2012-03-09 | Airbus Operations Sas | Procede et dispositif de protection automatique d'un aeronef contre un taux de descente excessif. |
US9261883B2 (en) * | 2010-05-07 | 2016-02-16 | Honeywell International Inc. | Systems and methods for performing excessive negative pitch alert and for biasing a sink rate alert |
US9644990B2 (en) * | 2011-10-31 | 2017-05-09 | Honeywell International Inc. | Systems and methods for adjusting sink rate alert envelope for special landing zones |
US9051061B2 (en) * | 2012-12-14 | 2015-06-09 | Safe Flight Instrument Corporation | Systems and methods for safely landing an aircraft |
US9828113B2 (en) | 2013-11-05 | 2017-11-28 | Safe Flight Instrument Corporation | Tailstrike warning system |
US9546003B2 (en) | 2014-03-14 | 2017-01-17 | Safe Flight Instrument Corporation | Deflare pitch command |
US9346552B2 (en) | 2014-04-11 | 2016-05-24 | Safe Flight Instrument Corporation | Autothrottle retard control |
US20170008639A1 (en) | 2015-07-08 | 2017-01-12 | Safe Flight Instrument Corporation | Aircraft turbulence detection |
US10089634B2 (en) | 2015-10-27 | 2018-10-02 | C Kirk Nance | Method to recover non-recognized errors in aircraft weight determinations to increase weight and center of gravity limitations for regulated aircraft |
FR3063715B1 (fr) | 2017-03-09 | 2019-04-12 | Dassault Aviation | Systeme d'avertissement de proximite au sol d'un aeronef, avionique et procede associe |
WO2020072696A1 (en) * | 2018-10-02 | 2020-04-09 | Aviation Communication & Surveillance Systems, Llc | Systems and methods for providing a barometric altitude monitor |
US20230150690A1 (en) * | 2021-11-15 | 2023-05-18 | Honeywell International Inc. | Systems and methods for providing safe landing assistance for a vehicle |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3936796A (en) * | 1974-06-19 | 1976-02-03 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
US3946358A (en) * | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
US3958218A (en) * | 1974-10-03 | 1976-05-18 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning system with speed compensation |
US3947808A (en) * | 1975-01-13 | 1976-03-30 | Sundstrand Data Control, Inc. | Excessive descent rate warning system for aircraft |
US3947809A (en) * | 1975-01-13 | 1976-03-30 | Sundstrand Data Control, Inc. | Below glide slope advisory warning system for aircraft |
US3934221A (en) * | 1975-03-06 | 1976-01-20 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
US3958219A (en) * | 1975-03-06 | 1976-05-18 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
US4060793A (en) * | 1976-07-19 | 1977-11-29 | Sundstrand Data Control, Inc. | Excessive sink rate warning system for aircraft |
US4215334A (en) * | 1978-02-09 | 1980-07-29 | Sundstrand Data Control, Inc. | Aircraft excessive descent rate warning system |
IL57402A (en) * | 1978-09-20 | 1982-05-31 | Israel Aircraft Ind Ltd | Excessive descent-rate warning system |
IL55605A (en) * | 1978-09-20 | 1982-02-28 | Israel Aircraft Ind Ltd | Excessive descent-rate warning system |
US4319218A (en) * | 1980-01-04 | 1982-03-09 | Sundstrand Corporation | Negative climb after take-off warning system with configuration warning means |
-
1983
- 1983-06-10 US US06/503,218 patent/US4551723A/en not_active Expired - Lifetime
-
1984
- 1984-03-23 CA CA000450409A patent/CA1213013A/en not_active Expired
- 1984-04-20 IL IL71604A patent/IL71604A/xx unknown
- 1984-05-14 DE DE3417834A patent/DE3417834A1/de active Granted
- 1984-05-14 FI FI841929A patent/FI841929A/fi not_active Application Discontinuation
- 1984-05-21 GB GB08412950A patent/GB2141086B/en not_active Expired
- 1984-05-25 FR FR8408219A patent/FR2547276B1/fr not_active Expired
- 1984-05-30 AU AU28841/84A patent/AU548328B2/en not_active Ceased
- 1984-06-06 CH CH2754/84A patent/CH660157A5/fr not_active IP Right Cessation
- 1984-06-07 IT IT8448340A patent/IT1208683B/it active
- 1984-06-07 GR GR74950A patent/GR82108B/el unknown
- 1984-06-08 SE SE8403095A patent/SE460282B/sv not_active IP Right Cessation
- 1984-06-08 BE BE0/213112A patent/BE899878A/fr not_active IP Right Cessation
- 1984-06-08 JP JP59116817A patent/JPS608194A/ja active Pending
- 1984-06-12 NL NL8401854A patent/NL8401854A/nl not_active Application Discontinuation
- 1984-11-14 GB GB08428731A patent/GB2148823B/en not_active Expired
- 1984-11-14 GB GB08428730A patent/GB2148822B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2148823A (en) | 1985-06-05 |
CH660157A5 (fr) | 1987-03-31 |
GB2141086B (en) | 1986-12-31 |
NL8401854A (nl) | 1985-01-02 |
FR2547276B1 (fr) | 1988-10-14 |
FI841929A (fi) | 1984-12-11 |
GR82108B (it) | 1984-12-13 |
US4551723A (en) | 1985-11-05 |
FI841929A0 (fi) | 1984-05-14 |
GB2148822A (en) | 1985-06-05 |
AU548328B2 (en) | 1985-12-05 |
SE460282B (sv) | 1989-09-25 |
AU2884184A (en) | 1984-12-13 |
GB2141086A (en) | 1984-12-12 |
IL71604A (en) | 1990-04-29 |
GB8428730D0 (en) | 1984-12-27 |
CA1213013A (en) | 1986-10-21 |
GB8412950D0 (en) | 1984-06-27 |
SE8403095L (sv) | 1984-12-11 |
DE3417834C2 (it) | 1989-01-12 |
JPS608194A (ja) | 1985-01-17 |
IT1208683B (it) | 1989-07-10 |
DE3417834A1 (de) | 1984-12-13 |
GB8428731D0 (en) | 1984-12-27 |
GB2148823B (en) | 1986-12-10 |
SE8403095D0 (sv) | 1984-06-08 |
GB2148822B (en) | 1986-12-10 |
FR2547276A1 (fr) | 1984-12-14 |
BE899878A (fr) | 1984-12-10 |
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