SU83972A1 - Method of reducing speed (braking) of aircraft flight - Google Patents
Method of reducing speed (braking) of aircraft flightInfo
- Publication number
- SU83972A1 SU83972A1 SU379127A SU379127A SU83972A1 SU 83972 A1 SU83972 A1 SU 83972A1 SU 379127 A SU379127 A SU 379127A SU 379127 A SU379127 A SU 379127A SU 83972 A1 SU83972 A1 SU 83972A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- braking
- aircraft flight
- reducing speed
- aircraft
- flight
- Prior art date
Links
Landscapes
- Tires In General (AREA)
Description
Известны различные способы уменьшени скорости полета самолета на маневре нутем увеличени его лобового сопротивлени .Various methods are known for reducing the speed of flight of an aircraft while maneuvering in an increase in its drag.
В описываемом изобретении увеличение лобового сопротивлен 1 самолета достигаетс тем, что из несущих поверхностей самолета выпускают эластичные ленты, которые под действием встречного потока прнход в колебательное движение и преобразуют кинетнческую энергию этого потока в лобовое сопротивление.In the described invention, an increase in the frontal resistance of an aircraft 1 is achieved by the production of elastic ribbons from the bearing surfaces of the aircraft, which, under the action of the oncoming flow, transform into oscillatory motion and convert the kinetnic energy of this flow into frontal resistance.
На чертеже изображена схема, иллюстрирующа способ уменьшени скорости полета самолета на маневре.The drawing shows a diagram illustrating a method for reducing the speed of flight of an aircraft during a maneuver.
Этот способ заключаетс в том, что эластичные ленты /, выт гиваемые из несущих поверхностей 2 вблизи задней кромки, привод тс в колебательное движение под действием набегающего потока воздуха. Поглощаема при этом энерги движущегос воздуха про вл етс в виде лобового сопротивлени .This method consists in the fact that the elastic bands / pulled from the supporting surfaces 2 near the trailing edge are driven into oscillatory motion by the incident air flow. The energy absorbed by the moving air is manifested in the form of drag.
Выт гивание лент из несущих поверхностей осуществл етс силой начального лобоаого сопротивлени прикрепленных к ним узких ленточек (на чертеже не показаны), подверженных действию воздушного потока в нор.мальном полете.The ribbons are pulled out of the bearing surfaces by the force of the initial lobe resistance of the narrow ribbons attached to them (not shown) exposed to the air flow in normal flight.
Предмет изобретени Subject invention
Споеоб уменьшени (торможени ) скорости полета самолета на маневре путем увеличени его лобового сопротивлени , отличающ н и с тем, что дл увеличени лобового сопротивлени из несущих поверхностей самолета вдоль их задних кромок выпускают эластичные ленты, которые под действием встречного потока приход т в колебательное движение и преобразуют кинетическую энергию потока в лобовое сопротивление.To reduce (decelerate) the flight speed of an aircraft at a maneuver by increasing its frontal resistance, it is different in that, in order to increase frontal resistance, elastic belts are released from the bearing surfaces of the aircraft along their rear edges, which, under the action of a counter flow, come into oscillatory motion convert the kinetic energy of the flow into drag.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU379127A SU83972A1 (en) | 1948-05-17 | 1948-05-17 | Method of reducing speed (braking) of aircraft flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU379127A SU83972A1 (en) | 1948-05-17 | 1948-05-17 | Method of reducing speed (braking) of aircraft flight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU83972A1 true SU83972A1 (en) | 1949-11-30 |
Family
ID=48256752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU379127A SU83972A1 (en) | 1948-05-17 | 1948-05-17 | Method of reducing speed (braking) of aircraft flight |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU83972A1 (en) |
-
1948
- 1948-05-17 SU SU379127A patent/SU83972A1/en active
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