DE3338286A1 - Flugzeugtriebwerksgondel und verfahren zum erzeugen eines profils derselben - Google Patents
Flugzeugtriebwerksgondel und verfahren zum erzeugen eines profils derselbenInfo
- Publication number
- DE3338286A1 DE3338286A1 DE19833338286 DE3338286A DE3338286A1 DE 3338286 A1 DE3338286 A1 DE 3338286A1 DE 19833338286 DE19833338286 DE 19833338286 DE 3338286 A DE3338286 A DE 3338286A DE 3338286 A1 DE3338286 A1 DE 3338286A1
- Authority
- DE
- Germany
- Prior art keywords
- profile
- chord
- nacelle
- edge
- leading edge
- 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.)
- Ceased
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 3
- 238000009826 distribution Methods 0.000 claims description 43
- 238000000926 separation method Methods 0.000 claims description 13
- 230000007423 decrease Effects 0.000 claims description 12
- 230000032798 delamination Effects 0.000 claims description 6
- 230000003247 decreasing effect Effects 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 239000003973 paint Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 8
- 230000002829 reductive effect Effects 0.000 description 5
- 230000002411 adverse Effects 0.000 description 4
- 238000013459 approach Methods 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000036961 partial effect Effects 0.000 description 2
- 230000002441 reversible effect Effects 0.000 description 2
- 101100129500 Caenorhabditis elegans max-2 gene Proteins 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 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
- 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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US43758182A | 1982-10-29 | 1982-10-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3338286A1 true DE3338286A1 (de) | 1984-05-03 |
Family
ID=23737028
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19833338286 Ceased DE3338286A1 (de) | 1982-10-29 | 1983-10-21 | Flugzeugtriebwerksgondel und verfahren zum erzeugen eines profils derselben |
Country Status (11)
Country | Link |
---|---|
JP (1) | JPS5996462A (sv) |
AU (1) | AU555526B2 (sv) |
CA (1) | CA1209354A (sv) |
CH (1) | CH667434A5 (sv) |
DE (1) | DE3338286A1 (sv) |
GB (1) | GB2128945B (sv) |
IL (1) | IL69906A (sv) |
IT (1) | IT1171783B (sv) |
NL (1) | NL8303716A (sv) |
SE (1) | SE456077B (sv) |
SU (1) | SU1391490A3 (sv) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920143B1 (fr) * | 2007-08-20 | 2010-01-22 | Aircelle Sa | Dispositif de commande des actionneurs de maintenance de capots d'une nacelle de turboreacteur |
DE102009003084B4 (de) | 2009-05-13 | 2013-03-14 | Airbus Operations Gmbh | Verkleidung für eine Auftriebshilfe |
GB2595724B (en) | 2020-06-05 | 2022-10-05 | Rolls Royce Plc | Nacelle for gas turbine engine and aircraft comprising the same |
FR3116043B1 (fr) * | 2020-11-09 | 2023-04-28 | Safran Aircraft Engines | Entrée d’air de nacelle d’ensemble propulsif d’aéronef pour favoriser une phase d’inversion de poussée |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3533237A (en) * | 1964-07-01 | 1970-10-13 | Gen Electric | Low drag nacelle arrangement for jet propulsion power plants |
DE2254888A1 (de) * | 1971-11-09 | 1973-05-10 | Nasa | Tragfluegel fuer unterschallgeschwindigkeit |
US3765623A (en) * | 1971-10-04 | 1973-10-16 | Mc Donnell Douglas Corp | Air inlet |
DE2322654A1 (de) * | 1972-05-04 | 1973-11-08 | Mc Donnell Douglas Corp | Hochleistungstragfluegel und verfahren zum konstruieren derselben |
DE2608414A1 (de) * | 1975-03-04 | 1976-09-16 | Secr Defence Brit | Ueberkritisches tragfluegelprofil |
DE2626276A1 (de) * | 1975-06-12 | 1976-12-23 | Secr Defence Brit | Ueberkritisches tragfluegelprofil |
DE2712717A1 (de) * | 1977-03-23 | 1978-09-28 | Ver Flugtechnische Werke | Ueberkritisches tragfluegelprofil |
DE2922200A1 (de) * | 1978-05-29 | 1979-12-06 | Aerospatiale | Tragfluegelprofil |
US4209149A (en) * | 1977-12-27 | 1980-06-24 | Boeing Commercial Airplane Company | Contracted inlet for jet engine being transported as cargo |
DE3107496A1 (de) * | 1980-03-03 | 1981-12-24 | General Electric Co., Schenectady, N.Y. | Blaesertriebwerk, insbesondere den stroemungswiderstand vermindernde triebwerksgondel |
DE3033101A1 (de) * | 1980-09-03 | 1982-03-11 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren zur erhoehung der resultierenden vortriebskraft bei flugzeugen |
-
1983
- 1983-09-12 AU AU19026/83A patent/AU555526B2/en not_active Ceased
- 1983-10-04 IL IL69906A patent/IL69906A/xx unknown
- 1983-10-07 CA CA000438631A patent/CA1209354A/en not_active Expired
- 1983-10-14 JP JP58191060A patent/JPS5996462A/ja active Granted
- 1983-10-18 SU SU833652711A patent/SU1391490A3/ru active
- 1983-10-21 CH CH5734/83A patent/CH667434A5/de not_active IP Right Cessation
- 1983-10-21 DE DE19833338286 patent/DE3338286A1/de not_active Ceased
- 1983-10-24 GB GB08328400A patent/GB2128945B/en not_active Expired
- 1983-10-27 IT IT23478/83A patent/IT1171783B/it active
- 1983-10-27 SE SE8305904A patent/SE456077B/sv not_active IP Right Cessation
- 1983-10-28 NL NL8303716A patent/NL8303716A/nl not_active Application Discontinuation
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3533237A (en) * | 1964-07-01 | 1970-10-13 | Gen Electric | Low drag nacelle arrangement for jet propulsion power plants |
DE1526812A1 (de) * | 1964-07-01 | 1971-01-14 | Gen Electric | Turbogeblaese-Triebwerk |
US3765623A (en) * | 1971-10-04 | 1973-10-16 | Mc Donnell Douglas Corp | Air inlet |
DE2254888A1 (de) * | 1971-11-09 | 1973-05-10 | Nasa | Tragfluegel fuer unterschallgeschwindigkeit |
DE2322654A1 (de) * | 1972-05-04 | 1973-11-08 | Mc Donnell Douglas Corp | Hochleistungstragfluegel und verfahren zum konstruieren derselben |
DE2608414A1 (de) * | 1975-03-04 | 1976-09-16 | Secr Defence Brit | Ueberkritisches tragfluegelprofil |
DE2626276A1 (de) * | 1975-06-12 | 1976-12-23 | Secr Defence Brit | Ueberkritisches tragfluegelprofil |
DE2712717A1 (de) * | 1977-03-23 | 1978-09-28 | Ver Flugtechnische Werke | Ueberkritisches tragfluegelprofil |
US4209149A (en) * | 1977-12-27 | 1980-06-24 | Boeing Commercial Airplane Company | Contracted inlet for jet engine being transported as cargo |
DE2922200A1 (de) * | 1978-05-29 | 1979-12-06 | Aerospatiale | Tragfluegelprofil |
DE3107496A1 (de) * | 1980-03-03 | 1981-12-24 | General Electric Co., Schenectady, N.Y. | Blaesertriebwerk, insbesondere den stroemungswiderstand vermindernde triebwerksgondel |
DE3033101A1 (de) * | 1980-09-03 | 1982-03-11 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren zur erhoehung der resultierenden vortriebskraft bei flugzeugen |
Also Published As
Publication number | Publication date |
---|---|
IT8323478A0 (it) | 1983-10-27 |
GB2128945B (en) | 1986-03-26 |
CH667434A5 (de) | 1988-10-14 |
SE8305904D0 (sv) | 1983-10-27 |
IT1171783B (it) | 1987-06-10 |
IL69906A0 (en) | 1984-01-31 |
JPH0344221B2 (sv) | 1991-07-05 |
GB2128945A (en) | 1984-05-10 |
AU1902683A (en) | 1984-05-03 |
IL69906A (en) | 1990-04-29 |
SU1391490A3 (ru) | 1988-04-23 |
GB8328400D0 (en) | 1983-11-23 |
CA1209354A (en) | 1986-08-12 |
SE456077B (sv) | 1988-09-05 |
SE8305904L (sv) | 1984-04-30 |
AU555526B2 (en) | 1986-09-25 |
NL8303716A (nl) | 1984-05-16 |
JPS5996462A (ja) | 1984-06-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8110 | Request for examination paragraph 44 | ||
8131 | Rejection |