FR3076859B1 - DETACHABLE THERMAL INSULATION GASKET - Google Patents

DETACHABLE THERMAL INSULATION GASKET Download PDF

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Publication number
FR3076859B1
FR3076859B1 FR1871891A FR1871891A FR3076859B1 FR 3076859 B1 FR3076859 B1 FR 3076859B1 FR 1871891 A FR1871891 A FR 1871891A FR 1871891 A FR1871891 A FR 1871891A FR 3076859 B1 FR3076859 B1 FR 3076859B1
Authority
FR
France
Prior art keywords
panel
latch
panels
motor
thermal insulation
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 - Fee Related
Application number
FR1871891A
Other languages
French (fr)
Other versions
FR3076859A1 (en
Inventor
Pretty Michael Sean
Stephen M Erickson
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.)
Rohr Inc
Original Assignee
Rohr 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 Rohr Inc filed Critical Rohr Inc
Priority to FR1871891A priority Critical patent/FR3076859B1/en
Publication of FR3076859A1 publication Critical patent/FR3076859A1/en
Application granted granted Critical
Publication of FR3076859B1 publication Critical patent/FR3076859B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24Heat or noise insulation
    • F02C7/25Fire protection or prevention
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/08Inspection panels for power plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • F01D25/14Casings modified therefor
    • F01D25/145Thermally insulated casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/72Maintenance

Abstract

Un système de propulsion (110), comprenant : un turboréacteur (140) ; un premier panneau (131A) et un deuxième panneaux (131B) adaptés pour être amovibles entre une position ouverte dans laquelle l’accès au moteur (140) est permis pendant l’entretien et une position fermée dans laquelle le premier et le deuxième panneau (131A, 131B) entourent et renferment sensiblement au moins une partie du moteur (140) ; une première moitié de loquet (136) connectée au premier panneau (131A) ; une deuxième moitié de loquet (137) connectée au deuxième panneau (131B), la première et la deuxième moitié du loquet (136, 137) étant adaptées pour se verrouiller ensemble lorsque le premier et le deuxième panneaux (131A, 131B) sont en position fermée pour maintenir les panneaux (131A, 131B) en position fermée ; un système de protection thermique (135) couvrant une partie importante d’une face du premier panneau (131A) faisant face au moteur (140) lorsque le premier et le deuxième panneaux (131A, 131B) sont fermés ; et le système de protection thermique (135) peut comprendre une partie détachable (133) entourant et couvrant sensiblement le premier demi-loquet (136). Figure pour l’abrégé : Fig. 4AA propulsion system (110), comprising: a turbojet (140); a first panel (131A) and a second panel (131B) adapted to be removable between an open position in which access to the motor (140) is allowed during maintenance and a closed position in which the first and the second panel ( 131A, 131B) surround and substantially enclose at least a portion of the motor (140); a first latch half (136) connected to the first panel (131A); a second latch half (137) connected to the second panel (131B), the first and second half of the latch (136, 137) being adapted to lock together when the first and second panels (131A, 131B) are in position closed to hold the panels (131A, 131B) in the closed position; a thermal protection system (135) covering a substantial part of a face of the first panel (131A) facing the motor (140) when the first and second panels (131A, 131B) are closed; and the thermal protection system (135) may include a detachable portion (133) surrounding and substantially covering the first half-latch (136). Figure for the abstract: Fig. 4A

FR1871891A 2018-11-27 2018-11-27 DETACHABLE THERMAL INSULATION GASKET Expired - Fee Related FR3076859B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1871891A FR3076859B1 (en) 2018-11-27 2018-11-27 DETACHABLE THERMAL INSULATION GASKET

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1871891 2018-11-27
FR1871891A FR3076859B1 (en) 2018-11-27 2018-11-27 DETACHABLE THERMAL INSULATION GASKET

Publications (2)

Publication Number Publication Date
FR3076859A1 FR3076859A1 (en) 2019-07-19
FR3076859B1 true FR3076859B1 (en) 2021-01-01

Family

ID=66049265

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1871891A Expired - Fee Related FR3076859B1 (en) 2018-11-27 2018-11-27 DETACHABLE THERMAL INSULATION GASKET

Country Status (1)

Country Link
FR (1) FR3076859B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2897339B1 (en) * 2006-02-16 2008-04-11 Aircelle Sa NACELLE DE TURBOREACTEUR WITH LATERAL OPENING OF HOODS
US8916011B2 (en) * 2011-06-24 2014-12-23 United Technologies Corporation Fireshield fastener hood
US10179639B2 (en) * 2013-05-06 2019-01-15 Rohr, Inc. Attachment system for thermal protection panels

Also Published As

Publication number Publication date
FR3076859A1 (en) 2019-07-19

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