GB744920A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB744920A
GB744920A GB1329653A GB1329653A GB744920A GB 744920 A GB744920 A GB 744920A GB 1329653 A GB1329653 A GB 1329653A GB 1329653 A GB1329653 A GB 1329653A GB 744920 A GB744920 A GB 744920A
Authority
GB
United Kingdom
Prior art keywords
strips
gas turbine
relating
tablets
wall
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
GB1329653A
Inventor
Leslie James Pratt
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 GB1329653A priority Critical patent/GB744920A/en
Publication of GB744920A publication Critical patent/GB744920A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports

Abstract

744,920. Supporting and mounting bearings. ROLLS-ROYCE, Ltd. July 13, 1954 [May 12, 1953], No. 13296/53. Class 12 (1). [Also in Group XXVI] In a gas turbine engine, a bearing housing 54 downstream of the turbine motor disc is supported from the outer wall 63 of the exhaust duct structure by means of a series of strips 60 which are connected tangentially to the bearing housing. The strips have tablets 61 at their outer ends, the tablets being secured in holes in the wall 63. The strips are enclosed in aerofoil-section fairings 64 where they extend across the exhaust annulus. The bearing is cooled by air flowing through ports from the hollow shaft.
GB1329653A 1953-05-12 1953-05-12 Improvements in or relating to gas turbine engines Expired GB744920A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1329653A GB744920A (en) 1953-05-12 1953-05-12 Improvements in or relating to gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1329653A GB744920A (en) 1953-05-12 1953-05-12 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
GB744920A true GB744920A (en) 1956-02-15

Family

ID=10020374

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1329653A Expired GB744920A (en) 1953-05-12 1953-05-12 Improvements in or relating to gas turbine engines

Country Status (1)

Country Link
GB (1) GB744920A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877623A (en) * 1956-11-27 1959-03-17 Klompas Nicholas Annular fairing structure for the rear frame housing of a gas turbine engine
US2938336A (en) * 1956-12-06 1960-05-31 United Aircraft Corp Gas flow straightening vanes
FR2355163A1 (en) * 1976-06-17 1978-01-13 United Technologies Corp TURBINE CONSTRUCTION
GB2229229A (en) * 1988-12-16 1990-09-19 Gen Electric A jet engine subassembly
EP1428985A1 (en) * 2002-12-09 2004-06-16 Mitsubishi Heavy Industries, Ltd. Gas turbine
JP2013520609A (en) * 2010-02-25 2013-06-06 ターボメカ Flexible rear bearing mount with protrusions for turbine engines

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877623A (en) * 1956-11-27 1959-03-17 Klompas Nicholas Annular fairing structure for the rear frame housing of a gas turbine engine
US2938336A (en) * 1956-12-06 1960-05-31 United Aircraft Corp Gas flow straightening vanes
FR2355163A1 (en) * 1976-06-17 1978-01-13 United Technologies Corp TURBINE CONSTRUCTION
GB2229229A (en) * 1988-12-16 1990-09-19 Gen Electric A jet engine subassembly
GB2229229B (en) * 1988-12-16 1992-08-19 Gen Electric Jet engine turbine support
EP1428985A1 (en) * 2002-12-09 2004-06-16 Mitsubishi Heavy Industries, Ltd. Gas turbine
US7410343B2 (en) 2002-12-09 2008-08-12 Mitsubishi Heavy Industries, Ltd. Gas turbine
JP2013520609A (en) * 2010-02-25 2013-06-06 ターボメカ Flexible rear bearing mount with protrusions for turbine engines

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