IT1119069B - Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed - Google Patents
Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speedInfo
- Publication number
- IT1119069B IT1119069B IT6778579A IT6778579A IT1119069B IT 1119069 B IT1119069 B IT 1119069B IT 6778579 A IT6778579 A IT 6778579A IT 6778579 A IT6778579 A IT 6778579A IT 1119069 B IT1119069 B IT 1119069B
- Authority
- IT
- Italy
- Prior art keywords
- supersonic
- aircraft
- canard
- stabiliser
- disconnected
- Prior art date
Links
- 241000272517 Anseriformes Species 0.000 title abstract 3
- 239000003381 stabilizer Substances 0.000 title abstract 2
- 230000007704 transition Effects 0.000 title 1
- 230000000694 effects Effects 0.000 abstract 1
- 230000007935 neutral effect Effects 0.000 abstract 1
- 239000013589 supplement Substances 0.000 abstract 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The forward stabiliser or canard (2) of a supersonic aircraft is linked to the aircraft flying controls to improve control of the aircraft during landing and take-off. In these cases it produces a lifting force F2 to supplement the lifting force F1 of the main wing (1). The canard can be disconnected from the flying controls and allowed to 'float' so that it occupies a neutral attitude and has no effect on the aircraft. This enables the centre of pressure to be changed when passing from subsonic to supersonic speed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT6778579A IT1119069B (en) | 1979-04-13 | 1979-04-13 | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT6778579A IT1119069B (en) | 1979-04-13 | 1979-04-13 | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7967785A0 IT7967785A0 (en) | 1979-04-13 |
IT1119069B true IT1119069B (en) | 1986-03-03 |
Family
ID=11305279
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT6778579A IT1119069B (en) | 1979-04-13 | 1979-04-13 | Canard for supersonic aircraft - has stabiliser disconnected from flying controls to facilitate transition to supersonic speed |
Country Status (1)
Country | Link |
---|---|
IT (1) | IT1119069B (en) |
-
1979
- 1979-04-13 IT IT6778579A patent/IT1119069B/en active
Also Published As
Publication number | Publication date |
---|---|
IT7967785A0 (en) | 1979-04-13 |
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