GB2244526B - Compressor blade in a turbine engine. - Google Patents

Compressor blade in a turbine engine.

Info

Publication number
GB2244526B
GB2244526B GB9112321A GB9112321A GB2244526B GB 2244526 B GB2244526 B GB 2244526B GB 9112321 A GB9112321 A GB 9112321A GB 9112321 A GB9112321 A GB 9112321A GB 2244526 B GB2244526 B GB 2244526B
Authority
GB
United Kingdom
Prior art keywords
turbine engine
compressor blade
compressor
blade
turbine
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 - Lifetime
Application number
GB9112321A
Other versions
GB9112321D0 (en
GB2244526A (en
Inventor
Seigfried Sikorski
R Werner Huther
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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
Priority claimed from DE19873718678 external-priority patent/DE3718678A1/en
Application filed by MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB9112321D0 publication Critical patent/GB9112321D0/en
Publication of GB2244526A publication Critical patent/GB2244526A/en
Application granted granted Critical
Publication of GB2244526B publication Critical patent/GB2244526B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9112321A 1987-06-04 1991-06-07 Compressor blade in a turbine engine. Expired - Lifetime GB2244526B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19873718678 DE3718678A1 (en) 1987-06-04 1987-06-04 FIBER TECHNICAL COMPRESSOR VAN
GB8812721A GB2208125B (en) 1987-06-04 1988-05-27 Mounting a fibre-technology formed rotor blade.

Publications (3)

Publication Number Publication Date
GB9112321D0 GB9112321D0 (en) 1991-07-24
GB2244526A GB2244526A (en) 1991-12-04
GB2244526B true GB2244526B (en) 1992-02-26

Family

ID=25856284

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9112321A Expired - Lifetime GB2244526B (en) 1987-06-04 1991-06-07 Compressor blade in a turbine engine.

Country Status (1)

Country Link
GB (1) GB2244526B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5680172A (en) * 1992-01-21 1997-10-21 Video Post & Transfer, Inc. Consecutive frame scanning of cinematographic film
GB2518643B (en) * 2013-09-26 2016-06-08 Ge Aviat Systems Ltd Propeller assembly and propeller blade retention assembly

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2832098A1 (en) * 1978-07-21 1980-01-31 Messerschmitt Boelkow Blohm ARRANGEMENT FOR TRAIN OR LENGTH FORCE INTRODUCTION TO A SANDWICH DESIGN COMPONENT
EP0284778A2 (en) * 1987-03-28 1988-10-05 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Fan blade, particularly for prop-fan engines

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2832098A1 (en) * 1978-07-21 1980-01-31 Messerschmitt Boelkow Blohm ARRANGEMENT FOR TRAIN OR LENGTH FORCE INTRODUCTION TO A SANDWICH DESIGN COMPONENT
EP0284778A2 (en) * 1987-03-28 1988-10-05 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Fan blade, particularly for prop-fan engines

Also Published As

Publication number Publication date
GB9112321D0 (en) 1991-07-24
GB2244526A (en) 1991-12-04

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Legal Events

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

Effective date: 19940527