BRPI0801285A2 - sonda para uma aeronave e mÉtodo para isolar tÉrmicamente pelo menos uma linha pneumÁtica em uma sonda de uma aeronave - Google Patents

sonda para uma aeronave e mÉtodo para isolar tÉrmicamente pelo menos uma linha pneumÁtica em uma sonda de uma aeronave

Info

Publication number
BRPI0801285A2
BRPI0801285A2 BRPI0801285-7A BRPI0801285A BRPI0801285A2 BR PI0801285 A2 BRPI0801285 A2 BR PI0801285A2 BR PI0801285 A BRPI0801285 A BR PI0801285A BR PI0801285 A2 BRPI0801285 A2 BR PI0801285A2
Authority
BR
Brazil
Prior art keywords
probe
aircraft
manifold
pneumatic line
pneumatic
Prior art date
Application number
BRPI0801285-7A
Other languages
English (en)
Inventor
Scott Joseph Braun
Patrick John Moynihan
Timothy Thomas Golly
Alexander Nathan Reid
Original Assignee
Rosemount Aerospace 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 Rosemount Aerospace Inc filed Critical Rosemount Aerospace Inc
Publication of BRPI0801285A2 publication Critical patent/BRPI0801285A2/pt
Publication of BRPI0801285B1 publication Critical patent/BRPI0801285B1/pt

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/165—Arrangements or constructions of Pitot tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Fluid Pressure (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Multi-Conductor Connections (AREA)

Abstract

SONDA PARA UMA AERONAVE E MÉTODO PARA ISOLAR TÉRMICAMENTE PELO MENOS UMA LINHA PNEUMÁTICA EM UMA SONDA DE UMA AERONAVE. A invenção apresenta uma sonda para uma aeronave que inclui um suporte que tem uma passagem interior para acomodar uma pluralidade de linhas pneumáticas, uma cabeça de sonda que se estende do suporte e tem pelo menos uma abertura de entrada que se comunica com as linhas pneumáticas, uma placa base situada abaixo do suporte para unir a sonda à aeronave, e um distribuidor situado abaixo da placa base para se comunicar com as linhas pneumáticas, em que a placa base é adaptada e configurada de modo que as linhas pneumáticas que se comunicam com o distribuidor sejam isoladas termicamente da placa base. A invenção também apresenta um método para isolar termicamente pelo menos uma linha pneumática em uma sonda de uma aeronave.
BRPI0801285-7A 2007-04-11 2008-04-01 Sonda para uma aeronave e método para isolar térmicamente pelo menos uma linha pneumática em uma sonda de uma aeronave BRPI0801285B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/786,225 2007-04-11
US11/786,225 US7597018B2 (en) 2007-04-11 2007-04-11 Pneumatic line isolation and heating for air data probes

Publications (2)

Publication Number Publication Date
BRPI0801285A2 true BRPI0801285A2 (pt) 2008-11-25
BRPI0801285B1 BRPI0801285B1 (pt) 2019-05-14

Family

ID=39642663

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0801285-7A BRPI0801285B1 (pt) 2007-04-11 2008-04-01 Sonda para uma aeronave e método para isolar térmicamente pelo menos uma linha pneumática em uma sonda de uma aeronave

Country Status (4)

Country Link
US (1) US7597018B2 (pt)
EP (1) EP1980860B1 (pt)
BR (1) BRPI0801285B1 (pt)
CA (1) CA2622133C (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070174429A1 (en) 2006-01-24 2007-07-26 Citrix Systems, Inc. Methods and servers for establishing a connection between a client system and a virtual machine hosting a requested computing environment
FR2924498B1 (fr) * 2007-11-30 2009-12-11 Thales Sa Girouette de mesure de l'orientation du vent a rechauffeur integre
ES2394558B1 (es) * 2010-01-18 2013-12-12 Eads Construcciones Aeronáuticas, S.A. Dispositivo de soporte para sonda.
WO2013028220A1 (en) * 2011-08-19 2013-02-28 Aerovironment Inc. Water resisitant aircraft pitot device
US8857255B2 (en) * 2012-08-22 2014-10-14 Rosemount Aerospace Inc. Moisture resistant air data probes
US9174743B2 (en) * 2013-05-10 2015-11-03 Serias Design LLC Protective cover for aircraft pitot probes
GB201503138D0 (en) 2015-02-25 2015-04-08 Rolls Royce Controls & Data Services Ltd Icing prevention of a pressure sensing assembly
US11209330B2 (en) 2015-03-23 2021-12-28 Rosemount Aerospace Inc. Corrosion resistant sleeve for an air data probe
US9841304B2 (en) * 2015-04-17 2017-12-12 Rosemount Aerospace Inc. Air data system
US9909905B2 (en) 2015-10-15 2018-03-06 Honeywell International Inc. Multi-part air data probe assembly to facilitate rapid replacement
US10472072B2 (en) * 2015-11-25 2019-11-12 Hamilton Sundstrand Corporation Supply tube for sensor
US9758257B1 (en) * 2016-04-07 2017-09-12 Sunlight Photonics Inc. Airflow sensing systems and apparatus
US10384787B2 (en) 2016-06-23 2019-08-20 Honeywell International Inc. Forming an air data probe from a porous cover and brazing material
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
US10730637B2 (en) * 2017-09-29 2020-08-04 Rosemount Aerospace Inc. Integral vane base angle of attack sensor
US20190104568A1 (en) * 2017-09-29 2019-04-04 Rosemount Aerospace Inc. Self-regulating heater compensation
US10613112B2 (en) * 2018-01-19 2020-04-07 Rosemount Aerospace Inc. Air data probe assembly method
US10716171B2 (en) 2018-03-23 2020-07-14 Rosemount Aerospace Inc. Power efficient heater control of air data sensor
US11414195B2 (en) 2018-03-23 2022-08-16 Rosemount Aerospace Inc. Surface modified heater assembly
US10876858B2 (en) * 2018-06-15 2020-12-29 Rosemount Aerospace Inc. Method and device for leak check of air data system
US11002754B2 (en) 2018-11-06 2021-05-11 Rosemount Aerospace Inc. Pitot probe with mandrel and pressure swaged outer shell
US10884014B2 (en) 2019-03-25 2021-01-05 Rosemount Aerospace Inc. Air data probe with fully-encapsulated heater
US11486785B2 (en) 2019-03-28 2022-11-01 Rosemount Aerospace Inc. Thermal management system for air data sensor module
US11428707B2 (en) 2019-06-14 2022-08-30 Rosemount Aerospace Inc. Air data probe with weld sealed insert
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
FR3123723B1 (fr) * 2021-06-07 2023-04-21 Thales Sa Sonde de mesure de pression comprenant une carte capteur de pression
US11624637B1 (en) 2021-10-01 2023-04-11 Rosemount Aerospace Inc Air data probe with integrated heater bore and features
US11662235B2 (en) 2021-10-01 2023-05-30 Rosemount Aerospace Inc. Air data probe with enhanced conduction integrated heater bore and features
US12409939B2 (en) * 2022-07-11 2025-09-09 Rosemount Aerospace Inc. Air data probe electronics housing with thermal isolating features

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2221547A (en) * 1938-03-12 1940-11-12 Square D Co Heat protected pitot-static tube
GB541684A (en) * 1940-05-03 1941-12-08 Smith & Sons Ltd S Improvements in pneumatic pressure heads
US3585859A (en) * 1969-05-26 1971-06-22 Rosemount Eng Co Ltd Aerodynamically compensated static pressure tube
US4378696A (en) 1981-02-23 1983-04-05 Rosemount Inc. Pressure sensor for determining airspeed altitude and angle of attack
US5025661A (en) * 1989-12-11 1991-06-25 Allied-Signal Inc. Combination air data probe
JP2954349B2 (ja) * 1991-03-22 1999-09-27 ローズマウント インコーポレイテッド 連続曲面支柱で支持されたセンサ
US5458008A (en) * 1993-12-10 1995-10-17 The B.F. Goodrich Company Condensation and evaporation system for air data sensor system
US5601254A (en) * 1994-10-28 1997-02-11 Rosemount Aerospace Inc. Single sided backbone strut for air data sensor
US5543183A (en) * 1995-02-17 1996-08-06 General Atomics Chromium surface treatment of nickel-based substrates
US5653538A (en) * 1995-06-07 1997-08-05 Rosemount Aerospace Inc. Total temperature probe
JP2001505659A (ja) * 1996-10-16 2001-04-24 ローズマウント・エアロスペース・インコーポレーテッド 加熱式空気データプローブ
US6012331A (en) 1998-07-02 2000-01-11 Avionics Specialties, Inc. Multifunction aircraft probes
US6076963A (en) 1998-10-20 2000-06-20 Avionics Specialties, Inc. Aircraft probe with integral air temperature sensor
US6305218B1 (en) * 1999-02-22 2001-10-23 Rosemount Aerospace Inc. Method of and apparatus for using an alternate pressure to measure mach number at high probe angles of attack
US6557243B2 (en) * 2001-04-27 2003-05-06 Christopher M. Feeley Method to repair a permanently sealed air data tube
US6550344B2 (en) * 2001-05-04 2003-04-22 Rosemount Aerospace Inc. Semi-flush air data sensor
US6591696B2 (en) * 2001-07-12 2003-07-15 Rosemount Aerospace, Inc. Integral electric pressure probe for aircraft
US6622390B2 (en) * 2001-08-29 2003-09-23 Rosemount Aerospace Inc. Method and apparatus for installation and alignment of air data sensing probe
US6668640B1 (en) 2002-08-12 2003-12-30 Rosemount Aerospace Inc. Dual-channel electronic multi-function probes and methods for realizing dissimilar and independent air data outputs
US6892584B2 (en) * 2002-11-19 2005-05-17 Rosemount Aerospace Inc. Fabricated pitot probe assembly
US6941805B2 (en) * 2003-06-26 2005-09-13 Rosemount Aerospace Inc. Multi-function air data sensing probe having an angle of attack vane
US6974250B2 (en) * 2004-04-15 2005-12-13 Rosemount Aerospace Inc. Temperature sensor with controlled thermal offset for determining static temperature

Also Published As

Publication number Publication date
EP1980860B1 (en) 2011-11-16
BRPI0801285B1 (pt) 2019-05-14
EP1980860A3 (en) 2009-12-30
US20080250884A1 (en) 2008-10-16
US7597018B2 (en) 2009-10-06
EP1980860A2 (en) 2008-10-15
CA2622133C (en) 2013-01-08
CA2622133A1 (en) 2008-10-11

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B06A Notification to applicant to reply to the report for non-patentability or inadequacy of the application [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 14/05/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 14/05/2019, OBSERVADAS AS CONDICOES LEGAIS