SE8305904D0 - GONDOL WITH Laminated Flood - Google Patents
GONDOL WITH Laminated FloodInfo
- Publication number
- SE8305904D0 SE8305904D0 SE8305904A SE8305904A SE8305904D0 SE 8305904 D0 SE8305904 D0 SE 8305904D0 SE 8305904 A SE8305904 A SE 8305904A SE 8305904 A SE8305904 A SE 8305904A SE 8305904 D0 SE8305904 D0 SE 8305904D0
- Authority
- SE
- Sweden
- Prior art keywords
- nacelle
- leading edge
- chord
- intersection
- aft
- Prior art date
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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0226—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Structure Of Belt Conveyors (AREA)
Abstract
An improved nacelle is provided for housing an aircraft engine and reducing aerodynamic drag during aircraft operation. In one embodiment, the nacelle houses a gas turbine engine and forms the fan cowl 24 of a turbofan engine having a fan 16 and comprises a leading edge and a trailing edge, having a reference chord extending therebetween, and an outer surface which is continuous from the leading edge to the trailing edge. The outer surface includes a forward portion, an intermediate portion and an aft portion and has a profile defined by a varying thickness measured perpendicularly from the chord to the outer surface. The profile has a maximum thickness at the intersection of the forward and intermediate portions, which intersection is located greater than about 36% and probably at 56% of the chord from the leading edge, and is effective for increasing laminar flow over the nacelle for reducing aerodynamic drag. The flow is turbulent aft of the maximum thickness. <IMAGE>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US43758182A | 1982-10-29 | 1982-10-29 |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8305904D0 true SE8305904D0 (en) | 1983-10-27 |
SE8305904L SE8305904L (en) | 1984-04-30 |
SE456077B SE456077B (en) | 1988-09-05 |
Family
ID=23737028
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8305904A SE456077B (en) | 1982-10-29 | 1983-10-27 | AIRPLANE GONDOL WITH Laminated Flood |
Country Status (11)
Country | Link |
---|---|
JP (1) | JPS5996462A (en) |
AU (1) | AU555526B2 (en) |
CA (1) | CA1209354A (en) |
CH (1) | CH667434A5 (en) |
DE (1) | DE3338286A1 (en) |
GB (1) | GB2128945B (en) |
IL (1) | IL69906A (en) |
IT (1) | IT1171783B (en) |
NL (1) | NL8303716A (en) |
SE (1) | SE456077B (en) |
SU (1) | SU1391490A3 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920143B1 (en) * | 2007-08-20 | 2010-01-22 | Aircelle Sa | DEVICE FOR CONTROLLING HOUSING MAINTENANCE ACTUATORS OF A TURBOREACTOR NACELLE |
DE102009003084B4 (en) | 2009-05-13 | 2013-03-14 | Airbus Operations Gmbh | Cladding for a buoyancy aid |
GB2595724B (en) | 2020-06-05 | 2022-10-05 | Rolls Royce Plc | Nacelle for gas turbine engine and aircraft comprising the same |
FR3116043B1 (en) * | 2020-11-09 | 2023-04-28 | Safran Aircraft Engines | Aircraft propulsion unit nacelle air inlet to promote a thrust reversal phase |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1211192A (en) * | 1964-07-01 | 1970-11-04 | Gen Electric | Improvements in low drag exhaust nozzle and nacelle arrangement for turbofan engines |
US3765623A (en) * | 1971-10-04 | 1973-10-16 | Mc Donnell Douglas Corp | Air inlet |
US3952971A (en) * | 1971-11-09 | 1976-04-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Airfoil shape for flight at subsonic speeds |
IL42041A (en) * | 1972-05-04 | 1977-05-31 | Mc Donnell Douglas Corp | Low drag airfoils and method of designing same |
GB1554713A (en) * | 1975-03-04 | 1979-10-24 | Secr Defence | Wings |
GB1553816A (en) * | 1975-06-12 | 1979-10-10 | Secr Defence | Wings |
DE2712717A1 (en) * | 1977-03-23 | 1978-09-28 | Ver Flugtechnische Werke | ABOVE CRITICAL WING PROFILE |
US4209149A (en) * | 1977-12-27 | 1980-06-24 | Boeing Commercial Airplane Company | Contracted inlet for jet engine being transported as cargo |
FR2427249A1 (en) * | 1978-05-29 | 1979-12-28 | Aerospatiale | SAIL PROFILE FOR AIRCRAFT |
CA1185101A (en) * | 1980-03-03 | 1985-04-09 | Daniel J. Lahti | Drag-reducing nacelle |
DE3033101C2 (en) * | 1980-09-03 | 1984-11-22 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Arrangement for increasing the resulting propulsive force in aircraft |
-
1983
- 1983-09-12 AU AU19026/83A patent/AU555526B2/en not_active Ceased
- 1983-10-04 IL IL69906A patent/IL69906A/en unknown
- 1983-10-07 CA CA000438631A patent/CA1209354A/en not_active Expired
- 1983-10-14 JP JP58191060A patent/JPS5996462A/en active Granted
- 1983-10-18 SU SU833652711A patent/SU1391490A3/en active
- 1983-10-21 CH CH5734/83A patent/CH667434A5/en not_active IP Right Cessation
- 1983-10-21 DE DE19833338286 patent/DE3338286A1/en not_active Ceased
- 1983-10-24 GB GB08328400A patent/GB2128945B/en not_active Expired
- 1983-10-27 SE SE8305904A patent/SE456077B/en not_active IP Right Cessation
- 1983-10-27 IT IT23478/83A patent/IT1171783B/en active
- 1983-10-28 NL NL8303716A patent/NL8303716A/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
JPS5996462A (en) | 1984-06-02 |
IL69906A (en) | 1990-04-29 |
DE3338286A1 (en) | 1984-05-03 |
IT8323478A0 (en) | 1983-10-27 |
CA1209354A (en) | 1986-08-12 |
CH667434A5 (en) | 1988-10-14 |
AU555526B2 (en) | 1986-09-25 |
IT1171783B (en) | 1987-06-10 |
NL8303716A (en) | 1984-05-16 |
SE456077B (en) | 1988-09-05 |
GB2128945B (en) | 1986-03-26 |
GB2128945A (en) | 1984-05-10 |
AU1902683A (en) | 1984-05-03 |
SE8305904L (en) | 1984-04-30 |
JPH0344221B2 (en) | 1991-07-05 |
SU1391490A3 (en) | 1988-04-23 |
IL69906A0 (en) | 1984-01-31 |
GB8328400D0 (en) | 1983-11-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5058617A (en) | Nacelle inlet for an aircraft gas turbine engine | |
US9102397B2 (en) | Airfoils including tip profile for noise reduction and method for fabricating same | |
SE8203975L (en) | KOMPOUNDDRIVAGGREGAT | |
SE8204424L (en) | BERYTEBLAD | |
ES8706546A1 (en) | Duct for hot air. | |
GB1304678A (en) | ||
EP0995675A3 (en) | Method for reducing wave resistance in airplane | |
GB2279920A (en) | Nacelle apparatus for an airplane | |
US4799633A (en) | Laminar flow necelle | |
EP0940338A3 (en) | Gearbox breather outlet | |
SE8305904L (en) | GONDOL WITH Laminated Flood | |
GB2138507B (en) | Mounting and exhausting in turbo-propellor aircraft engines | |
Selig | The design of airfoils at low Reynolds numbers | |
GB849212A (en) | Supersonic aircraft | |
JPS5888499A (en) | Aerofoil of fan for overland car | |
Douglass | Aerodynamic installation of high-bypass-ratio fan engines | |
IT1135607B (en) | AERODYNAMIC RESISTANCE REDUCING SHIP | |
Chi et al. | Some recent advances in the understanding and prediction of turbomachine subsonic stall flutter | |
US3002716A (en) | Aircraft | |
Anderson et al. | Investigation of an NACA Submerged Inlet at Mach Numbers from 1.17 to 1.99 | |
GB2012372A (en) | Turbine Blades | |
JPH04314692A (en) | Air stream exfoliation preventing device for aircraft main wing | |
JPS55107037A (en) | Jet wake flow of aircraft | |
Barber et al. | Computational design and validation tests of advanced concept subsonic inlets | |
SE8602031D0 (en) | AIR GAS TURBINE ENGINE |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8305904-8 Effective date: 19940510 Format of ref document f/p: F |