FR1144879A - Exhaust manifold for gas turbine type airplane power plant - Google Patents

Exhaust manifold for gas turbine type airplane power plant

Info

Publication number
FR1144879A
FR1144879A FR1144879DA FR1144879A FR 1144879 A FR1144879 A FR 1144879A FR 1144879D A FR1144879D A FR 1144879DA FR 1144879 A FR1144879 A FR 1144879A
Authority
FR
France
Prior art keywords
gas turbine
power plant
exhaust manifold
turbine type
airplane power
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
Other languages
French (fr)
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son 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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Application granted granted Critical
Publication of FR1144879A publication Critical patent/FR1144879A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/20Mounting or supporting of plant; Accommodating heat expansion or creep
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1144879D 1955-03-30 1956-03-28 Exhaust manifold for gas turbine type airplane power plant Expired FR1144879A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1144879X 1955-03-30

Publications (1)

Publication Number Publication Date
FR1144879A true FR1144879A (en) 1957-10-18

Family

ID=10877473

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1144879D Expired FR1144879A (en) 1955-03-30 1956-03-28 Exhaust manifold for gas turbine type airplane power plant

Country Status (1)

Country Link
FR (1) FR1144879A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3296804A (en) * 1962-08-24 1967-01-10 Rolls Royce Gas turbine vertical lift engine
FR2565293A1 (en) * 1984-06-04 1985-12-06 Aerospatiale JET DILUATOR-DEVIATOR ASSEMBLY FOR AERODYNE TURBOMOTEUR

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3296804A (en) * 1962-08-24 1967-01-10 Rolls Royce Gas turbine vertical lift engine
FR2565293A1 (en) * 1984-06-04 1985-12-06 Aerospatiale JET DILUATOR-DEVIATOR ASSEMBLY FOR AERODYNE TURBOMOTEUR
EP0165167A1 (en) * 1984-06-04 1985-12-18 AEROSPATIALE Société Nationale Industrielle Jet dilution and deviation device to suppress the infrared radiation of a turbo motor
US4662174A (en) * 1984-06-04 1987-05-05 Societe Nationale Industrielle Et Aerospatiale Plume diluter diverter assembly for a turbine engine of a heavier than air machine

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