IT1058337B - Perfezionamenti in o relativi al montaggio di motori a turbina a gas a by pass su aeromobili - Google Patents

Perfezionamenti in o relativi al montaggio di motori a turbina a gas a by pass su aeromobili

Info

Publication number
IT1058337B
IT1058337B IT3078475A IT3078475A IT1058337B IT 1058337 B IT1058337 B IT 1058337B IT 3078475 A IT3078475 A IT 3078475A IT 3078475 A IT3078475 A IT 3078475A IT 1058337 B IT1058337 B IT 1058337B
Authority
IT
Italy
Prior art keywords
casing
engine
mounting
jet engines
plane
Prior art date
Application number
IT3078475A
Other languages
English (en)
Original Assignee
Rolls Royce 1971 Ltd
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 GB55768/74A external-priority patent/GB1516980A/en
Application filed by Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1058337B publication Critical patent/IT1058337B/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT3078475A 1974-12-24 1975-12-24 Perfezionamenti in o relativi al montaggio di motori a turbina a gas a by pass su aeromobili IT1058337B (it)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB55768/74A GB1516980A (en) 1974-12-24 1974-12-24 Mounting ducted fan gas turbine engines on aircraft
GB5576875 1975-12-10

Publications (1)

Publication Number Publication Date
IT1058337B true IT1058337B (it) 1982-04-10

Family

ID=26267572

Family Applications (1)

Application Number Title Priority Date Filing Date
IT3078475A IT1058337B (it) 1974-12-24 1975-12-24 Perfezionamenti in o relativi al montaggio di motori a turbina a gas a by pass su aeromobili

Country Status (1)

Country Link
IT (1) IT1058337B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230182912A1 (en) * 2021-12-09 2023-06-15 Rolls-Royce Plc Support structure for attaching a gas turbine engine to an aircraft pylon

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230182912A1 (en) * 2021-12-09 2023-06-15 Rolls-Royce Plc Support structure for attaching a gas turbine engine to an aircraft pylon
US11945595B2 (en) * 2021-12-09 2024-04-02 Rolls-Royce Plc Support structure for attaching a gas turbine engine to an aircraft pylon

Similar Documents

Publication Publication Date Title
GB1516980A (en) Mounting ducted fan gas turbine engines on aircraft
ZA777122B (en) Inlet air cleaner assembly for turbine engines
BE854751A (fr) Assemblage de pales de rotor en ceramique pour moteur a turbine a gaz
GB2044358B (en) Gas turbine jet engine mounting
IT8222040A0 (it) Propulsore composito particolarmente applicabile a turbomotori a gas.
GB2186918B (en) Propeller module for an aero gas turbine engine
GB2043796B (en) Bladed rotor for gas turbine engine
GB2254378B (en) Gas turbine engine ring shroud ring mounting
GB1549422A (en) Axial flow gas turbine engine compressor
DE3371927D1 (de) Diffuser for gas turbine engine
GB2129498B (en) Mounting system for two coupled turboshaft gas turbine engines
GB1236917A (en) Improvements in or relating to means for supporting a gas turbine engine in an aircraft
JPS5314215A (en) Thrust setting device for gas turbine engine
GB1077196A (en) Air intake duct for a gas turbine engine
IT8324164A0 (it) Perfezionamenti apportati alle prese d'aria di motori a turbina agas montati su aeromobili.
IT1058337B (it) Perfezionamenti in o relativi al montaggio di motori a turbina a gas a by pass su aeromobili
SU1009150A1 (ru) Регулируемое сверхзвуковое сопло газотурбинного двигателя
JPS57198348A (en) Thrust reversal/exhaust gas nozzle assemblage for gas turbine engine
GB1024894A (en) Improvements in aircraft jet-propulsion power-plants
GB1542642A (en) Thrust reverser for by-pass gas turbine engine
GB1470146A (en) Aircraft with an encased pusher propeller
GB1424552A (en) Inlet structure for turbine
JPS52144511A (en) Bypass gas turbine aircraft engine
IT7847993A0 (it) Perfezionamento nelle pompe da vuoto adatte al montaggio su motori diveicoli
SU270403A1 (ru) Узел креплени вспомогательных агрегатов