GB609956A - Improvements in or relating to mountings for internal combustion turbines - Google Patents

Improvements in or relating to mountings for internal combustion turbines

Info

Publication number
GB609956A
GB609956A GB9343/46A GB934346A GB609956A GB 609956 A GB609956 A GB 609956A GB 9343/46 A GB9343/46 A GB 9343/46A GB 934346 A GB934346 A GB 934346A GB 609956 A GB609956 A GB 609956A
Authority
GB
United Kingdom
Prior art keywords
engine
attached
casing
brackets
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
Application number
GB9343/46A
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
Publication of GB609956A publication Critical patent/GB609956A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • Y02T50/40—Weight reduction
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

609,956. Gas turbines; jet propulsion plant. LOMBARD, A. A. March 26, 1946, No. 9343. [Class 110 (iii)] [Also in Group XXV] A gas turbine or jet propulsion engine is attached to its supporting structure by two mountings arranged at different places along its length, one mounting comprising a linkage system connected to the supporting structure at at least two points and allowing the engine to turn about its axis and the other mounting providing no such freedom. The compressor casing 5, Fig. 4, of a gas turbine jet propulsion unit is attached to the ribs 11 of an aircraft wing by two trunnions 13 disposed at opposite sides of the compressor on a common horizontal axis transverse to the longitudinal axis of the engine. The trunnions locate the engine in the horizontal plane, but allow it to rock in the vertical plane. The turbine casing 6, Fig. 2, is attached to the ribs 11 by a pair of struts 20 which are articulated together at 23 and a pair of links 19 which are articulated to the struts 20 at 17 and to two brackets 22 attached to the casing 6. The point 23 is pivotally attached to the casing by a shackle 24 and the pivot points 17 to the ribs 11 by shackles 15. This arrangement allows the turbine casing to turn on its axis relative to the supporting structure so that no torsional loads due to deformation of the structure are imparted to the turbine plant. The shackles 15 are mounted on brackets 16 by pins 26 and the widths of the brackets are less than the free lengths of the pins so that the shackles can slide relative to the brackets to accommodate axial expansion of the engine.
GB9343/46A 1946-03-26 1946-03-26 Improvements in or relating to mountings for internal combustion turbines Expired GB609956A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB266016X 1946-03-26
GB100147X 1947-01-10

Publications (1)

Publication Number Publication Date
GB609956A true GB609956A (en) 1948-10-08

Family

ID=26247160

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9343/46A Expired GB609956A (en) 1946-03-26 1946-03-26 Improvements in or relating to mountings for internal combustion turbines

Country Status (3)

Country Link
CH (1) CH266016A (en)
FR (1) FR939980A (en)
GB (1) GB609956A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11542023B2 (en) 2018-01-15 2023-01-03 Lord Corporation Engine mount system and elements for reduced force transmission and reduced static motion and associated methods

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11542023B2 (en) 2018-01-15 2023-01-03 Lord Corporation Engine mount system and elements for reduced force transmission and reduced static motion and associated methods
US11787552B2 (en) 2018-01-15 2023-10-17 Lord Corporation Engine mount system and elements for reduced force transmission and reduced static motion

Also Published As

Publication number Publication date
CH266016A (en) 1949-12-31
FR939980A (en) 1948-11-30

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