GB1375868A – – Google Patents
GB1375868A – – Google Patents
Info
Publication number
GB1375868A
GB1375868A
GB3206971A
GB3206971A
GB1375868A
GB 1375868 A
GB1375868 A
GB 1375868A
GB 3206971 A
GB3206971 A
GB 3206971A
GB 3206971 A
GB3206971 A
GB 3206971A
GB 1375868 A
GB1375868 A
GB 1375868A
Authority
GB
United Kingdom
Prior art keywords
cowl
pylon
bolted
gas turbine
rigid member
Prior art date
1972-09-22
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
GB3206971A
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.)
1972-09-22
Filing date
1972-09-22
Publication date
1974-11-27
1972-09-22
Application filed
filed
Critical
1972-09-22
Priority to GB3206971A
priority
Critical
patent/GB1375868A/en
1974-11-27
Publication of GB1375868A
publication
Critical
patent/GB1375868A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
Classifications
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
B64D27/02—Aircraft characterised by the type or position of power plant
B64D27/16—Aircraft characterised by the type or position of power plant of jet type
B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
Abstract
1375868 Cowls for gas turbine power plants ROLLS-ROYCE (1971) Ltd 22 Sept 1972 [8 July 1971] 32069/71 Heading B7G A gas turbine power plant 16 has a streamlined cowl which is divided into at least two portions 22, 26, the or each division being in a plane normal to the cowl axis, and a rigid member 12 which is fixed to a vehicle, one of the cowl portions 26 is adapted for movement relative to the rigid member in directions axially of the cowl, into and out of locking engagement with the rigid member 12 and one other cowl portion 22. In the illustrated embodiment the power plant, which is a gas turbine of either the ducted fan or pure jet type, is suspended from the wing 10 of an aircraft by means of a pylon 12. The cowl portion 22 is bolted at a single point 24 to the pylon, and the remaining cowl portion 26 is slotted at the top along its full length, the walls of the slot being provided with rollers (32), Fig. 6 (not shown), which engage in slots 36 in the sides of the pylon. The engine is rigidly connected to the pylon by means of a connecting wedge 14, and the cowl portions are bolted to each other and to the pylon, nowhere is the cowl connected to the engine. When the cowl portion 26 has been bolted in position small access doors in the top thereof are opened, and the rollers (32) brought out of contact with the rails 36.
GB3206971A
1972-09-22
1972-09-22
Expired
GB1375868A
(en)
Priority Applications (1)
Application Number
Priority Date
Filing Date
Title
GB3206971A
GB1375868A
(en)
1972-09-22
1972-09-22
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
GB3206971A
GB1375868A
(en)
1972-09-22
1972-09-22
Publications (1)
Publication Number
Publication Date
GB1375868A
true
GB1375868A
(en)
1974-11-27
Family
ID=10332710
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB3206971A
Expired
GB1375868A
(en)
1972-09-22
1972-09-22
Country Status (1)
Country
Link
GB
(1)
GB1375868A
(en)
Cited By (8)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US4043522A
(en)
*
1975-12-22
1977-08-23
The Boeing Company
Common pod for housing a plurality of different turbofan jet propulsion engines
GB2225060A
(en)
*
1988-09-28
1990-05-23
Short Brothers Plc
Ducted fan turbine engine
WO1994016945A1
(en)
*
1993-01-26
1994-08-04
Short Brothers Plc
An aircraft propulsive power unit
US6179249B1
(en)
*
1996-12-26
2001-01-30
Aerospatiale Societe Nationale Industrielle
Turbojet pod with laminar flow
EP1918203A1
(en)
*
2006-10-31
2008-05-07
Airbus Espana, S.L.
Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
FR2916737A1
(en)
*
2007-06-01
2008-12-05
Airbus France Sas
AIRCRAFT ENGINE ASSEMBLY WITH SLIDING CARGO.
JP2012510021A
(en)
*
2008-11-26
2012-04-26
エムアールエイ・システムズ・インコーポレイテッド
Nacelle and assembly method thereof
WO2019122753A1
(en)
*
2017-12-22
2019-06-27
Safran Nacelles
Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle
1972
1972-09-22
GB
GB3206971A
patent/GB1375868A/en
not_active
Expired
Cited By (14)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US4043522A
(en)
*
1975-12-22
1977-08-23
The Boeing Company
Common pod for housing a plurality of different turbofan jet propulsion engines
GB2225060A
(en)
*
1988-09-28
1990-05-23
Short Brothers Plc
Ducted fan turbine engine
US5136839A
(en)
*
1988-09-28
1992-08-11
Short Brothers Plc
Ducted fan turbine engine
GB2225060B
(en)
*
1988-09-28
1993-03-24
Short Brothers Plc
Ducted fan turbine engine
WO1994016945A1
(en)
*
1993-01-26
1994-08-04
Short Brothers Plc
An aircraft propulsive power unit
GB2274490B
(en)
*
1993-01-26
1996-09-18
Short Brothers Plc
An aircraft propulsive power unit
US5609313A
(en)
*
1993-01-26
1997-03-11
Short Brothers Plc
Aircraft propulsive power unit
US6179249B1
(en)
*
1996-12-26
2001-01-30
Aerospatiale Societe Nationale Industrielle
Turbojet pod with laminar flow
EP1918203A1
(en)
*
2006-10-31
2008-05-07
Airbus Espana, S.L.
Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
FR2916737A1
(en)
*
2007-06-01
2008-12-05
Airbus France Sas
AIRCRAFT ENGINE ASSEMBLY WITH SLIDING CARGO.
JP2012510021A
(en)
*
2008-11-26
2012-04-26
エムアールエイ・システムズ・インコーポレイテッド
Nacelle and assembly method thereof
WO2019122753A1
(en)
*
2017-12-22
2019-06-27
Safran Nacelles
Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle
FR3075886A1
(en)
*
2017-12-22
2019-06-28
Safran Nacelles
TURBOJET NACELLE COMPRISING HOOD OPENINGS BEFORE ACCESSING NACELLE FASTENING POINTS
US11454194B2
(en)
2017-12-22
2022-09-27
Safran Nacelles
Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle
Similar Documents
Publication
Publication Date
Title
GB1318748A
(en)
1973-05-31
Gas turgine ducted fan engines for aircraft
GB937829A
(en)
1963-09-25
Deflector assembly defining convergent nozzles
GB1066360A
(en)
1967-04-26
Aircraft
GB1069033A
(en)
1967-05-17
Improvements in or relating to gas turbine jet propulsion engines
GB1104764A
(en)
1968-02-28
Improvements in thrust reverters for jet propulsion powerplants
GB1040510A
(en)
1966-08-24
Improvements in jet propulsion engines having thrust deflectors
GB1172782A
(en)
1969-12-03
Lift Fan Installations for Vertical Take Off and Landing Aircraft.
GB1085619A
(en)
1967-10-04
Gas turbine engine
GB1375868A
(en)
1974-11-27
GB1079296A
(en)
1967-08-16
A system and method for generating lift of aircraft
GB1012832A
(en)
1965-12-08
Improvements in or relating to vertical take off and landing aircraft
GB1501044A
(en)
1978-02-15
Airplanes having fuselage housed thrust-reversable power plant installations
GB1170809A
(en)
1969-11-19
Discharge Nozzle Apparatus for Jet Aircraft
GB1024894A
(en)
1966-04-06
Improvements in aircraft jet-propulsion power-plants
GB1166396A
(en)
1969-10-08
Improvements in Power Plant with Thrust Reverser.
GB1033583A
(en)
1966-06-22
Thrust reverser for a jet propulsion engine
GB1272836A
(en)
1972-05-03
Gas turbine engines
GB965371A
(en)
1964-07-29
Improvements in and relating to supersonic aircraft
GB1357370A
(en)
1974-06-19
Ducted fan gas turbine jet propulsion engine with thrust control means
GB1030521A
(en)
1966-05-25
Mounting arrangement for gas turbine engines in aircraft
GB1071075A
(en)
1967-06-07
Improvements in aircraft
GB1140472A
(en)
1969-01-22
Articulated structure especially for jet propulsion nozzle
GB1210939A
(en)
1970-11-04
An aircraft jet propulsion engine incorporating a nozzle having a thrust-directing arrangement
GB1148034A
(en)
1969-04-10
Gas turbine power plant
GB886201A
(en)
1962-01-03
Jet noise silencer for an aircraft
Legal Events
Date
Code
Title
Description
1975-04-09
PS
Patent sealed
1980-04-30
PCNP
Patent ceased through non-payment of renewal fee
