GB1228297A - - Google Patents

Info

Publication number
GB1228297A
GB1228297A GB1228297DA GB1228297A GB 1228297 A GB1228297 A GB 1228297A GB 1228297D A GB1228297D A GB 1228297DA GB 1228297 A GB1228297 A GB 1228297A
Authority
GB
United Kingdom
Prior art keywords
engine
ring gear
teeth
shaft
alternator
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
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 filed Critical
Publication of GB1228297A publication Critical patent/GB1228297A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H1/00Toothed gearings for conveying rotary motion
    • F16H1/28Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H1/46Systems consisting of a plurality of gear trains each with orbital gears, i.e. systems having three or more central gears
    • 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275Mechanical drives
    • F02C7/277Mechanical drives the starter being a separate turbine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N15/00Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00 - F02N13/00

Landscapes

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

Abstract

1,228,297. Engine turning gear. GARRETT CORP. Sept.16, 1969, No.45683/69. Heading F1K. [Also in Division F2] Transmission gearing between a starter and a gas turbine engine includes a planetary train having a ring gear 23 Fig. 1 or 60 Fig. 2 associated with a one-way detent which holds the ring gear during starting but becomes inoperative when the ring gear rotates in its permitted direction above a predetermined speed, i.e. when the engine is self-sustaining, to prevent wear and drag in the detent during normal engine running. The detent comprises ratchet pawls 35 Fig. 1A pivoted to the ring gear 23, each with a nose 36 urged by a spring 38 into engagement with fixed ratchet teeth 37. When the ring gear rotates anti-clockwise above the predetermined speed, centrifugal action on the tail 40 of the pawl overcome the spring 38 to move the nose 36 clear of the ratchet teeth 37. In Fig. 1, a constant speed drive to an alternator (not shown) is provided by combining inputs from a gas turbine engine (not shown) and an air turbine starter motor 10 the inlet guide vanes 13 of which are controlled in accordance with alternator and engine speeds. A planet carrier 21 splined to the engine shaft 28 carries a first set of stepped planets 20 having teeth 19 meshing a sun gear 18 on the air turbine shaft 17 and teeth 22 meshing internal teeth of a ring 23d splined to an annulus 23a, and a second set of stepped planets 26 having teeth 32 meshing teeth 23c of the annulus 23a and teeth 33 meshing a sun gear 34 on an alternator drive-shaft. For engine starting, the air turbine motor 10 drives the engine shaft, the annulus 23 being held stationary by the one-way detent 35, 37. When the engine is self-sustaining, the air supply to the motor 10 is reduced, the two power sources then driving the alternator conjointly, with the ring gear 23 rotating freely anti-clockwise Fig. 1A. In Fig. 2, an air turbine starter motor 47 is connected to an engine drive shaft 58 by gearing comprising a pinion 48 on the air turbine shaft, idlers 50 mounted in the casing 42, a ring gear 52 coupled to a sum pinion 53, and planets 56 in a carrier 57 rigid with the shaft 58. The planets mesh a ring gear 60 held by a one-way detent during starting. (For Figures see next page)
GB1228297D 1969-09-16 1969-09-16 Expired GB1228297A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4568369 1969-09-16

Publications (1)

Publication Number Publication Date
GB1228297A true GB1228297A (en) 1971-04-15

Family

ID=10438153

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1228297D Expired GB1228297A (en) 1969-09-16 1969-09-16

Country Status (2)

Country Link
FR (1) FR2064618A5 (en)
GB (1) GB1228297A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3376005A1 (en) * 2017-03-17 2018-09-19 Hamilton Sundstrand Corporation Air turbine starter with automated variable inlet vanes
GB2624170A (en) * 2022-11-08 2024-05-15 Rolls Royce Plc Rotary assembly
US11988100B2 (en) 2021-12-14 2024-05-21 Rolls-Royce Plc Blower assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2804173A (en) * 1955-07-20 1957-08-27 Radian Corp Turning device for rotatable body
US3307426A (en) * 1960-01-11 1967-03-07 Garrett Corp Constant speed drive starter
GB1119988A (en) * 1965-10-14 1968-07-17 Nat Res Dev Transmission system for interconnecting two rotary machines
FR1535875A (en) * 1966-09-02 1968-08-09 English Electric Co Ltd Transmission of a rotational movement

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3376005A1 (en) * 2017-03-17 2018-09-19 Hamilton Sundstrand Corporation Air turbine starter with automated variable inlet vanes
US10767564B2 (en) 2017-03-17 2020-09-08 Hamilton Sunstrand Corporation Air turbine starter with automated variable inlet vanes
US11988100B2 (en) 2021-12-14 2024-05-21 Rolls-Royce Plc Blower assembly
GB2624170A (en) * 2022-11-08 2024-05-15 Rolls Royce Plc Rotary assembly

Also Published As

Publication number Publication date
FR2064618A5 (en) 1971-07-23

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee