SE453767B - Konvergent/divergent munstycksaggregat - Google Patents

Konvergent/divergent munstycksaggregat

Info

Publication number
SE453767B
SE453767B SE8206771A SE8206771A SE453767B SE 453767 B SE453767 B SE 453767B SE 8206771 A SE8206771 A SE 8206771A SE 8206771 A SE8206771 A SE 8206771A SE 453767 B SE453767 B SE 453767B
Authority
SE
Sweden
Prior art keywords
flaps
common ring
upstream
downstream
convergent
Prior art date
Application number
SE8206771A
Other languages
English (en)
Swedish (sv)
Other versions
SE8206771D0 (sv
SE8206771L (sv
Inventor
W H Wiley
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SE8206771D0 publication Critical patent/SE8206771D0/xx
Publication of SE8206771L publication Critical patent/SE8206771L/xx
Publication of SE453767B publication Critical patent/SE453767B/sv

Links

Classifications

    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1292—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/292—Three-dimensional machined; miscellaneous tapered
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/323—Arrangement of components according to their shape convergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/34—Arrangement of components translated

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SE8206771A 1981-12-28 1982-11-26 Konvergent/divergent munstycksaggregat SE453767B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/334,490 US4440346A (en) 1981-12-28 1981-12-28 Axially translatable variable area convergent/divergent nozzle

Publications (3)

Publication Number Publication Date
SE8206771D0 SE8206771D0 (sv) 1982-11-26
SE8206771L SE8206771L (sv) 1983-06-29
SE453767B true SE453767B (sv) 1988-02-29

Family

ID=23307450

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8206771A SE453767B (sv) 1981-12-28 1982-11-26 Konvergent/divergent munstycksaggregat

Country Status (7)

Country Link
US (1) US4440346A (fr)
JP (1) JPS58117337A (fr)
DE (1) DE3242822A1 (fr)
EG (1) EG15577A (fr)
IL (1) IL67300A (fr)
SE (1) SE453767B (fr)
TR (1) TR21973A (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4552309A (en) * 1982-04-07 1985-11-12 Rolls-Royce Inc. Variable geometry nozzles for turbomachines
US5082182A (en) * 1990-08-23 1992-01-21 United Technologies Corporation Thrust vectoring exhaust nozzle
US5261605A (en) * 1990-08-23 1993-11-16 United Technologies Corporation Axisymmetric nozzle with gimbled unison ring
DE69232222T2 (de) * 1991-05-16 2002-08-22 General Electric Co., Schenectady Hitzeschild für achsymmetrische schwenkbare Schubdüse
US5431344A (en) * 1993-11-12 1995-07-11 United Technologies Corporation Sliding throat gas turbine engine nozzle
US5484105A (en) * 1994-07-13 1996-01-16 General Electric Company Cooling system for a divergent section of a nozzle
US5794850A (en) 1996-09-27 1998-08-18 United Technologies Corporation Enclosed pressure balanced sync ring nozzle
US5813611A (en) * 1996-09-27 1998-09-29 United Technologies Corporation Compact pressure balanced fulcrum-link nozzle
US6966175B2 (en) * 2003-05-09 2005-11-22 The Nordam Group, Inc. Rotary adjustable exhaust nozzle
JP2006231459A (ja) 2005-02-24 2006-09-07 Yuyama Manufacturing Co Ltd バイアル瓶搬送装置およびそのアーム
US20080072604A1 (en) * 2006-09-26 2008-03-27 United Technologies Corporation Pressure balance control for gas turbine engine nozzle
US7854124B2 (en) * 2006-10-27 2010-12-21 United Technologies Corporation Combined control for supplying cooling air and support air in a turbine engine nozzle
US8931281B2 (en) 2010-06-07 2015-01-13 United Technologies Corporation External flap retaining mechanism
US9511873B2 (en) 2012-03-09 2016-12-06 The Boeing Company Noise-reducing engine nozzle system
US9492832B2 (en) 2013-03-14 2016-11-15 Rain Bird Corporation Sprinkler with brake assembly
US10350619B2 (en) 2013-02-08 2019-07-16 Rain Bird Corporation Rotary sprinkler
US9700904B2 (en) 2014-02-07 2017-07-11 Rain Bird Corporation Sprinkler
GB201609071D0 (en) 2016-05-24 2016-07-06 Rolls Royce Plc Aircraft gas turbine engine nacelle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2972226A (en) * 1955-10-06 1961-02-21 United Aircraft Corp Variable area converging-diverging nozzle
US3792815A (en) * 1972-11-24 1974-02-19 United Aircraft Corp Balanced flap converging/diverging nozzle
US4196856A (en) * 1977-11-25 1980-04-08 The Boeing Company Variable geometry convergent divergent exhaust nozzle
US4245787A (en) * 1978-12-01 1981-01-20 General Electric Company Variable area nozzle system

Also Published As

Publication number Publication date
DE3242822A1 (de) 1983-07-07
IL67300A0 (en) 1983-03-31
TR21973A (tr) 1985-12-12
JPS58117337A (ja) 1983-07-12
IL67300A (en) 1989-10-31
US4440346A (en) 1984-04-03
JPH0261617B2 (fr) 1990-12-20
SE8206771D0 (sv) 1982-11-26
EG15577A (en) 1986-12-30
DE3242822C2 (fr) 1992-11-12
SE8206771L (sv) 1983-06-29

Similar Documents

Publication Publication Date Title
SE453767B (sv) Konvergent/divergent munstycksaggregat
US4409788A (en) Actuation system for use on a gas turbine engine
US3779665A (en) Combined variable angle stator and windmill control system
US3747341A (en) Fans
US3837411A (en) Diverter valve for a gas turbine with an augmenter
US11085310B2 (en) Variable pitch fan actuator
SE453768B (sv) Munstycksaggregat med varierbar area for gasturbinmotorer
US4755104A (en) Stator vane linkage
US3869221A (en) Rotor wheel fan blade adjusting apparatus for turbojet engines and the like
JPS6125902B2 (fr)
EP2626521B1 (fr) Ensemble d'engrenages d'anneau de conjugaison d'une turbine à gaz
SE449017B (sv) Munstycksaggregat med varierbar area for gasturbinmotorer
US4141501A (en) Nozzles for gas turbine engines
KR100453669B1 (ko) 축대칭수렴/확대배기노즐
GB2557435A (en) Propulsion assembly comprising a duct for feeding the gas generator in an inter-duct casing
SE433960B (sv) Stralrorsklaffanordning vid stralror med variabel area for gasturbinmotor
JP2016050579A (ja) 可変形状ベーンのための回転式アクチュエータ
JPS59134356A (ja) ガスタ−ビンエンジン用先細／末広排気ノズル組立体
KR0167796B1 (ko) 짐블드 유니즌 링이 구비된 축대칭 노즐
JP2007309316A (ja) 排気駆動式過給機の軸流タービンの案内羽根装置
SE453936B (sv) Munstycke for gasturbin-flygmotor
US10385721B2 (en) System for controlling variable pitch blades for a turbine engine
EP1916405B1 (fr) Tuyère à section variable de contrôle du vecteur de poussée pour nacelle de soufflante de turboréacteur
US8347601B2 (en) Device for pivoting at least one pivotable element in a gas turbine engine
US20220341342A1 (en) Variable vane apparatus

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 8206771-1

Effective date: 19930610

Format of ref document f/p: F