ES271723A1 - A device of elevated ascensional force of an aircraft (Machine-translation by Google Translate, not legally binding) - Google Patents
A device of elevated ascensional force of an aircraft (Machine-translation by Google Translate, not legally binding)Info
- Publication number
- ES271723A1 ES271723A1 ES271723A ES271723A ES271723A1 ES 271723 A1 ES271723 A1 ES 271723A1 ES 271723 A ES271723 A ES 271723A ES 271723 A ES271723 A ES 271723A ES 271723 A1 ES271723 A1 ES 271723A1
- Authority
- ES
- Spain
- Prior art keywords
- supercirculation
- aircraft
- aileron
- translation
- machine
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Abstract
A device of great ascensional force of an airplane due to supercirculation, characterized in that, in order to obtain a high effective ascensional force due to the supercirculation that occurs on the wings, the flow lines are taken to the position in which supercirculation occurs for a flap or hinged flap near a stagnation point for the theoretically maximum supercirculation or at any point between it and the trailing edge of the wing, whereby the occurrence of the supercirculation is completed by providing a rounded wing profile exit edge and a jet of air at the inner root of the aileron, whereby the air jet performs the function of perfecting the supercirculation when the aileron is opened, contributing to the weight support of the aircraft body with the vertical component force of the jet of air and constituting a push for the propulsion of the aircraft when the aileron is closed. (Machine-translation by Google Translate, not legally binding)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4421060 | 1960-11-08 | ||
| JP818361 | 1961-03-13 | ||
| JP2758761 | 1961-08-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES271723A1 true ES271723A1 (en) | 1962-03-01 |
Family
ID=27277922
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES271723A Expired ES271723A1 (en) | 1960-11-08 | 1961-11-03 | A device of elevated ascensional force of an aircraft (Machine-translation by Google Translate, not legally binding) |
Country Status (3)
| Country | Link |
|---|---|
| CH (1) | CH460540A (en) |
| ES (1) | ES271723A1 (en) |
| GB (1) | GB965298A (en) |
-
1961
- 1961-10-30 GB GB38680/61A patent/GB965298A/en not_active Expired
- 1961-11-03 ES ES271723A patent/ES271723A1/en not_active Expired
- 1961-11-06 CH CH1284461A patent/CH460540A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB965298A (en) | 1964-07-29 |
| CH460540A (en) | 1968-07-31 |
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