GB711719A - Improvements in aircraft equipped with a propelling motor at the rear - Google Patents
Improvements in aircraft equipped with a propelling motor at the rearInfo
- 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
Links
- 235000000396 iron Nutrition 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
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.
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)
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 |
-
1952
- 1952-02-27 GB GB5106/52A patent/GB711719A/en not_active Expired
Cited By (5)
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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