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
aircraft
light source
optical fibers
air
angle
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
Application number
ES480057A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Marel Inc
Original Assignee
Marel Meat Processing Inc
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 Marel Meat Processing Inc filed Critical Marel Meat Processing Inc
Publication of ES480057A1 publication Critical patent/ES480057A1/es
Expired legal-status Critical Current

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)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (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.
ES480057A 1978-05-01 1979-04-27 Un dispositivo para indicar el angulo de incidencia del a- vion. Expired ES480057A1 (es)

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)

* Cited by examiner, † Cited by third party
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
DE69102914T2 (de) * 1990-03-21 1995-03-16 Karl Osen Winkelmesseinrichtung und Verwendung derselben.
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
US10393766B2 (en) 2017-08-17 2019-08-27 Rosemount Aerospace Inc. Water management system for angle of attack sensors
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
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
US12360134B2 (en) 2020-02-25 2025-07-15 Rosemount Aerospace Inc. Angle of attack sensor with sloped faceplate
US11577853B2 (en) 2021-04-13 2023-02-14 William M. Fisher Aircraft angle of attack and sideslip angle indicator

Family Cites Families (10)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
FR2425054B1 (es) 1985-05-17
SE436189B (sv) 1984-11-19
IT7948877A0 (it) 1979-04-27
GB2036676B (en) 1982-11-17
NO149421B (no) 1984-01-09
NO791388L (no) 1979-11-02
CA1124370A (en) 1982-05-25
AU4627979A (en) 1979-11-08
WO1979001009A1 (en) 1979-11-29
AU530613B2 (en) 1983-07-21
SE7908981L (sv) 1979-11-02
MX146287A (es) 1982-06-02
DE7912560U1 (de) 1980-02-14
FR2425054A1 (fr) 1979-11-30
JPS55500511A (es) 1980-08-14
NO149421C (no) 1984-04-25
GB2036676A (en) 1980-07-02
IT1117446B (it) 1986-02-17
BE875958A (fr) 1979-08-16
US4230290A (en) 1980-10-28

Similar Documents

Publication Publication Date Title
ES480057A1 (es) Un dispositivo para indicar el angulo de incidencia del a- vion.
US3303807A (en) Helicopter rapid securing device
KR880007323A (ko) 태양광 수집 비행체
ES2127382T3 (es) Avion de ala libre stol-vtol con larguero de cola articulado.
GB1356886A (en) Optical devices
JPS5531944A (en) Surface stress measuring unit for wind cooled tempered glass
ES2044918T3 (es) Metodo y apparato para dirigir el vuelo de un avion en cortante del viento.
US3349234A (en) Illuminating apparatus
ES2036700T3 (es) Dispositivo de visualizacion en pantalla plana con presentacion visual de las informaciones bajo mando del operador.
US2738491A (en) Projected warning signal device for airplanes
ATE70237T1 (de) Flugzeug.
GB1477965A (en) Device for determining the state of the atmosphere at aero dromes from measurements of the optical transmission or reflection properties of the atmosphere
ES2059091T3 (es) Mecanismo de mando del movimiento de los marcos de garras de un dispositivo de formacion de la calada.
US1498023A (en) Method of and means for aerodynamic testing
FR2377936A1 (fr) Systeme d'eclairement d'un girodyne en vol de nuit
CN207670674U (zh) 一种小型无人机空速测量与安全开关一体化装置
ES178645A1 (es) Perfeccionamientos en la construccion de aviones
GB526775A (en) Improvements in or relating to aircraft-stabilizing devices
CN208530870U (zh) 一种飞机轮胎防尘帽取出装置
MERKEL et al. An illustrated guide of optical characteristics of aircraft transparencies(Final Report, Feb. 1988- Feb. 1989)
CN120986715A (zh) 一种无人机用升降式双层设备安装架
SU541328A1 (ru) Система управления летательным аппаратом вертикального взлета и посадки
GB609153A (en) Landing and emergency device for heavier-than-air craft
ES2068007T3 (es) Un dispositivo anticongelante para un ala de avion.
Weick Full Scale Drag Tests on Various Parts of Sperry Messenger Airplane

Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20001204