[go: up one dir, main page]

GB638094A - Improvements in or relating to gas-turbine-engine installations - Google Patents

Improvements in or relating to gas-turbine-engine installations

Info

Publication number
GB638094A
GB638094A GB2311947A GB2311947A GB638094A GB 638094 A GB638094 A GB 638094A GB 2311947 A GB2311947 A GB 2311947A GB 2311947 A GB2311947 A GB 2311947A GB 638094 A GB638094 A GB 638094A
Authority
GB
United Kingdom
Prior art keywords
grid
pipes
gas
hot gas
chamber
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
GB2311947A
Inventor
Adrian Albert Lombard
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Priority to GB2311947A priority Critical patent/GB638094A/en
Priority to CH266734D priority patent/CH266734A/en
Publication of GB638094A publication Critical patent/GB638094A/en
Expired legal-status Critical Current

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
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

638,094. Jet propulsion plant for aircraft. ROLLS-ROYCE, Ltd. Aug. 20, 1947, No. 23119. [Class 110(iii)] The air duct 18 of a jet-propulsion or other gas turbine plant is provided with an open grid formed by pipes 17 to which hot gas is supplied and a fine grid 19. Under severe conditions, the grid 19 may be blocked and air then passes through an annular byepass channel around the grid formed by walls 12a, 20. Solid matter entering the byepass will pass outside the wall 20 and collect in a chamber 200 from which it is evacuated. The hot gas is led by pipes 16 to a chamber 115 from which it goes to the grid pipes 17. Or the pipes 16 may convey the gas to a short annular chamber around the grid 17. The means supplying hot gas to the grid may be omitted or may be as described in Specifications 619,390, 636,612 and 638,079.
GB2311947A 1947-08-20 1947-08-20 Improvements in or relating to gas-turbine-engine installations Expired GB638094A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2311947A GB638094A (en) 1947-08-20 1947-08-20 Improvements in or relating to gas-turbine-engine installations
CH266734D CH266734A (en) 1947-08-20 1948-09-14 Gas turbine plant.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2311947A GB638094A (en) 1947-08-20 1947-08-20 Improvements in or relating to gas-turbine-engine installations

Publications (1)

Publication Number Publication Date
GB638094A true GB638094A (en) 1950-05-31

Family

ID=10190407

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2311947A Expired GB638094A (en) 1947-08-20 1947-08-20 Improvements in or relating to gas-turbine-engine installations

Country Status (2)

Country Link
CH (1) CH266734A (en)
GB (1) GB638094A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1184560B (en) * 1960-03-14 1964-12-31 Rolls Royce Heat exchangers, in particular for de-icing inlet struts for gas turbine engines
WO2003048546A1 (en) * 2001-12-04 2003-06-12 Honeywell International Inc. High energy particle arrestor for air turbine starters

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2149017B (en) * 1983-11-03 1988-01-27 Gen Electric Aircraft engine air intake including a foreign object separator
DE102009058352B4 (en) * 2009-12-15 2011-09-01 Diehl Aircabin Gmbh Line piece for absorbing foreign bodies and aircraft cabin equipped therewith

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1184560B (en) * 1960-03-14 1964-12-31 Rolls Royce Heat exchangers, in particular for de-icing inlet struts for gas turbine engines
WO2003048546A1 (en) * 2001-12-04 2003-06-12 Honeywell International Inc. High energy particle arrestor for air turbine starters
US6814539B2 (en) 2001-12-04 2004-11-09 Honeywell International, Inc. High energy particle arrestor for air turbine starters

Also Published As

Publication number Publication date
CH266734A (en) 1950-02-15

Similar Documents

Publication Publication Date Title
GB627832A (en) Improvement in propulsion plant comprising a gas turbine driven airscrew
GB726290A (en) Improvements in or relating to variable area nozzles for jet propulsion power plant
GB587513A (en) Improvements relating to gas turbine cooling systems
GB614548A (en) Improvements in or relating to air intakes for high speed flight
GB650462A (en) Improvements in or relating to combustion apparatus
GB636605A (en) Improvements in or relating to duct intakes or entries for gaseous fluid flow diffuser systems
GB1116930A (en) Improvements in cooled flameholder assembly
GB659151A (en) Improvements in or relating to gas turbine power plants
GB737322A (en) Improvements in or relating to aircraft and aircraft power plant arrangements
GB638094A (en) Improvements in or relating to gas-turbine-engine installations
GB627634A (en) Improvements in or relating to gas turbine aircraft propulsion power plants
GB922069A (en) Combustion chamber for a gas turbine engine
GB847500A (en) Improvements in piping systems or channels for the passage of fluids
GB656930A (en) Improvements in gas turbines
GB627396A (en) Improvements in or relating to aircraft gas-turbine power-plant installations
GB712633A (en) Improvements relating to gas-turbine engines
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB735645A (en) Improvements relating to aircraft reaction propulsion units and installations
GB638103A (en) Improvements in or relating to gas-turbine power-plant installations
GB779667A (en) Improvements relating to aircraft power plant installations
GB731418A (en) Improvements in combustion apparatus
GB587571A (en) Improvements in or relating to internal combustion turbine power plants
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB639468A (en) Improvements in combustion systems
GB746832A (en) Jet pipes of gas turbine engines