GB820605A - Improvements in and relating to the driving of auxiliaries of combustion turbine engines - Google Patents

Improvements in and relating to the driving of auxiliaries of combustion turbine engines

Info

Publication number
GB820605A
GB820605A GB33407/57A GB3340757A GB820605A GB 820605 A GB820605 A GB 820605A GB 33407/57 A GB33407/57 A GB 33407/57A GB 3340757 A GB3340757 A GB 3340757A GB 820605 A GB820605 A GB 820605A
Authority
GB
United Kingdom
Prior art keywords
teeth
shaft
mesh
bevel
gear
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
GB33407/57A
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.)
Blackburn and General Aircraft Ltd
Original Assignee
Blackburn and General Aircraft 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 Blackburn and General Aircraft Ltd filed Critical Blackburn and General Aircraft Ltd
Priority to GB33407/57A priority Critical patent/GB820605A/en
Publication of GB820605A publication Critical patent/GB820605A/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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gear Transmission (AREA)

Abstract

820,605. Gas turbine plant. BLACKBURN & GENERAL AIRCRAFT Ltd., COUPE, N. P., and LITTLEFOLD, F. Oct. 25, 1957, No. 33407/57. Class 110 (3). The auxiliaries drive from the shaft of a small combustion turbine engine comprises spur teeth integral or fast with the engine shaft which mesh with the teeth of a double planet-wheel, the smaller gear of which meshes with the internal teeth of a flanged drum mounted concentric with the engine shaft and terminating with bevel gear-teeth which mesh with a bevel-wheel on an output shaft. The engine shaft 1 has spur teeth 2, integral or fast with the shaft, which mesh with the teeth 3 of a double planet wheel of which the smaller ring of teeth 4 mesh with the internal teeth 5 on the rim of a flanged drum 6. This drum, which is supported by bearings 7, 8 concentric with the shaft 1, terminates in bevel gear teeth 9 which mesh with one or more bevel-wheels 10 on radial driveshafts 11. The shafts 11 drive the auxiliaries through bevel gearing 12, 13. The engine shaft 1 may be extended at 1<1> to drive a gear-box or other equipment forwardly of the auxiliary drive-shafts. The reduction gear may be contained in a bullet casing 14 supported by struts 15 through which the shafts 11 may extend.
GB33407/57A 1957-10-25 1957-10-25 Improvements in and relating to the driving of auxiliaries of combustion turbine engines Expired GB820605A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33407/57A GB820605A (en) 1957-10-25 1957-10-25 Improvements in and relating to the driving of auxiliaries of combustion turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33407/57A GB820605A (en) 1957-10-25 1957-10-25 Improvements in and relating to the driving of auxiliaries of combustion turbine engines

Publications (1)

Publication Number Publication Date
GB820605A true GB820605A (en) 1959-09-23

Family

ID=10352544

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33407/57A Expired GB820605A (en) 1957-10-25 1957-10-25 Improvements in and relating to the driving of auxiliaries of combustion turbine engines

Country Status (1)

Country Link
GB (1) GB820605A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2151707A (en) * 1983-12-09 1985-07-24 Teledyne Ind Accessory drive for a turbine engine
WO2002099263A1 (en) * 2001-06-05 2002-12-12 Volvo Aero Corporation Gas turbine arrangement

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2151707A (en) * 1983-12-09 1985-07-24 Teledyne Ind Accessory drive for a turbine engine
WO2002099263A1 (en) * 2001-06-05 2002-12-12 Volvo Aero Corporation Gas turbine arrangement

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