GB711719A - Improvements in aircraft equipped with a propelling motor at the rear - Google Patents

Improvements in aircraft equipped with a propelling motor at the rear

Info

Publication number
GB711719A
GB711719A GB5106/52A GB510652A GB711719A GB 711719 A GB711719 A GB 711719A GB 5106/52 A GB5106/52 A GB 5106/52A GB 510652 A GB510652 A GB 510652A GB 711719 A GB711719 A GB 711719A
Authority
GB
United Kingdom
Prior art keywords
fuselage
engine
bolted
aircraft equipped
propelling motor
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
GB5106/52A
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.)
SNCAN
Original Assignee
SNCAN
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 SNCAN filed Critical SNCAN
Publication of GB711719A publication Critical patent/GB711719A/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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/06—Fins
    • 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Engines (AREA)

Abstract

711,719. Gas turbine plant. SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU NORD. Feb. 27, 1952 [Dec. 20, 1951], No. 5106/52. Class 110(3) [Also in Group XXXIII] A turbo jet engine 6, housed in the fuselage behind the cabin. is mounted by being slid on rollers 21 along angle irons 19 through the rear opening of the fuselage, and then bolted in position. In a modification, the engine is mounted higher in the fuselage, and may be lowered through doors in the top of the fuselage and bolted to supports which form a cradle for the engine.
GB5106/52A 1951-12-20 1952-02-27 Improvements in aircraft equipped with a propelling motor at the rear Expired GB711719A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR711719X 1951-12-20

Publications (1)

Publication Number Publication Date
GB711719A true GB711719A (en) 1954-07-07

Family

ID=9076912

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5106/52A Expired GB711719A (en) 1951-12-20 1952-02-27 Improvements in aircraft equipped with a propelling motor at the rear

Country Status (1)

Country Link
GB (1) GB711719A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944766A (en) * 1958-03-31 1960-07-12 Boeing Co Aircraft engine installation
DE1129833B (en) * 1959-11-24 1962-05-17 Messerschmitt Ag Airplane with an air-breathing jet engine in the fuselage tail
DE2550525A1 (en) * 1974-11-13 1976-05-20 Snecma DEVICE FOR ATTACHING A JET ENGINE TO AN AIRPLANE
FR2928137A1 (en) * 2008-02-29 2009-09-04 Airbus France Sas Auxiliary propulsion system for civil transport aircraft, has auxiliary reactor fixed to bearing structure, where structure has beams overhangingly assembled on part of their length along longitudinal direction of fuselage of aircraft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944766A (en) * 1958-03-31 1960-07-12 Boeing Co Aircraft engine installation
DE1129833B (en) * 1959-11-24 1962-05-17 Messerschmitt Ag Airplane with an air-breathing jet engine in the fuselage tail
DE2550525A1 (en) * 1974-11-13 1976-05-20 Snecma DEVICE FOR ATTACHING A JET ENGINE TO AN AIRPLANE
FR2928137A1 (en) * 2008-02-29 2009-09-04 Airbus France Sas Auxiliary propulsion system for civil transport aircraft, has auxiliary reactor fixed to bearing structure, where structure has beams overhangingly assembled on part of their length along longitudinal direction of fuselage of aircraft
US8220739B2 (en) 2008-02-29 2012-07-17 Airbus Operations Sas Beam mounted rear propulsion system for an aircraft and aircraft with such system

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