GB744695A - Improvements in static structures for jet propulsion engines - Google Patents

Improvements in static structures for jet propulsion engines

Info

Publication number
GB744695A
GB744695A GB21017/53A GB2101753A GB744695A GB 744695 A GB744695 A GB 744695A GB 21017/53 A GB21017/53 A GB 21017/53A GB 2101753 A GB2101753 A GB 2101753A GB 744695 A GB744695 A GB 744695A
Authority
GB
United Kingdom
Prior art keywords
compressor
annular
engine
wall
jet propulsion
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
GB21017/53A
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.)
MAX ADOLF MULLER
Original Assignee
MAX ADOLF MULLER
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 MAX ADOLF MULLER filed Critical MAX ADOLF MULLER
Priority to GB21017/53A priority Critical patent/GB744695A/en
Publication of GB744695A publication Critical patent/GB744695A/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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • 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)
  • Supercharger (AREA)

Abstract

744,695. Gas turbine jet propulsion plant. MULLER, M. A. July 29, 1953. No. 21017/53. Class 110(3) A gas turbine jet propulsion engine of the by-pass type comprises an annular intake 3 at the front of the engine in which is disposed a pre-compressor 4, 5, the air from this compressor being divided into two streams 6, 12 by an annular wall 1. The inner air stream 6 passes to a main compressor 7 and then to combustion equipment 9 and turbine 10, the exhaust gases then discharging through the propulsion nozzle 11. The outer air stream flows through the annular passage 13 and then into guide tubes 14 which are disposed along the outer casing 15 of the main compressor 7 and are circumferentially spaced. This by-pass stream flowing through the tubes 14 passes directly to the propulsion nozzle 11. The driving gear 20b for the pre-compressor 4; 5 is contained within a wall 20a forming the inner wall of the: inner annular passage for the air-flow 6. The spaces between the guide tubes are utilized for accommodating combustion chambers 9 and engine auxiliaries 23 which are driven by means of gearing. The bearing 19 adjacent the turbine wheel 10 is supported by means of adjustable rods 18 from an annular ring 17.
GB21017/53A 1953-07-29 1953-07-29 Improvements in static structures for jet propulsion engines Expired GB744695A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21017/53A GB744695A (en) 1953-07-29 1953-07-29 Improvements in static structures for jet propulsion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21017/53A GB744695A (en) 1953-07-29 1953-07-29 Improvements in static structures for jet propulsion engines

Publications (1)

Publication Number Publication Date
GB744695A true GB744695A (en) 1956-02-15

Family

ID=10155785

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21017/53A Expired GB744695A (en) 1953-07-29 1953-07-29 Improvements in static structures for jet propulsion engines

Country Status (1)

Country Link
GB (1) GB744695A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005005810A1 (en) * 2003-07-08 2005-01-20 Rolls-Royce Plc Aircraft turbine engine arrangement
AU2013325122B2 (en) * 2012-09-28 2015-10-08 Lunair Pty Limited Thrust propulsion system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005005810A1 (en) * 2003-07-08 2005-01-20 Rolls-Royce Plc Aircraft turbine engine arrangement
US7484354B2 (en) 2003-07-08 2009-02-03 Rolls-Royce Plc Aircraft engine arrangement
AU2013325122B2 (en) * 2012-09-28 2015-10-08 Lunair Pty Limited Thrust propulsion system
CN105209741A (en) * 2012-09-28 2015-12-30 卢奈尔私人有限公司 Thrust propulsion system
WO2014047694A3 (en) * 2012-09-28 2016-07-07 Lunothrust Pty. Ltd. Thrust propulsion system
CN105209741B (en) * 2012-09-28 2017-05-17 卢奈尔私人有限公司 thrust propulsion system

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