DE2303382C3 - Turbostrahltriebwerk - Google Patents

Turbostrahltriebwerk

Info

Publication number
DE2303382C3
DE2303382C3 DE19732303382 DE2303382A DE2303382C3 DE 2303382 C3 DE2303382 C3 DE 2303382C3 DE 19732303382 DE19732303382 DE 19732303382 DE 2303382 A DE2303382 A DE 2303382A DE 2303382 C3 DE2303382 C3 DE 2303382C3
Authority
DE
Germany
Prior art keywords
hollow shaft
shaft
rotor
sections
pressure compressor
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
Application number
DE19732303382
Other languages
German (de)
English (en)
Other versions
DE2303382A1 (de
DE2303382B2 (de
Inventor
Andre Emile Seine-Port Duclos
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE2303382A1 publication Critical patent/DE2303382A1/de
Publication of DE2303382B2 publication Critical patent/DE2303382B2/de
Application granted granted Critical
Publication of DE2303382C3 publication Critical patent/DE2303382C3/de
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/026—Shaft to shaft connections
    • 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
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE19732303382 1972-01-27 1973-01-24 Turbostrahltriebwerk Expired DE2303382C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7202693A FR2168938B1 (US20080094685A1-20080424-C00004.png) 1972-01-27 1972-01-27

Publications (3)

Publication Number Publication Date
DE2303382A1 DE2303382A1 (de) 1973-08-02
DE2303382B2 DE2303382B2 (de) 1980-07-03
DE2303382C3 true DE2303382C3 (de) 1981-04-30

Family

ID=9092530

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19732303382 Expired DE2303382C3 (de) 1972-01-27 1973-01-24 Turbostrahltriebwerk

Country Status (3)

Country Link
DE (1) DE2303382C3 (US20080094685A1-20080424-C00004.png)
FR (1) FR2168938B1 (US20080094685A1-20080424-C00004.png)
GB (1) GB1357712A (US20080094685A1-20080424-C00004.png)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2046843B (en) * 1979-04-17 1983-01-26 Rolls Royce Gas turbine engines-de-icing-icing
FR2621554B1 (fr) * 1987-10-07 1990-01-05 Snecma Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe
US4860534A (en) * 1988-08-24 1989-08-29 General Motors Corporation Inlet particle separator with anti-icing means
GB9120113D0 (en) * 1991-09-20 1992-09-23 Short Brothers Plc Thermal antiicing of aircraft structures
FR2950928B1 (fr) * 2009-10-02 2011-12-09 Snecma Cone d'entree autodegivrant pour turbomachine d'aeronef
ITCO20110017A1 (it) * 2011-05-19 2012-11-20 Nuovo Pignone Spa Sistema di turbina a gas integrato e metodo
FR2998620B1 (fr) * 2012-11-29 2018-04-06 Safran Aircraft Engines Capot de turbomachine apte a recouvrir un cone de soufflante
FR3025551B1 (fr) 2014-09-05 2019-08-23 Safran Aircraft Engines Arbre de turbomachine
CN107061013B (zh) * 2017-03-30 2019-05-24 中国航发沈阳发动机研究所 一种用于发动机进口旋转整流帽罩的热气防冰方法
CN112302725B (zh) * 2020-09-18 2022-07-26 中国航发四川燃气涡轮研究院 一种紧凑型航空发动机高压转子连接结构
FR3143545A1 (fr) * 2022-12-16 2024-06-21 Safran Nacelles Capot d’une turbomachine d’aéronef comprenant une interface centrale de préhension

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2757857A (en) * 1951-06-19 1956-08-07 United Aircraft Corp Locking means between compressor and turbine
FR1520460A (fr) * 1967-01-11 1968-04-12 Snecma Perfectionnements aux turboréacteurs à flux multiples
GB1210202A (en) * 1969-03-06 1970-10-28 Rolls Royce Gas turbine engine

Also Published As

Publication number Publication date
FR2168938A1 (US20080094685A1-20080424-C00004.png) 1973-09-07
FR2168938B1 (US20080094685A1-20080424-C00004.png) 1974-12-13
DE2303382A1 (de) 1973-08-02
DE2303382B2 (de) 1980-07-03
GB1357712A (en) 1974-06-26

Similar Documents

Publication Publication Date Title
DE2363339C2 (de) Enteisungsanlage für Strömungsmaschinen von Luftfahrzeugen
DE3828834C1 (US20080094685A1-20080424-C00004.png)
DE2303382C3 (de) Turbostrahltriebwerk
DE2364431C2 (de) Verbindungsvorrichtung für das freie Ende einer mit dem Turbinenrotor einer Gasturbinenanlage verbundenen Welle
DE3015650C2 (de) Notschmiereinrichtung für Gasturbinenanlagen
DE102005043615B4 (de) Propellerantriebseinheit
DE602004002049T2 (de) Niederdruck-Turbine einer Turbomaschine
DE3310529A1 (de) Vorrichtung zum Kühlen des Rotors einer Gasturbine
DE3219615A1 (de) Strahlturbine mit gegenlaeufigen raedern
DE2121069A1 (de) Gasturbinentriebwerk mit Kuhlsystem
DE2327243A1 (de) Brennergehaeuse und konzentrische luftabzweigungsstruktur
EP0834645A1 (de) Verdichterradbefestigung für Turbolader
DE1476791A1 (de) Leitungsverbindungen fuer Gasturbinentriebwerke von Flugzeugen
CH669428A5 (US20080094685A1-20080424-C00004.png)
EP3189934A1 (de) Vorrichtung zur reinigung eines strahltriebwerks
DE2140337A1 (de) Gasturbinentriebwerk
DE1800925C3 (de) Gasturbinen Hubgeblasetriebwerk
DE2327244A1 (de) Brennergehaeuse und kuehlstruktur
DE899298C (de) Gasturbine fuer wechselnde Belastungen
DE672114C (de) Gleichdruckgasturbinentriebwerk, insbesondere fuer Flugzeuge
DE9090085U1 (de) Brennkraftmaschine
DE889243C (de) Strahltriebwerk
DE807574C (de) Brennkraftturbine
DE2042669A1 (de) Verfahren und Vorrichtung zur Erzeugung einer Drehmomentbelastung an einer Welle
DE1301653B (de) Gasturbinenstrahltriebwerk mit zwei gegenlaeufig rotierenden Wellen

Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee