IT971528B - Presse d aria per un motore a turbina a gas - Google Patents

Presse d aria per un motore a turbina a gas

Info

Publication number
IT971528B
IT971528B IT32470/72A IT3247072A IT971528B IT 971528 B IT971528 B IT 971528B IT 32470/72 A IT32470/72 A IT 32470/72A IT 3247072 A IT3247072 A IT 3247072A IT 971528 B IT971528 B IT 971528B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
air presses
presses
air
Prior art date
Application number
IT32470/72A
Other languages
English (en)
Original Assignee
Rolls Royce 1971 Ltd
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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT971528B publication Critical patent/IT971528B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT32470/72A 1971-12-04 1972-12-04 Presse d aria per un motore a turbina a gas IT971528B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5639471A GB1382809A (en) 1971-12-04 1971-12-04 Air intakes for gas turbine engines

Publications (1)

Publication Number Publication Date
IT971528B true IT971528B (it) 1974-05-10

Family

ID=10476503

Family Applications (1)

Application Number Title Priority Date Filing Date
IT32470/72A IT971528B (it) 1971-12-04 1972-12-04 Presse d aria per un motore a turbina a gas

Country Status (6)

Country Link
US (1) US3763874A (it)
JP (1) JPS4875913A (it)
DE (1) DE2259238A1 (it)
FR (1) FR2162225A1 (it)
GB (1) GB1382809A (it)
IT (1) IT971528B (it)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4133567A (en) * 1977-05-11 1979-01-09 Texaco Inc. Combined cycle electric power generating system with improvement
US4209149A (en) * 1977-12-27 1980-06-24 Boeing Commercial Airplane Company Contracted inlet for jet engine being transported as cargo
US4220171A (en) * 1979-05-14 1980-09-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Curved centerline air intake for a gas turbine engine
US5000399A (en) * 1990-02-23 1991-03-19 General Electric Company Variable contour annular air inlet for an aircraft engine nacelle
FR2731049B1 (fr) * 1995-02-28 1997-05-09 Aerospatiale Dispositif de fixation d'une bouche d'entree d'air sur un reacteur et reacteur comportant un tel dispositif
US6089505A (en) * 1997-07-22 2000-07-18 Mcdonnell Douglas Corporation Mission adaptive inlet
US20050274103A1 (en) * 2004-06-10 2005-12-15 United Technologies Corporation Gas turbine engine inlet with noise reduction features
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
US7797944B2 (en) 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
US7870721B2 (en) 2006-11-10 2011-01-18 United Technologies Corporation Gas turbine engine providing simulated boundary layer thickness increase
US8408491B2 (en) 2007-04-24 2013-04-02 United Technologies Corporation Nacelle assembly having inlet airfoil for a gas turbine engine
US8205430B2 (en) 2007-05-16 2012-06-26 United Technologies Corporation Variable geometry nacelle assembly for a gas turbine engine
US8727267B2 (en) 2007-05-18 2014-05-20 United Technologies Corporation Variable contraction ratio nacelle assembly for a gas turbine engine
US20080310956A1 (en) * 2007-06-13 2008-12-18 Jain Ashok K Variable geometry gas turbine engine nacelle assembly with nanoelectromechanical system
US8402739B2 (en) 2007-06-28 2013-03-26 United Technologies Corporation Variable shape inlet section for a nacelle assembly of a gas turbine engine
US9228534B2 (en) 2007-07-02 2016-01-05 United Technologies Corporation Variable contour nacelle assembly for a gas turbine engine
US9004399B2 (en) 2007-11-13 2015-04-14 United Technologies Corporation Nacelle flow assembly
US8186942B2 (en) 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
US8192147B2 (en) 2007-12-14 2012-06-05 United Technologies Corporation Nacelle assembly having inlet bleed
EP2157299A1 (en) 2008-07-17 2010-02-24 United Technologies Corporation Nacelle assembly for a gas turbine engine with variable shape inlet section, corresponding gas turbine engine and operating method
GB0813482D0 (en) * 2008-07-24 2008-08-27 Rolls Royce Plc Gas turbine engine nacelle
GB0813484D0 (en) * 2008-07-24 2008-08-27 Rolls Royce Plc Gas turbine engine nacelle
US8240597B2 (en) 2008-08-06 2012-08-14 Honeywell International Inc. UAV ducted fan lip shaping
EP2391542B1 (fr) * 2009-02-02 2014-07-30 Airbus Operations (S.A.S.) Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise
FR2941674B1 (fr) * 2009-02-04 2011-02-11 Aircelle Sa Nacelle de turboreacteur.
FR2978734B1 (fr) * 2011-08-05 2015-01-02 Airbus Operations Sas Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
US11480104B2 (en) * 2013-03-04 2022-10-25 Raytheon Technologies Corporation Gas turbine engine inlet
US11441482B2 (en) * 2019-06-04 2022-09-13 Rohr, Inc. Single track translating inlet
WO2024006584A2 (en) * 2022-07-01 2024-01-04 Xagon Solutions Inc. Adaptive duct fan with individually controlled slats

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2948111A (en) * 1955-05-02 1960-08-09 Doak Aircraft Co Inc Means to increase static pressure and enhance forward thrust of aircraft components
FR1589899A (it) * 1968-10-24 1970-04-06

Also Published As

Publication number Publication date
US3763874A (en) 1973-10-09
GB1382809A (en) 1975-02-05
JPS4875913A (it) 1973-10-12
DE2259238A1 (de) 1973-06-14
FR2162225A1 (it) 1973-07-13

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