GB697006A - Water separating guide vanes for gas turbine engines - Google Patents

Water separating guide vanes for gas turbine engines

Info

Publication number
GB697006A
GB697006A GB1069250A GB1069250A GB697006A GB 697006 A GB697006 A GB 697006A GB 1069250 A GB1069250 A GB 1069250A GB 1069250 A GB1069250 A GB 1069250A GB 697006 A GB697006 A GB 697006A
Authority
GB
United Kingdom
Prior art keywords
guide vanes
gas turbine
guide
turbine engines
water separating
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
GB1069250A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1069250A priority Critical patent/GB697006A/en
Publication of GB697006A publication Critical patent/GB697006A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

697,006. Gas turbine plant. BOYD, W., and ORR, J. L. April 25, 1951 [May 1, 1950], No. 10692/50. Classes 110(i) and 110(iii) In a gas turbine engine having an air intake and spaced guide vanes extending across the intake, the guide vanes are so constructed that the leading edge 18 of a guide vane and the trailing edge 19 of the next adjacent guide vane are in overlapping relationship throughout their length, the object being to separate out water particles carried by the airstream by means of the greater inertia of the water particles, and to deposit it on the surface of the guide vanes. The guide vanes in the air intake are structurally separate from the blades of the compressor of the engine. Means may be provided for effective removal of the water deposited on the guide vanes, for example by means of electrical resistance elements 20 embedded in the guide vane.
GB1069250A 1950-05-01 1950-05-01 Water separating guide vanes for gas turbine engines Expired GB697006A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1069250A GB697006A (en) 1950-05-01 1950-05-01 Water separating guide vanes for gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1069250A GB697006A (en) 1950-05-01 1950-05-01 Water separating guide vanes for gas turbine engines

Publications (1)

Publication Number Publication Date
GB697006A true GB697006A (en) 1953-09-16

Family

ID=9972532

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1069250A Expired GB697006A (en) 1950-05-01 1950-05-01 Water separating guide vanes for gas turbine engines

Country Status (1)

Country Link
GB (1) GB697006A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1728991A2 (en) 2005-05-31 2006-12-06 United Technologies Corporation Electrothermal inlet ice protection system
WO2011045373A1 (en) * 2009-10-16 2011-04-21 Snecma Gas turbine engine air intake in a nacelle
FR2951504A1 (en) * 2009-10-16 2011-04-22 Snecma Gas turbine engine and nacelle assembly for e.g. helicopter, has secondary deflecting channel shaped such that flow velocity of air increases from upstream to downstream, where channel has outlet with opening leading into wall of nacelle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1728991A2 (en) 2005-05-31 2006-12-06 United Technologies Corporation Electrothermal inlet ice protection system
EP1728991A3 (en) * 2005-05-31 2009-09-30 United Technologies Corporation Electrothermal inlet ice protection system
US8366047B2 (en) 2005-05-31 2013-02-05 United Technologies Corporation Electrothermal inlet ice protection system
WO2011045373A1 (en) * 2009-10-16 2011-04-21 Snecma Gas turbine engine air intake in a nacelle
FR2951504A1 (en) * 2009-10-16 2011-04-22 Snecma Gas turbine engine and nacelle assembly for e.g. helicopter, has secondary deflecting channel shaped such that flow velocity of air increases from upstream to downstream, where channel has outlet with opening leading into wall of nacelle
US9091207B2 (en) 2009-10-16 2015-07-28 Snecma Gas turbine engine air intake in a nacelle

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