BR0100086A - Bico de velame de aeronave, velame de aeronave, e, aeronave - Google Patents

Bico de velame de aeronave, velame de aeronave, e, aeronave

Info

Publication number
BR0100086A
BR0100086A BR0100086-1A BR0100086A BR0100086A BR 0100086 A BR0100086 A BR 0100086A BR 0100086 A BR0100086 A BR 0100086A BR 0100086 A BR0100086 A BR 0100086A
Authority
BR
Brazil
Prior art keywords
aircraft
nozzle
canopy
hot air
velame
Prior art date
Application number
BR0100086-1A
Other languages
English (en)
Other versions
BR0100086B1 (pt
Inventor
Paul Laugt
Original Assignee
Dassault Aviat
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 Dassault Aviat filed Critical Dassault Aviat
Publication of BR0100086A publication Critical patent/BR0100086A/pt
Publication of BR0100086B1 publication Critical patent/BR0100086B1/pt

Links

Classifications

    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Drying Of Solid Materials (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
  • Cold Air Circulating Systems And Constructional Details In Refrigerators (AREA)

Abstract

"BICO DE VELAME DE AERONAVE, VELAME DE AERONAVE, E, AERONAVE". Esse bico (1a) de velame (V) de aeronave compreende uma parede externa (5a) e um dispositivo de anticongelamento do tipo que permite fazer circular ar quente de acordo com a direção da envergadura do dito velame. Esse dispositivo compreende a) um conduto de distribuição de ar quente (15a) que se estende no interior do dito bico de acordo com a dita direção e que possui uma pluralidade de orifícios (25a) distribuídos em pelo menos uma parte de seu comprimento, e b) meios de alimentação com ar quente (19a) que se comunicam com uma (17a) das extremidades do dito conduto de distribuiçãio (15a; 15b). Esses meios de alimentação com ar quente (19a) são adaptados para ser ligados por condutos (C) situados no exterior do dito bico a pelo menos um motor (M) de propulsão da dita aeronave.
BRPI0100086-1A 2000-01-17 2001-01-16 bordo de ataque de asa de aeronave dotado de sistema de degelo integrado. BR0100086B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0000525A FR2803821B1 (fr) 2000-01-17 2000-01-17 Bec de voilure d'aeronef equipe d'un dispositif d'antigivrage, voilure equipee d'un tel bec, et aeronef equipe d'une telle voilure

Publications (2)

Publication Number Publication Date
BR0100086A true BR0100086A (pt) 2001-08-28
BR0100086B1 BR0100086B1 (pt) 2009-01-13

Family

ID=8845970

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0100086-1A BR0100086B1 (pt) 2000-01-17 2001-01-16 bordo de ataque de asa de aeronave dotado de sistema de degelo integrado.

Country Status (7)

Country Link
US (1) US6467730B2 (pt)
EP (1) EP1116656B1 (pt)
BR (1) BR0100086B1 (pt)
CA (1) CA2330397C (pt)
DE (1) DE60102840T2 (pt)
FR (1) FR2803821B1 (pt)
IL (1) IL140885A (pt)

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AU2001249862A1 (en) * 2000-04-05 2001-10-23 Bell Helicopter Textron Inc. K-spar configuration for bonded wing construction
US7178760B2 (en) 2003-05-30 2007-02-20 Bombardier Aéronautique Method and apparatus for inhibiting accretion of airborne material on a surface of an aircraft
US7331421B2 (en) * 2005-03-30 2008-02-19 The Boeing Company Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods
US20070080481A1 (en) * 2005-10-12 2007-04-12 The Boeing Company Apparatus and methods for fabrication of composite components
US7157663B1 (en) 2005-10-12 2007-01-02 The Boeing Company Conducting-fiber deicing systems and methods
GB2440133A (en) * 2006-07-18 2008-01-23 Gkn Aerospace Transparency Sys A de-icing heated leading edge component of an aircraft
US7980515B2 (en) * 2006-08-25 2011-07-19 0832042 B.C. Ltd. Aircraft wing modification and related methods
US8052089B2 (en) * 2008-11-03 2011-11-08 The Boeing Company Anti-icing apparatus for honeycomb structures
US8061657B2 (en) * 2008-12-31 2011-11-22 General Electric Company Method and apparatus for aircraft anti-icing
US8100364B2 (en) * 2009-01-15 2012-01-24 Textron Innovations Inc. Anti-icing piccolo tube standoff
FR2954279B1 (fr) * 2009-12-18 2014-08-22 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises
JP2011183922A (ja) * 2010-03-08 2011-09-22 Mitsubishi Heavy Ind Ltd 航空機における翼前縁部の防除氷装置及び航空機主翼
DE102012002132A1 (de) 2012-02-03 2013-08-08 Airbus Operations Gmbh Vereisungsschutzsystem für ein Flugzeug und Verfahren zum Betreiben eines Vereisungsschutzsystems
JP6193691B2 (ja) * 2013-09-11 2017-09-06 三菱航空機株式会社 防氷システム、及び、航空機
US9896190B1 (en) * 2014-05-07 2018-02-20 The Boeing Company Wing leading edge architecture suitable for laminar flow
US10393020B2 (en) * 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US9815558B2 (en) 2015-12-09 2017-11-14 King Fahd University Of Petroleum And Minerals Anti-icing apparatus and system
JP6666159B2 (ja) * 2016-01-21 2020-03-13 三菱航空機株式会社 防氷装置、及び、航空機
JP2017136893A (ja) * 2016-02-01 2017-08-10 三菱航空機株式会社 防氷装置、及び、航空機
JP6839920B2 (ja) * 2016-02-12 2021-03-10 三菱航空機株式会社 防氷装置、及び、航空機
WO2018005529A1 (en) * 2016-06-29 2018-01-04 Bombardier Inc. Temperature monitoring unit for aircraft wing structure and associated installation method
GB201710385D0 (en) * 2017-06-29 2017-08-16 Airbus Operations Gmbh Aerofoil structure and method of assembly
CN107905961B (zh) * 2017-11-09 2019-12-20 新疆金风科技股份有限公司 叶片的加热除冰系统及其方法、叶片和风力发电机组
ES2943266T3 (es) * 2017-12-28 2023-06-12 Airbus Operations Gmbh Estructura de borde de ataque para un sistema de control de flujo de una aeronave
US20190359341A1 (en) * 2018-05-25 2019-11-28 The Boeing Company Method of thermal ice protection for an aircraft wing
US11440665B2 (en) 2018-10-23 2022-09-13 Airbus Operations Gmbh Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly
US11286034B2 (en) 2018-11-22 2022-03-29 Airbus Operations Gmbh Leading-edge slat for an aircraft
EP3683140B1 (en) 2019-01-18 2022-10-12 Asco Industries NV Slat for an aircraft wing, method for manufacturing such a slat
US20210024221A1 (en) * 2019-07-25 2021-01-28 Airbus Operations Sas Leading edge member for an airfoil of an aircraft
BE1028506B1 (fr) * 2020-12-24 2022-02-11 Sonaca Sa Système pour aeronef de protection contre le givre par air chaud souffle a penalite energetique reduite
EP4331992A1 (en) * 2022-09-02 2024-03-06 Rohr, Inc. Thermal anti-icing system for an aircraft propulsion system

Family Cites Families (14)

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Publication number Priority date Publication date Assignee Title
US2320870A (en) * 1940-09-20 1943-06-01 Lockheed Aircraft Corp Anti-icing duct
FR979460A (fr) * 1942-05-07 1951-04-26 Dispositif du dégivrage par réchauffage du bord d'attaque des ailes
US2556736A (en) * 1945-06-22 1951-06-12 Curtiss Wright Corp Deicing system for aircraft
US2581760A (en) * 1946-04-02 1952-01-08 Douglas Aircraft Co Inc Airplane deicing construction
US2470128A (en) * 1947-10-07 1949-05-17 Glenn L Martin Co Airplane wing leading edge construction
GB1032681A (en) * 1961-05-12 1966-06-15 Napier & Son Ltd Ice protection systems for aerofoil surfaces
US4099691A (en) * 1976-12-13 1978-07-11 The Boeing Company Boundary layer control system for aircraft
US4615499A (en) * 1983-08-12 1986-10-07 The Boeing Company Wing slat anti-ice air duct system
US4741499A (en) * 1984-12-31 1988-05-03 The Boeing Company Anti-icing system for aircraft
US4752049A (en) * 1985-12-30 1988-06-21 The Boeing Company Leading edge slat/anti-icing system and method for airfoil
US4688745A (en) * 1986-01-24 1987-08-25 Rohr Industries, Inc. Swirl anti-ice system
US5088277A (en) * 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US5807454A (en) * 1995-09-05 1998-09-15 Honda Giken Kogyo Kabushiki Kaisha Method of maufacturing a leading edge structure for aircraft

Also Published As

Publication number Publication date
US6467730B2 (en) 2002-10-22
BR0100086B1 (pt) 2009-01-13
FR2803821A1 (fr) 2001-07-20
IL140885A0 (en) 2002-02-10
EP1116656A1 (fr) 2001-07-18
US20010023909A1 (en) 2001-09-27
IL140885A (en) 2004-01-04
CA2330397A1 (en) 2001-07-17
FR2803821B1 (fr) 2002-04-05
DE60102840T2 (de) 2005-04-28
DE60102840D1 (de) 2004-05-27
EP1116656B1 (fr) 2004-04-21
CA2330397C (en) 2008-10-28

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B15K Others concerning applications: alteration of classification

Free format text: ALTERADA DA INT.CL.7.: B64C 9/04.

Ipc: B64C 3/28 (2008.04), B64D 15/04 (2008.04)

B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 16/01/2001, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time
B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)