AU3621695A - Linkage to deploy a surface relative to a wing - Google Patents
Linkage to deploy a surface relative to a wingInfo
- Publication number
- AU3621695A AU3621695A AU36216/95A AU3621695A AU3621695A AU 3621695 A AU3621695 A AU 3621695A AU 36216/95 A AU36216/95 A AU 36216/95A AU 3621695 A AU3621695 A AU 3621695A AU 3621695 A AU3621695 A AU 3621695A
- Authority
- AU
- Australia
- Prior art keywords
- deploy
- wing
- linkage
- surface relative
- relative
- 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.)
- Abandoned
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
- B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
- B63B1/28—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
- B63B1/285—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils changing the angle of attack or the lift of the foil
- B63B1/286—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils changing the angle of attack or the lift of the foil using flaps
-
- 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
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Applications Claiming Priority (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NZ260216 | 1994-09-29 | ||
NZ26021694 | 1994-09-29 | ||
NZ264904 | 1994-11-11 | ||
NZ26490494 | 1994-11-11 | ||
NZ27011494 | 1994-12-09 | ||
NZ270114 | 1994-12-09 | ||
NZ27088595 | 1995-04-06 | ||
NZ270885 | 1995-04-06 | ||
PCT/NZ1995/000096 WO1996009955A1 (en) | 1994-09-29 | 1995-09-27 | Linkage to deploy a surface relative to a wing |
Publications (1)
Publication Number | Publication Date |
---|---|
AU3621695A true AU3621695A (en) | 1996-04-19 |
Family
ID=27484338
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU36216/95A Abandoned AU3621695A (en) | 1994-09-29 | 1995-09-27 | Linkage to deploy a surface relative to a wing |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU3621695A (en) |
WO (1) | WO1996009955A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997038900A1 (en) * | 1996-04-13 | 1997-10-23 | Michael Craig Broadbent | Variable camber wing mechanism |
GB9607707D0 (en) * | 1996-04-13 | 1996-06-19 | Broadbent Michael C | A self-sealing parallelogram slat mechanism |
GB9703683D0 (en) * | 1997-02-21 | 1997-04-09 | Broadbent Michael C | Interconnection system for slat/flap deployment |
US6010097A (en) * | 1997-10-16 | 2000-01-04 | Northrop Grumman Corporation | Scissor linkage type slotted flap mechanism |
GB0012176D0 (en) * | 2000-05-20 | 2000-07-12 | Broadbent Michael C | Deployment system for a moveable wing surface |
GB0114634D0 (en) * | 2001-06-15 | 2001-08-08 | Broadbent Michael C | Contiguous variable camber device |
GB0314000D0 (en) * | 2003-06-17 | 2003-07-23 | Broadbent Michael C | Direct rotate swing slat system |
US6974112B2 (en) | 2003-06-17 | 2005-12-13 | Michael Craig Broadbent | Deployment system for a moveable wing surface |
GB0700604D0 (en) * | 2007-01-11 | 2007-02-21 | Airbus Uk Ltd | A leading edge structure for an aerofoil |
GB201214143D0 (en) | 2012-08-08 | 2012-09-19 | Airbus Operations Ltd | Slat support and deployment coupling |
US10974816B2 (en) | 2017-09-28 | 2021-04-13 | The Boeing Company | High-fowler flap actuation apparatus and related methods |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2246116A (en) * | 1937-10-28 | 1941-06-17 | Messerschmitt Boelkow Blohm | Airplane wing structure |
DE1917532C3 (en) * | 1969-04-05 | 1974-05-30 | Dornier Gmbh, 7990 Friedrichshafen | Slotted flap arrangement on wings for aircraft |
DE2103639A1 (en) * | 1971-01-27 | 1972-09-07 | Messerschmitt-Bölkow-Blöhm GmbH, 8000 München | Airfoil for aircraft with one or more one-part or multi-part slotted flaps |
DE2354420C3 (en) * | 1973-10-31 | 1978-04-06 | Dornier Gmbh, 7990 Friedrichshafen | Flap actuation assembly on a wing for aircraft |
US4202519A (en) * | 1978-09-08 | 1980-05-13 | The Boeing Company | Airfoil leading edge slat apparatus |
DE3013774A1 (en) * | 1980-04-10 | 1981-10-15 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | OPERATING ARRANGEMENT FOR FLAP VALVES |
-
1995
- 1995-09-27 WO PCT/NZ1995/000096 patent/WO1996009955A1/en active Application Filing
- 1995-09-27 AU AU36216/95A patent/AU3621695A/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO1996009955A1 (en) | 1996-04-04 |
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