IT1158416B - GAS TURBINE ENGINE FOR MISSILE PROPULSION - Google Patents

GAS TURBINE ENGINE FOR MISSILE PROPULSION

Info

Publication number
IT1158416B
IT1158416B IT5212577A IT5212577A IT1158416B IT 1158416 B IT1158416 B IT 1158416B IT 5212577 A IT5212577 A IT 5212577A IT 5212577 A IT5212577 A IT 5212577A IT 1158416 B IT1158416 B IT 1158416B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
missile propulsion
missile
propulsion
Prior art date
Application number
IT5212577A
Other languages
Italian (it)
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Application granted granted Critical
Publication of IT1158416B publication Critical patent/IT1158416B/en

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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives
    • F02C7/272—Fluid drives generated by cartridges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

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)
  • Supercharger (AREA)
IT5212577A 1976-12-17 1977-12-07 GAS TURBINE ENGINE FOR MISSILE PROPULSION IT1158416B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5270476A GB1605252A (en) 1976-12-17 1976-12-17 Gas turbine engines

Publications (1)

Publication Number Publication Date
IT1158416B true IT1158416B (en) 1987-02-18

Family

ID=10464958

Family Applications (1)

Application Number Title Priority Date Filing Date
IT5212577A IT1158416B (en) 1976-12-17 1977-12-07 GAS TURBINE ENGINE FOR MISSILE PROPULSION

Country Status (3)

Country Link
FR (1) FR2581127A1 (en)
GB (1) GB1605252A (en)
IT (1) IT1158416B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7097412B2 (en) * 2003-02-14 2006-08-29 United Technologies Corporation Turbine engine bearing support
CA2533425C (en) 2003-07-29 2012-09-25 Pratt & Whitney Canada Corp. Turbofan case and method of making
US7370467B2 (en) 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
GB0904970D0 (en) * 2009-03-24 2009-05-06 Rolls Royce Plc A casing arrangement
EP2700798A1 (en) * 2012-08-21 2014-02-26 Siemens Aktiengesellschaft Turbomachine comprising a rotor and a casing
WO2014051686A1 (en) * 2012-09-26 2014-04-03 United Technologies Corporation Combined high pressure turbine case and turbine intermediate case

Also Published As

Publication number Publication date
FR2581127A1 (en) 1986-10-31
GB1605252A (en) 1986-06-04

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