IT1057415B - Meccanismo di montaggio degli alettoni sul bordo di uscita delle ali di un aereoplano - Google Patents
Meccanismo di montaggio degli alettoni sul bordo di uscita delle ali di un aereoplanoInfo
- Publication number
- IT1057415B IT1057415B IT48684/76A IT4868476A IT1057415B IT 1057415 B IT1057415 B IT 1057415B IT 48684/76 A IT48684/76 A IT 48684/76A IT 4868476 A IT4868476 A IT 4868476A IT 1057415 B IT1057415 B IT 1057415B
- Authority
- IT
- Italy
- Prior art keywords
- ailers
- airplane
- wings
- outlet
- assembly mechanism
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jib Cranes (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US56109675A | 1975-03-24 | 1975-03-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1057415B true IT1057415B (it) | 1982-03-10 |
Family
ID=24240613
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT48684/76A IT1057415B (it) | 1975-03-24 | 1976-03-23 | Meccanismo di montaggio degli alettoni sul bordo di uscita delle ali di un aereoplano |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS51126700A (de) |
DE (1) | DE2611918A1 (de) |
FR (1) | FR2305342A1 (de) |
GB (5) | GB1547901A (de) |
IT (1) | IT1057415B (de) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62113697A (ja) * | 1985-11-14 | 1987-05-25 | 財団法人 日本航空機開発協会 | 飛行機翼後縁フラツプのリンク式作動機構 |
GB8915487D0 (en) * | 1989-07-06 | 1989-08-23 | Short Brothers Plc | A flap assembly |
DE10133920B4 (de) | 2001-07-12 | 2004-05-13 | Eads Deutschland Gmbh | Auftriebsklappen-Mechanismus |
DE10328540B4 (de) * | 2003-06-24 | 2008-02-14 | Eads Deutschland Gmbh | Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe |
DE10328717B3 (de) | 2003-06-25 | 2004-12-02 | Eads Deutschland Gmbh | Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe |
DE10339030B4 (de) | 2003-08-25 | 2005-11-03 | Man Technologie Ag | Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung |
GB0921007D0 (en) | 2009-11-30 | 2010-01-13 | Airbus Operations Ltd | Trailing edge flap |
CN109367761B (zh) * | 2018-10-11 | 2022-05-31 | 西北工业大学 | 一种用于旋转机翼的襟翼收放操纵机构 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3009668A (en) * | 1958-05-12 | 1961-11-21 | Lockheed Aircraft Corp | Displacement type airfoil flap with boundary layer control |
DE2100733A1 (de) * | 1970-01-12 | 1971-07-15 | Hawker Siddeley Aviation Ltd., Kingston-Upon-Thames, Surrey (Grossbritannien) | Vorrichtung an Flugzeugtragflachen |
US3874617A (en) * | 1974-07-17 | 1975-04-01 | Mc Donnell Douglas Corp | Stol flaps |
-
1976
- 1976-03-16 GB GB10509/76A patent/GB1547901A/en not_active Expired
- 1976-03-16 GB GB47061/78A patent/GB1547904A/en not_active Expired
- 1976-03-16 GB GB47059/78A patent/GB1547902A/en not_active Expired
- 1976-03-16 GB GB47062/78A patent/GB1547905A/en not_active Expired
- 1976-03-16 GB GB47060/78A patent/GB1547903A/en not_active Expired
- 1976-03-20 DE DE19762611918 patent/DE2611918A1/de not_active Withdrawn
- 1976-03-23 IT IT48684/76A patent/IT1057415B/it active
- 1976-03-24 FR FR7608552A patent/FR2305342A1/fr not_active Withdrawn
- 1976-03-24 JP JP51032368A patent/JPS51126700A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
GB1547901A (en) | 1979-06-27 |
FR2305342A1 (fr) | 1976-10-22 |
GB1547903A (en) | 1979-06-27 |
DE2611918A1 (de) | 1976-11-11 |
GB1547905A (en) | 1979-06-27 |
GB1547904A (en) | 1979-06-27 |
GB1547902A (en) | 1979-06-27 |
JPS51126700A (en) | 1976-11-04 |
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