IL103257A - From the mouth of the engine to the engine having a blower turbine placed in the pipe - Google Patents

From the mouth of the engine to the engine having a blower turbine placed in the pipe

Info

Publication number: IL103257A
Authority: IL; Israel
Prior art keywords: nacelle; discharge nozzle; assembly; outer discharge; nozzle
Prior art date: 1991-09-27

Application number

IL10325792A

Other languages

English (en)

Hebrew (he)

Original Assignee

Short Brothers Plc

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.)

1991-09-27

Filing date

1992-09-23

Publication date

1995-12-08

1992-09-23 Application filed by Short Brothers Plc filed Critical Short Brothers Plc

1995-12-08 Publication of IL103257A publication Critical patent/IL103257A/en

Links

230000005540 biological transmission Effects 0.000 claims description 2
230000000717 retained effect Effects 0.000 claims description 2
229910000838 Al alloy Inorganic materials 0.000 description 7
239000000463 material Substances 0.000 description 7
239000007789 gas Substances 0.000 description 4
PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
238000010276 construction Methods 0.000 description 3
239000000853 adhesive Substances 0.000 description 2
230000001070 adhesive effect Effects 0.000 description 2
230000037361 pathway Effects 0.000 description 2
DMYOHQBLOZMDLP-UHFFFAOYSA-N 1-[2-(2-hydroxy-3-piperidin-1-ylpropoxy)phenyl]-3-phenylpropan-1-one Chemical compound C1CCCCN1CC(O)COC1=CC=CC=C1C(=O)CCC1=CC=CC=C1 DMYOHQBLOZMDLP-UHFFFAOYSA-N 0.000 description 1
229910000831 Steel Inorganic materials 0.000 description 1
229920001079 Thiokol (polymer) Polymers 0.000 description 1
RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
239000004411 aluminium Substances 0.000 description 1
XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
229910052782 aluminium Inorganic materials 0.000 description 1
230000000712 assembly Effects 0.000 description 1
238000000429 assembly Methods 0.000 description 1
230000015556 catabolic process Effects 0.000 description 1
238000001816 cooling Methods 0.000 description 1
238000006731 degradation reaction Methods 0.000 description 1
230000000694 effects Effects 0.000 description 1
RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
229910001026 inconel Inorganic materials 0.000 description 1
238000007689 inspection Methods 0.000 description 1
239000003562 lightweight material Substances 0.000 description 1
238000000034 method Methods 0.000 description 1
230000006798 recombination Effects 0.000 description 1
238000005215 recombination Methods 0.000 description 1
239000007921 spray Substances 0.000 description 1
239000010959 steel Substances 0.000 description 1
239000010936 titanium Substances 0.000 description 1
229910052719 titanium Inorganic materials 0.000 description 1

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
- B64D29/00—Power-plant nacelles, fairings or cowlings
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Control Of Turbines (AREA)

IL10325792A 1991-09-27 1992-09-23 From the mouth of the engine to the engine having a blower turbine placed in the pipe IL103257A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB919120658A GB9120658D0 (en)	1991-09-27	1991-09-27	Ducted fan turbine engine

Publications (1)

Publication Number	Publication Date
IL103257A true IL103257A (en)	1995-12-08

Family

ID=10702134

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
IL10325792A IL103257A (en)	1991-09-27	1992-09-23	From the mouth of the engine to the engine having a blower turbine placed in the pipe

Country Status (10)

Country	Link
US (1)	US5603471A (pt)
EP (1)	EP0605525B1 (pt)
JP (1)	JPH06510724A (pt)
AU (1)	AU661717B2 (pt)
BR (1)	BR9206544A (pt)
CA (1)	CA2119440A1 (pt)
DE (1)	DE69209842T2 (pt)
GB (2)	GB9120658D0 (pt)
IL (1)	IL103257A (pt)
WO (1)	WO1993006006A1 (pt)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB9407632D0 (en) *	1994-04-18	1994-06-08	Short Brothers Plc	An aircraft propulsive power unit
FR2734540B1 (fr) *	1995-05-24	1997-08-08	Aerospatiale	Nacelle de moteur d'aeronef comportant un capot de nacelle
FR2771330B1 (fr) *	1997-11-26	2004-02-27	Aerospatiale	Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
FR2772342B1 (fr) *	1997-12-16	2000-02-18	Aerospatiale	Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
FR2844303B1 (fr)	2002-09-10	2006-05-05	Airbus France	Piece tubulaire d'attenuation acoustique pour entree d'air de reacteur d'aeronef
FR2851226B1 (fr) *	2003-02-19	2005-05-20	Snecma Moteurs	Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
WO2004101975A1 (de) *	2003-05-15	2004-11-25	Alstom Technology Ltd	Vorrichtung zur schalldämpfung in einem strömungskanal
FR2856379B1 (fr) *	2003-06-18	2006-11-24	Airbus France	Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
US20060145001A1 (en) *	2004-12-30	2006-07-06	Smith Matthew C	Fan cowl door elimination
US20110101158A1 (en) *	2005-03-29	2011-05-05	The Boeing Company	Thrust Reversers Including Monolithic Components
US7435050B2 (en) *	2006-01-11	2008-10-14	United Technologies Corporation	Split flange V-groove and anti-rotation mating system
FR2905734B1 (fr) *	2006-09-07	2012-07-13	Airbus France	Dispositif permettant d'ameliorer l'efficacite des traitements acoustiques dans un conduit d'une motorisation d'aeronef
FR2905991B1 (fr)	2006-09-20	2012-01-13	Snecma	Systeme propulsif integre comportant un moteur a turboreacteur a double flux.
FR2907759B1 (fr) *	2006-10-31	2008-12-12	Aircelle Sa	Nacelle pour turboreacteur a ouverture laterale
FR2915527B1 (fr) *	2007-04-30	2009-06-12	Aircelle Sa	Structure arriere de nacelle pour moteur a reacteur, telle qu'un inverseur de poussee
FR2916426B1 (fr) *	2007-05-22	2010-04-02	Aircelle Sa	Ensemble arriere de nacelle pour turboreacteur.
US7762057B2 (en) *	2007-06-05	2010-07-27	The Boeing Company	Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
US8726665B2 (en)	2007-06-05	2014-05-20	The Boeing Company	Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
FR2925120B1 (fr) *	2007-12-18	2010-02-19	Snecma	Extension de carter intermediaire pour turboreacteur d'aeronef, comprenant une rainure annulaire sectorisee de reception des capots de nacelle
FR2926112A1 (fr) *	2008-01-08	2009-07-10	Aircelle Sa	Inverseur de poussee a portes pour turboreacteur
FR2933071B1 (fr) *	2008-06-25	2010-06-11	Snecma	Dispositif de capotage de nacelle d'unite de puissance propulsive d'aeronef
FR2935753B1 (fr) *	2008-09-08	2011-07-01	Snecma Propulsion Solide	Liaisons souples a butee pour fixation de piece en cmc
FR2936777B1 (fr) *	2008-10-08	2010-10-22	Aircelle Sa	Structure d'entree d'air pour une nacelle pour turboreacteur
FR2939410B1 (fr) *	2008-12-04	2012-06-15	Airbus France	Systeme de fermeture d'un capot de soufflante pour aeronef
FR2949820B1 (fr) *	2009-09-04	2011-10-14	Aircelle Sa	Ensemble structurant pour une tuyere d'ejection.
FR2955312B1 (fr)	2010-01-20	2013-05-31	Airbus Operations Sas	Dispositif de liaison fusible entre une partie mobile et une partie fixe d'une nacelle d'aeronef
FR2958978B1 (fr) *	2010-04-20	2014-04-18	Aircelle Sa	Agencement de bielles de volets d'inversion de poussee sur la structure interne fixe d'une nacelle de turboreacteur
FR2978989B1 (fr)	2011-08-12	2013-07-26	Aircelle Sa	Cone d'ejection pour turboreacteur d'aeronef
FR2978988B1 (fr) *	2011-08-12	2013-07-26	Aircelle Sa	Cone d'ejection pour turboreacteur d'aeronef
FR2988777B1 (fr) *	2012-03-29	2014-04-25	Snecma Propulsion Solide	Integration de pieces d'arriere-corps de moteur aeronautique
US9108736B2 (en) *	2012-06-05	2015-08-18	United Technologies Corporation	Nacelle inner flow structure leading edge latching system
US9897007B2 (en) *	2012-07-24	2018-02-20	Rohr, Inc.	Thrust reverser-integrated track beam and inner fixed structure
US10060292B2 (en) *	2013-03-14	2018-08-28	United Technologies Corporation	Castellated latch mechanism for a gas turbine engine
FR3012114B1 (fr) *	2013-10-18	2017-02-24	Airbus Operations Sas	Ensemble propulsif d'aeronef comportant une nacelle pourvue d'un mecanisme de verrouillage et de fermeture des capots
US9366202B2 (en) *	2013-11-27	2016-06-14	Rohr, Inc.	System and method for captured inner fixed structure
US9574518B2 (en)	2014-06-02	2017-02-21	The Boeing Company	Turbofan engine with variable exhaust cooling
FR3024754B1 (fr) *	2014-08-11	2016-08-26	Snecma	Ensemble de liaison pour parties de carter d'une turbomachine
US9995247B2 (en) *	2015-10-06	2018-06-12	Spirit Aerosystems, Inc.	Hybrid thrust reverser inner wall for aircraft engines
FR3045570B1 (fr) *	2015-12-16	2017-12-22	Airbus Operations Sas	Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
DE102016101168A1 (de) *	2016-01-22	2017-07-27	Rolls-Royce Deutschland Ltd & Co Kg	Strömungsmaschine mit einer in einer Ausnehmung einer Wandung anordenbaren Einsetzeinrichtung
US11325717B2 (en)	2016-10-13	2022-05-10	Airbus Operations Sas	Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engine
FR3057544A1 (fr) *	2016-10-13	2018-04-20	Airbus Operations	Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation
US11535390B2 (en) *	2020-02-28	2022-12-27	Rohr, Inc.	Structural panel with integrated coupler
FR3121429A1 (fr) *	2021-04-02	2022-10-07	Airbus Operations	Nacelle d’aéronef comportant un système de joint avec ressort pour une casquette de ladite nacelle

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB587512A (en) *	1942-05-13	1947-04-29	Frank Whittle	Improvements relating to exhaust systems of jet propulsion installations in aircraft
BE487116A (pt) *	1946-07-16
US2809057A (en) *	1955-02-18	1957-10-08	Orenda Eugines Ltd	Flexible joint for annular members and employing wedge shaped connecting units
GB918778A (en) *	1959-06-23	1963-02-20	Rolls Royce	Improvements in or relating to gas-turbine engines
US3225636A (en) *	1960-11-01	1965-12-28	Houdaille Industries Inc	Punching machine and structure therefor
US3750402A (en) *	1963-08-07	1973-08-07	Gen Electric	Mixed flow augmentation system
FR1460577A (fr) *	1965-06-14	1966-03-04	Snecma	Perfectionnements à la liaison articulée des conduits, notamment à l'accrochage du canal d'éjection d'un propulseur à réaction
FR1579526A (pt) *	1968-02-29	1969-08-29
US3824784A (en) *	1969-09-29	1974-07-23	Secr Defence	Thrust deflectors for ducted fan gas turbine engines
FR2379433A1 (fr) *	1977-02-08	1978-09-01	Snecma	Systeme de securite pour capotage de nacelle de turboreacteur
US4772033A (en) *	1983-09-28	1988-09-20	General Electric Company	Flexible duct joint utilizing lip in recess in a flange
US4825648A (en) *	1987-03-02	1989-05-02	General Electric Company	Turbofan engine having a split cowl
GB8822798D0 (en) *	1988-09-28	1988-11-02	Short Brothers Ltd	Ducted fan turbine engine
FR2661213B1 (fr) *	1990-04-19	1992-07-03	Snecma	Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.

1991
- 1991-09-27 GB GB919120658A patent/GB9120658D0/en active Pending
1992
- 1992-09-23 CA CA002119440A patent/CA2119440A1/en not_active Abandoned
- 1992-09-23 DE DE69209842T patent/DE69209842T2/de not_active Expired - Fee Related
- 1992-09-23 IL IL10325792A patent/IL103257A/en not_active IP Right Cessation
- 1992-09-23 GB GB9220117A patent/GB2259954B/en not_active Expired - Fee Related
- 1992-09-23 JP JP5505928A patent/JPH06510724A/ja active Pending
- 1992-09-23 WO PCT/GB1992/001747 patent/WO1993006006A1/en not_active Ceased
- 1992-09-23 AU AU25941/92A patent/AU661717B2/en not_active Ceased
- 1992-09-23 EP EP92919854A patent/EP0605525B1/en not_active Expired - Lifetime
- 1992-09-23 BR BR9206544A patent/BR9206544A/pt not_active Application Discontinuation
- 1992-09-23 US US08/211,213 patent/US5603471A/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
WO1993006006A1 (en)	1993-04-01
EP0605525A1 (en)	1994-07-13
JPH06510724A (ja)	1994-12-01
GB2259954A (en)	1993-03-31
BR9206544A (pt)	1995-11-07
EP0605525B1 (en)	1996-04-10
DE69209842D1 (de)	1996-05-15
US5603471A (en)	1997-02-18
CA2119440A1 (en)	1993-04-01
GB2259954B (en)	1994-12-14
DE69209842T2 (de)	1996-10-31
AU2594192A (en)	1993-04-27
GB9220117D0 (en)	1992-11-04
AU661717B2 (en)	1995-08-03
GB9120658D0 (en)	1991-11-06

Legal Events

Date	Code	Title	Description
1996-06-18	FF	Patent granted
1999-09-22	RH	Patent void

Publication	Publication Date	Title
US5603471A (en)	1997-02-18	Ducted fan turbine engine nozzle assembly
US5136839A (en)	1992-08-11	Ducted fan turbine engine
US4731991A (en)	1988-03-22	Gas turbine engine thrust reverser
EP1430212B1 (en)	2013-09-11	Converging nozzle thrust reverser
EP1627812B1 (en)	2011-03-02	An engine mounting assembly
US3779010A (en)	1973-12-18	Combined thrust reversing and throat varying mechanism for a gas turbine engine
US5943856A (en)	1999-08-31	Turbofan engine with reduced noise
US3970252A (en)	1976-07-20	Cooled exhaust duct
US6170253B1 (en)	2001-01-09	Cascade structure arrangement for a gas turbine engine
US10947904B2 (en)	2021-03-16	Sealing cooling inner fixed structure
GB2437295A (en)	2007-10-24	Aeroengine ventilation system
US9714627B2 (en)	2017-07-25	Mounting of aircraft propulsion system outer sleeve and inner structure to pylon with distinct hinges
CA2726503A1 (en)	2011-06-21	Integrated nacelle assembly
JP5557855B2 (ja)	2014-07-23	熱的に平衡のとれた航空機構造
US11753968B2 (en)	2023-09-12	Nacelle cowling structure for a turbomachine
JPH0233455A (ja)	1990-02-02	ジェットエンジンおよび逆推進アセンブリならびにジェットエンジンの推力を転換させる方法
EP0761947B1 (en)	2000-05-24	Noise reduction kit for turbofan engine
US3310951A (en)	1967-03-28	Jet propulsion engines for aircraft
GB2179702A (en)	1987-03-11	Turbo-propeller aircraft engine
HK1006257A (en)	1999-02-19	Noise reduction kit for turbofan engine