GB640052A - Improvements in and relating to combustion turbines - Google Patents

Improvements in and relating to combustion turbines

Info

Publication number
GB640052A
GB640052A GB3276547A GB3276547A GB640052A GB 640052 A GB640052 A GB 640052A GB 3276547 A GB3276547 A GB 3276547A GB 3276547 A GB3276547 A GB 3276547A GB 640052 A GB640052 A GB 640052A
Authority
GB
United Kingdom
Prior art keywords
shaft
shafts
turbine
bearings
supported
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
GB3276547A
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 GB3276547A priority Critical patent/GB640052A/en
Publication of GB640052A publication Critical patent/GB640052A/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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Abstract

640,052. Universal joints; shafts. KOLB, P., and HRYNISZAK, W. Dec. 12, 1947, No. 32765 [Class 80(ii)] [Also in Group XXVI] A gas turbine rotor 3 drives an output shaft 8 through reduction gearing 6 and, to prevent vibrations being transmitted from the gears back to the turbine, the turbine drive includes a torsionally flexible element. The turbine shaft 9 is supported in bearings 11 and the shaft 10, which car ries the gear pinion 6 is supported in bearings 12. The two shafts are hollow and are drivingly connected by a quill shaft 13 which is splined to the shafts 9, 10 at 14. Specification 641,377, [Group XXVI], is referred to.
GB3276547A 1947-12-12 1947-12-12 Improvements in and relating to combustion turbines Expired GB640052A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3276547A GB640052A (en) 1947-12-12 1947-12-12 Improvements in and relating to combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3276547A GB640052A (en) 1947-12-12 1947-12-12 Improvements in and relating to combustion turbines

Publications (1)

Publication Number Publication Date
GB640052A true GB640052A (en) 1950-07-12

Family

ID=10343666

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3276547A Expired GB640052A (en) 1947-12-12 1947-12-12 Improvements in and relating to combustion turbines

Country Status (1)

Country Link
GB (1) GB640052A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2381945A1 (en) * 1977-02-24 1978-09-22 Gen Motors Corp HEAT RECOVERY DRIVE DEVICE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2381945A1 (en) * 1977-02-24 1978-09-22 Gen Motors Corp HEAT RECOVERY DRIVE DEVICE

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