GB681186A - Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor - Google Patents

Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor

Info

Publication number
GB681186A
GB681186A GB2702149A GB2702149A GB681186A GB 681186 A GB681186 A GB 681186A GB 2702149 A GB2702149 A GB 2702149A GB 2702149 A GB2702149 A GB 2702149A GB 681186 A GB681186 A GB 681186A
Authority
GB
United Kingdom
Prior art keywords
blade
compressor
embedded
electrodes
rotor
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
GB2702149A
Inventor
Albert George Elliott
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 GB2702149A priority Critical patent/GB681186A/en
Publication of GB681186A publication Critical patent/GB681186A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating 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)

Abstract

681,186. Electrically heated compressor blade. ROLLS-ROYCE, Ltd. Oct. 20, 1950 [Oct. 20, 1949], No. 27021/49. Class 39(iii) [Also in Group XXVI]. An anti-icing blade for a compressor is hollow and is wholly filled with conductive rubber 7, e.g. graphited rubber or similar homogenous material, e.g. graphite of low electric conductivity with one or more wire electrodes 8 embedded therein for passage of current therethrough. The stator blades 3a, 3b and the rotor blades 4a, 4b are of sheet metal or are cast and are closed at the tip and open at the base. An electrode 8 is embedded in the conductive rubber in each rotor blade, and current is fed thereto through a conductor ring 10 mounted. on but insulated from the rotating disc 5a, which carries a second conductor ring 11, so that the wall of the blade forms the other electrode. In the stator blade, two electrodes 13 are embedded in the conductive rubber 7, which is insulated from the blade by cement. The electrodes 13 are connected to terminals 16 on an insulating plug 17 in the stator casing 1. Current may be supplied from an A.C. generator having an armature winding on the compressor rotor and a fixed field portion, the output from which may be directly wired to the rotor blading. The generator may have a rotating field portion and a stationary ..armature, the latter being wired directly to the stator blades. The embedded electrodes may be positioned or shaped to give a desired heat distribution to the blade, e.g. by placing it near the leading edge of the blade. The compressor may be of the axial flow or centrifugal kind.
GB2702149A 1949-10-20 1949-10-20 Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor Expired GB681186A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2702149A GB681186A (en) 1949-10-20 1949-10-20 Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2702149A GB681186A (en) 1949-10-20 1949-10-20 Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor

Publications (1)

Publication Number Publication Date
GB681186A true GB681186A (en) 1952-10-22

Family

ID=10252878

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2702149A Expired GB681186A (en) 1949-10-20 1949-10-20 Improvements in or relating to compressor systems having electrically heated blades and to blading elements therefor

Country Status (1)

Country Link
GB (1) GB681186A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1009436B (en) * 1953-03-27 1957-05-29 Daimler Benz Ag Cooling and de-icing device for gas turbines
USB451248I5 (en) * 1974-03-14 1976-03-02
US7131815B2 (en) 2003-07-11 2006-11-07 Rolls-Royce Plc Inlet guide vane
WO2011008333A1 (en) * 2009-06-30 2011-01-20 General Electric Company Heated guide vane
CN102410088A (en) * 2011-12-22 2012-04-11 中国船舶重工集团公司第七�三研究所 Adjustable guide vane system of gas turbine power turbine
US9642190B2 (en) * 2015-05-29 2017-05-02 Philip Jarvinen Embedded turbofan deicer system
US11021259B1 (en) 2021-01-07 2021-06-01 Philip Onni Jarvinen Aircraft exhaust mitigation system and process
CN115013071A (en) * 2021-03-05 2022-09-06 通用电气公司 Gas turbine engine rotor blade retention system

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1009436B (en) * 1953-03-27 1957-05-29 Daimler Benz Ag Cooling and de-icing device for gas turbines
USB451248I5 (en) * 1974-03-14 1976-03-02
US3997758A (en) * 1974-03-14 1976-12-14 Westinghouse Electric Corporation Moisture control device for steam turbines
US7131815B2 (en) 2003-07-11 2006-11-07 Rolls-Royce Plc Inlet guide vane
WO2011008333A1 (en) * 2009-06-30 2011-01-20 General Electric Company Heated guide vane
CN102410088A (en) * 2011-12-22 2012-04-11 中国船舶重工集团公司第七�三研究所 Adjustable guide vane system of gas turbine power turbine
CN102410088B (en) * 2011-12-22 2013-08-28 中国船舶重工集团公司第七�三研究所 Adjustable guide vane system of gas turbine power turbine
US9642190B2 (en) * 2015-05-29 2017-05-02 Philip Jarvinen Embedded turbofan deicer system
US11021259B1 (en) 2021-01-07 2021-06-01 Philip Onni Jarvinen Aircraft exhaust mitigation system and process
CN115013071A (en) * 2021-03-05 2022-09-06 通用电气公司 Gas turbine engine rotor blade retention system
US20220282626A1 (en) * 2021-03-05 2022-09-08 General Electric Company Rotor blade retention system for a gas turbine engine
US11519278B2 (en) * 2021-03-05 2022-12-06 General Electric Company Rotor blade retention system for a gas turbine engine

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