BR112018077334A2 - Intuitive angle of attack guidance display on aircraft attitude indicator - Google Patents

Intuitive angle of attack guidance display on aircraft attitude indicator

Info

Publication number
BR112018077334A2
BR112018077334A2 BR112018077334A BR112018077334A BR112018077334A2 BR 112018077334 A2 BR112018077334 A2 BR 112018077334A2 BR 112018077334 A BR112018077334 A BR 112018077334A BR 112018077334 A BR112018077334 A BR 112018077334A BR 112018077334 A2 BR112018077334 A2 BR 112018077334A2
Authority
BR
Brazil
Prior art keywords
angle
display
attack
guidance display
stall
Prior art date
Application number
BR112018077334A
Other languages
Portuguese (pt)
Inventor
Watson Gary
Original Assignee
L 3 Tech Avionic Products
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 L 3 Tech Avionic Products filed Critical L 3 Tech Avionic Products
Publication of BR112018077334A2 publication Critical patent/BR112018077334A2/en

Links

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
    • B64D43/00—Arrangements or adaptations of instruments
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00—Indicating measured values
    • G01D7/02—Indicating value of two or more variables simultaneously
    • G01D7/08—Indicating value of two or more variables simultaneously using a common indicating element for two or more variables
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D2207/00—Indexing scheme relating to details of indicating measuring values
    • G01D2207/10—Displays which are primarily used in aircraft or display aircraft-specific information

Abstract

trata-se de um sistema aviônico de aeronave para uso em uma aeronave equipada que inclui um controlador e um visor. o controlador fornece dados de saída para o visor, sendo que os dados de saída produzem imagens visuais no visor. uma fonte de dados de ângulo de ataque fornece dados de ângulo de ataque atuais para a aeronave equipada. o controlador é responsivo aos dados de ângulo de ataque a fim de fornecer os dados de saída para acionar o visor para mostrar uma direção de controle necessária para impedir um estol. a exibição de direção de controle necessária é graduada com base em um nível atual de iminência de estol. a iminência de estol é uma função do ângulo de ataque da aeronave equipada.It is an avionic aircraft system for use in an equipped aircraft that includes a controller and a display. The controller provides output data to the display, and the output data produces visual images on the display. An angle of attack data source provides current angle of attack data for the equipped aircraft. The controller is responsive to the angle of attack data to provide the output data to trigger the display to show a control direction needed to prevent a stall. The required control direction display is scaled based on a current stall imminence level. Stall imminence is a function of the angle of attack of the equipped aircraft.

BR112018077334A 2016-06-29 2017-06-29 Intuitive angle of attack guidance display on aircraft attitude indicator BR112018077334A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201662356118P 2016-06-29 2016-06-29
PCT/IB2017/053928 WO2018002878A1 (en) 2016-06-29 2017-06-29 Intuitive display of angle of attack guidance on aircraft attitude indicator

Publications (1)

Publication Number Publication Date
BR112018077334A2 true BR112018077334A2 (en) 2019-04-02

Family

ID=60786169

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112018077334A BR112018077334A2 (en) 2016-06-29 2017-06-29 Intuitive angle of attack guidance display on aircraft attitude indicator

Country Status (4)

Country Link
EP (1) EP3478582A1 (en)
BR (1) BR112018077334A2 (en)
CA (1) CA3029131A1 (en)
WO (1) WO2018002878A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111060709B (en) * 2019-12-06 2021-10-15 江西洪都航空工业集团有限责任公司 Speed vector indicator driving method for unmanned aerial vehicle human-in-loop head-up display
US11830370B2 (en) 2021-08-25 2023-11-28 Honeywell International Inc. Methods, systems, and apparatuses for computation and annunciation of Mach tuck

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5979586A (en) * 1997-02-05 1999-11-09 Automotive Systems Laboratory, Inc. Vehicle collision warning system
US6131055A (en) * 1998-12-11 2000-10-10 The Boeing Company Aircraft non-normalized angle-of-attack indicating system
AU6488400A (en) * 1999-04-01 2000-11-10 Ricardo A. Price Electronic flight instrument displays
US8184020B2 (en) * 2009-07-29 2012-05-22 Honeywell International Inc. Method and system displaying a flight path to intercept an ILS glide path
JP5916283B2 (en) * 2010-07-01 2016-05-11 三菱重工業株式会社 Display device, steering support system, and display method
US9221550B2 (en) * 2013-03-12 2015-12-29 Geoffrey S. M. Hedrick Composite normalized angle of attack indicating system
US9193473B2 (en) * 2013-09-20 2015-11-24 Safe Flight Instrument Corporation Angle of attack display

Also Published As

Publication number Publication date
CA3029131A1 (en) 2018-01-04
EP3478582A1 (en) 2019-05-08
WO2018002878A1 (en) 2018-01-04

Similar Documents

Publication Publication Date Title
BR112017014574A2 (en) target path generation device and driving control device
BR112016014491A2 (en) DEVICE AND CONTROL METHOD, AND COMPUTER PROGRAM
BR112017003476A2 (en) cross device application discovery and control
BR112013029847A2 (en) tilt-based flight speed symbology and unreliable primary flight display power
ES2632259T3 (en) System to provide warning of overcoming on landing and avoidance.
BR112014005656A2 (en) system with a contactless user interface; control software in a computer readable medium; method for allowing a user to control a system's functionality through non-contact interaction with the system; and user interface
BR112018074293A2 (en) System and control method for a dynamic system and wind turbine park
BR112017022775A2 (en) occlusion control device
BR112017006388A2 (en) welding torch display system and method
BR102013016640A2 (en) flight control system, non-transient computer readable storage media and aircraft
BR112017021458A2 (en) System and method for indicating angle of attack without dedicated sensors and aircraft information
EP4309613A3 (en) Navigation systems for indicating line-of-sight errors
BR112014026898A2 (en) aircraft collision avoidance method, and drone provided with a system to implement the above mentioned method
BR112019000597A2 (en) displacement control method and displacement control apparatus
BR112016024955A2 (en) information display apparatus and information display method
BR112017019353A2 (en) dynamic positioning shutdown mitigation (dp) with inertial navigation system
BR112015012539A2 (en) display device and control method
BR112016014819A2 (en) MOMENT CONTROL GYROSCOPE ASSEMBLY INCLUDING MULTIPLE MOMENT CONTROL GYROSCOPES, ATTITUDE CONTROL UNIT, ATTITUDE CONTROL SYSTEM AND SPACE PLATFORM
BR112016017406A2 (en) METHOD AND DEVICE FOR DETERMINING AN ENVIRONMENTAL MODEL OF N+1 DIMENSION AND PROSPECTING APPARATUS
BR112016004258A2 (en) PROXIMITY DETECTION SYSTEMS AND METHODS
BR112018077334A2 (en) Intuitive angle of attack guidance display on aircraft attitude indicator
BR112017005763A2 (en) remote power supply parameter setting
BR112017003416A2 (en) custom contextual menu for inserting content into a current application
BR112017016025A2 (en) aircraft component positioning device, aircraft assembly system and aircraft assembly method
BR112017000731A2 (en) direct access application representations

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 3A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2594 DE 24-09-2020 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]