ES480057A1 - Un dispositivo para indicar el angulo de incidencia del a- vion. - Google Patents
Un dispositivo para indicar el angulo de incidencia del a- vion.Info
- Publication number
- ES480057A1 ES480057A1 ES480057A ES480057A ES480057A1 ES 480057 A1 ES480057 A1 ES 480057A1 ES 480057 A ES480057 A ES 480057A ES 480057 A ES480057 A ES 480057A ES 480057 A1 ES480057 A1 ES 480057A1
- Authority
- ES
- Spain
- Prior art keywords
- airplane
- attack
- angle
- indicator
- flight
- 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.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P13/00—Indicating or recording presence, absence, or direction, of movement
- G01P13/02—Indicating direction only, e.g. by weather vane
- G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
- Navigation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
Abstract
Método y su correspondiente dispositivo para indicar el ángulo de incidencia del avión (10), caracterizado porque dicho dispositivo comprende un dispositivo accionado por el aire (46) que comunica con el aire al exterior del fusilaje y que responde al ángulo de incidencia del avión que se desplaza a través del aire, una fuente de luz (64) montada en dicho avión, una pluralidad de fibras ópticas (68) en dicho avión que tienen cada una una extremidad situada para estar sometida a dicha fuente de luz (64) un dispositivo de pantalla de luz (48) soportado por dicho avión de modo que pueda desplazarse entre dicha fuente de luz y dicha extremidad de dichas fibras ópticas (68) expuestas a dicha fuente de luz (64), un dispositivo (44) que conecta dicho dispositivo de pantalla de luz (48) y dicho dispositivo accionado por el aire (46) de tal manera que la disposición de dicho dispositivo de pantalla de luz (48) entre dicha fuente de luz y las fibras ópticas (68) responda a la posición de pivotamientode dicho dispositivo accionado por el aire (46), y un dispositivo indicador (80) en dicha zona del puesto de pilotaje que responde a la iluminación de dichas fibras ópticas.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/901,717 US4230290A (en) | 1978-05-01 | 1978-05-01 | Airplane angle of attack and direction of flight indicator |
Publications (1)
Publication Number | Publication Date |
---|---|
ES480057A1 true ES480057A1 (es) | 1980-08-16 |
Family
ID=25414700
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES480057A Expired ES480057A1 (es) | 1978-05-01 | 1979-04-27 | Un dispositivo para indicar el angulo de incidencia del a- vion. |
Country Status (14)
Country | Link |
---|---|
US (1) | US4230290A (es) |
JP (1) | JPS55500511A (es) |
AU (1) | AU530613B2 (es) |
BE (1) | BE875958A (es) |
CA (1) | CA1124370A (es) |
DE (1) | DE7912560U1 (es) |
ES (1) | ES480057A1 (es) |
FR (1) | FR2425054A1 (es) |
GB (1) | GB2036676B (es) |
IT (1) | IT1117446B (es) |
MX (1) | MX146287A (es) |
NO (1) | NO149421C (es) |
SE (1) | SE436189B (es) |
WO (1) | WO1979001009A1 (es) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4333704A (en) * | 1980-04-18 | 1982-06-08 | Hyman Steinberg | Solar alignment device |
US5220322A (en) * | 1984-07-18 | 1993-06-15 | Sundstrand Corporation | Ground proximity warning system for use with aircraft having egraded performance |
US4908619A (en) * | 1984-11-13 | 1990-03-13 | The Boeing Company | Aircraft stall warning system |
US4718273A (en) * | 1985-12-31 | 1988-01-12 | The Garrett Corporation | Combination alpha, static and total pressure probe |
US4968879A (en) * | 1988-07-29 | 1990-11-06 | The Boeing Company | Method and apparatus for measuring aircraft flight parameters |
DE8811776U1 (de) * | 1988-09-16 | 1988-12-29 | Siemens AG, 1000 Berlin und 8000 München | Datenübertragungsvorrichtung in Flugzeugen, insbesondere zur Triebwerksüberwachung |
US5025661A (en) * | 1989-12-11 | 1991-06-25 | Allied-Signal Inc. | Combination air data probe |
EP0447974B1 (fr) * | 1990-03-21 | 1994-07-20 | Karl Osen | Dispositif de mesure d'angle et utilisation de celui-ci |
US5115237A (en) * | 1990-04-16 | 1992-05-19 | Safe Flight Instrument Corporation | Combination aircraft yaw/angle of attack sensor |
US5225829A (en) * | 1991-05-09 | 1993-07-06 | Sundstrand Corporation | Independent low airspeed alert |
US5238208A (en) * | 1991-06-11 | 1993-08-24 | E-Systems, Inc. | Load mitigation system for a multi-dimensional transducer array |
US5590853A (en) * | 1992-02-03 | 1997-01-07 | Safe Flight Instrument Corporation | Aircraft control system |
US5299455A (en) * | 1992-03-27 | 1994-04-05 | Mangalam Siva M | Method and instrumentation system for measuring airspeed and flow angle |
US5753505A (en) * | 1995-07-06 | 1998-05-19 | Emory University | Neuronal progenitor cells and uses thereof |
US5852237A (en) * | 1997-05-28 | 1998-12-22 | Lockheed Martin Corporation | Apparatus and method for measuring the side slip of a low observable aircraft |
US6342846B1 (en) * | 1998-09-09 | 2002-01-29 | Argen Aviation, Inc. | Angle of attack detection and indication system |
US6131055A (en) * | 1998-12-11 | 2000-10-10 | The Boeing Company | Aircraft non-normalized angle-of-attack indicating system |
US6502459B1 (en) | 2000-09-01 | 2003-01-07 | Honeywell International Inc. | Microsensor for measuring velocity and angular direction of an incoming air stream |
US6609421B2 (en) * | 2001-05-08 | 2003-08-26 | Rosemount Aerospace Inc. | Sideslip correction for a multi-function three probe air data system |
US6702229B2 (en) * | 2001-08-08 | 2004-03-09 | Norman G. Anderson | Method, apparatus and article to display flight information |
US7395705B2 (en) * | 2006-06-21 | 2008-07-08 | Greene Leonard M | System for measuring an airflow angle at the wingtip of an aircraft |
JP5916283B2 (ja) * | 2010-07-01 | 2016-05-11 | 三菱重工業株式会社 | 表示装置、操縦支援システム、及び表示方法 |
SE536253C2 (sv) * | 2011-09-20 | 2013-07-16 | Bae Systems Bofors Ab | Metod och gnc-system för bestämning av anfallsvinkel |
CN104501702B (zh) * | 2015-01-16 | 2017-06-16 | 安徽江淮汽车集团股份有限公司 | 汽车接近角和离去角测量装置及测量、验证方法 |
US10457412B2 (en) * | 2016-09-16 | 2019-10-29 | Rosemount Aerospace Inc. | Electrical isolation of angle of attack vane bearings |
US10730637B2 (en) * | 2017-09-29 | 2020-08-04 | Rosemount Aerospace Inc. | Integral vane base angle of attack sensor |
US11181545B2 (en) | 2017-08-17 | 2021-11-23 | Rosemount Aerospace Inc. | Angle of attack sensor with thermal enhancement |
US10393766B2 (en) | 2017-08-17 | 2019-08-27 | Rosemount Aerospace Inc. | Water management system for angle of attack sensors |
US11162970B2 (en) | 2019-06-17 | 2021-11-02 | Rosemount Aerospace Inc. | Angle of attack sensor |
US11649057B2 (en) | 2019-12-13 | 2023-05-16 | Rosemount Aerospace Inc. | Static plate heating arrangement |
EP4111213A4 (en) * | 2020-02-25 | 2024-02-21 | Rosemount Aerospace Inc. | ANGLE OF ATTACK SENSOR WITH INCLINED FRONT PANEL |
US11577853B2 (en) | 2021-04-13 | 2023-02-14 | William M. Fisher | Aircraft angle of attack and sideslip angle indicator |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1332810A (en) * | 1917-02-03 | 1920-03-02 | Oscar A Danielson | Combined air-speed meter and angle of incidence and side slip indicator with dial therefor |
FR886791A (fr) * | 1941-09-16 | 1943-10-25 | Perfectionnements aux indicateurs d'incidence et de route pour les avions | |
US3036153A (en) * | 1960-09-02 | 1962-05-22 | Gulton Ind Inc | Electro-optical scanning system |
US3272174A (en) * | 1965-09-07 | 1966-09-13 | Gen Motors Corp | Remote level indication |
US3566826A (en) * | 1968-10-03 | 1971-03-02 | Lloyd M Forster | Aircraft drift meter |
US3475958A (en) * | 1968-12-09 | 1969-11-04 | Steve Sabadishin | Angle of attack indicator |
US3514997A (en) * | 1968-12-23 | 1970-06-02 | Teledyne Inc | Airstream direction detector |
US3677619A (en) * | 1970-04-20 | 1972-07-18 | Electro Mechanical Instr Co In | Readout devices with light conducting channels |
US3742233A (en) * | 1971-08-20 | 1973-06-26 | Dresser Ind | Motion displacement transducer |
US4139949A (en) * | 1977-07-13 | 1979-02-20 | Abraham Goldman | Compass having a fiber optic output |
-
1978
- 1978-05-01 US US05/901,717 patent/US4230290A/en not_active Expired - Lifetime
-
1979
- 1979-04-18 JP JP50073679A patent/JPS55500511A/ja active Pending
- 1979-04-18 CA CA325,679A patent/CA1124370A/en not_active Expired
- 1979-04-18 WO PCT/US1979/000249 patent/WO1979001009A1/en unknown
- 1979-04-18 GB GB7932439A patent/GB2036676B/en not_active Expired
- 1979-04-23 AU AU46279/79A patent/AU530613B2/en not_active Ceased
- 1979-04-26 NO NO791388A patent/NO149421C/no unknown
- 1979-04-27 ES ES480057A patent/ES480057A1/es not_active Expired
- 1979-04-27 FR FR7910770A patent/FR2425054A1/fr active Granted
- 1979-04-27 IT IT48877/79A patent/IT1117446B/it active
- 1979-04-30 DE DE19797912560U patent/DE7912560U1/de not_active Expired
- 1979-04-30 MX MX177488A patent/MX146287A/es unknown
- 1979-04-30 BE BE0/194919A patent/BE875958A/xx not_active IP Right Cessation
- 1979-10-30 SE SE7908981A patent/SE436189B/sv unknown
Also Published As
Publication number | Publication date |
---|---|
DE7912560U1 (de) | 1980-02-14 |
FR2425054A1 (fr) | 1979-11-30 |
SE7908981L (sv) | 1979-11-02 |
US4230290A (en) | 1980-10-28 |
CA1124370A (en) | 1982-05-25 |
GB2036676A (en) | 1980-07-02 |
FR2425054B1 (es) | 1985-05-17 |
JPS55500511A (es) | 1980-08-14 |
AU530613B2 (en) | 1983-07-21 |
NO791388L (no) | 1979-11-02 |
SE436189B (sv) | 1984-11-19 |
NO149421C (no) | 1984-04-25 |
NO149421B (no) | 1984-01-09 |
IT7948877A0 (it) | 1979-04-27 |
IT1117446B (it) | 1986-02-17 |
BE875958A (fr) | 1979-08-16 |
GB2036676B (en) | 1982-11-17 |
MX146287A (es) | 1982-06-02 |
WO1979001009A1 (en) | 1979-11-29 |
AU4627979A (en) | 1979-11-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 20001204 |