JPH0258159B2 - - Google Patents
Info
- Publication number
- JPH0258159B2 JPH0258159B2 JP54164642A JP16464279A JPH0258159B2 JP H0258159 B2 JPH0258159 B2 JP H0258159B2 JP 54164642 A JP54164642 A JP 54164642A JP 16464279 A JP16464279 A JP 16464279A JP H0258159 B2 JPH0258159 B2 JP H0258159B2
- Authority
- JP
- Japan
- Prior art keywords
- wing
- tip extension
- wing tip
- main
- main wing
- 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.)
- Expired - Lifetime
Links
- 230000007704 transition Effects 0.000 claims description 4
- 238000000926 separation method Methods 0.000 description 8
- 230000007423 decrease Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 101100272667 Xenopus laevis ripply2.2 gene Proteins 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Tires In General (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2909245A DE2909245C2 (de) | 1979-03-09 | 1979-03-09 | Quertriebskörper, insbesondere Flugzeugtragflügel |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS55119595A JPS55119595A (en) | 1980-09-13 |
JPH0258159B2 true JPH0258159B2 (ru) | 1990-12-06 |
Family
ID=6064916
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP16464279A Granted JPS55119595A (en) | 1979-03-09 | 1979-12-18 | Main wing for aircraft |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS55119595A (ru) |
DE (1) | DE2909245C2 (ru) |
FR (1) | FR2450744A1 (ru) |
GB (1) | GB2043572B (ru) |
IT (1) | IT1127987B (ru) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3378573D1 (en) * | 1982-12-30 | 1989-01-05 | Boeing Co | Tapered thickness-chord ratio wing |
US4611773A (en) * | 1982-12-30 | 1986-09-16 | The Boeing Company | Tapered thickness-chord ratio wing |
WO1998056654A1 (en) * | 1997-06-13 | 1998-12-17 | The Boeing Company | Blunt-leading-edge raked wingtips |
GB2472766A (en) * | 2009-07-29 | 2011-02-23 | Ian Morton Hannay | Wing |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR435600A (fr) * | 1910-11-13 | 1912-03-05 | Alois Wolfmueller | Aéroplane avec surface gauche de sustentation en forme de croissant |
GB129834A (en) * | 1918-08-02 | 1919-07-24 | Alexander Albert Holle | Improvements in Aerofoils for Aeroplanes and the like. |
CH88677A (fr) * | 1919-07-24 | 1921-03-16 | Holle Alexandre Albert | Aile pour machine volante. |
US1622242A (en) * | 1921-10-15 | 1927-03-22 | Taylor Cecil Hamelin | Aeroplane |
FR545639A (fr) * | 1922-01-05 | 1922-10-17 | Aviation Louis Breguet Sa | Mode de construction des ailes d'aéroplanes à épaisseur relative variable en vue d'améliorer leurs qualités aérodynamiques |
FR799706A (fr) * | 1935-03-22 | 1936-06-18 | Perfectionnement aux formes d'ailes d'avion et adaptation de ces formes aux avions ailes tripartites | |
FR931251A (fr) * | 1942-06-08 | 1948-02-18 | Avion | |
US3721507A (en) * | 1971-09-22 | 1973-03-20 | United Aircraft Corp | Blade for high speed helicopter |
-
1979
- 1979-03-09 DE DE2909245A patent/DE2909245C2/de not_active Expired
- 1979-12-18 JP JP16464279A patent/JPS55119595A/ja active Granted
-
1980
- 1980-01-28 IT IT67112/80A patent/IT1127987B/it active
- 1980-02-20 GB GB8005691A patent/GB2043572B/en not_active Expired
- 1980-02-29 FR FR8004874A patent/FR2450744A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
IT8067112A0 (it) | 1980-01-28 |
FR2450744B1 (ru) | 1984-10-05 |
FR2450744A1 (fr) | 1980-10-03 |
GB2043572A (en) | 1980-10-08 |
JPS55119595A (en) | 1980-09-13 |
GB2043572B (en) | 1983-04-20 |
IT1127987B (it) | 1986-05-28 |
DE2909245C2 (de) | 1983-01-27 |
DE2909245A1 (de) | 1980-09-11 |
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