SU73281A1 - Aircraft bearing surface having slats - Google Patents
Aircraft bearing surface having slatsInfo
- Publication number
- SU73281A1 SU73281A1 SU11345A SU11345A SU73281A1 SU 73281 A1 SU73281 A1 SU 73281A1 SU 11345 A SU11345 A SU 11345A SU 11345 A SU11345 A SU 11345A SU 73281 A1 SU73281 A1 SU 73281A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- slats
- bearing surface
- aircraft bearing
- aircraft
- air
- Prior art date
Links
Landscapes
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Description
Предлагаетс несу|ца поверхность самолета, имеюща предкрылки , в которых расположена магистраль, позвол ющ а производить дополнительный обдув несущей новерхности воздухом или газом с НС-мощью специальной установки дл увеличени подъемной силы и улучшени взлетно-посадочных свойств самолета.A plane's surface is proposed, having slats in which the line is located, allowing additional airflow with the HC-power of a special installation to blow the carrier surface with air to increase lift force and improve the take-off and landing properties of the aircraft.
{-la чертеже схематично изО|бражен нрофиль кр1з1ла с предл агаеМЫ:М предкрылком.{-la drawing schematically from | brazil the profile of the crane with the suggestion: M slat.
Предкрылок 1 самолета .выполнен из двух Г1ро( 2 и , даюндих возможность изменени величины щелевидного зазора 4 между ними и перестановки профилей вдоль хорды крыла. В передпей Части предкрылка помещаетс затвор, поз/вол ющий закрывать П1.елевидный зазор 4 между профил ми 2 и 3, и магистр аль, :идуща вдоль передпей кромки крыла, через которую производитс .дополмительным обдув несущих поверхностей воздухом или газом с помощью спениальной устанс-вкн.The slat 1 of the aircraft is made of two G1ros (2 and, yes, the possibility of changing the size of the slit gap 4 between them and rearranging the profiles along the wing chord. 3, and Master Al,: walking along the leading edge of the wing, through which the air surfaces of the load bearing surfaces are blown by air or gas using a sleeping-air ustans-vkn.
РегулирОВашие ве.тичины зазора :между профил чИ 2 и 3 предкрылка и перестановка профи тей вдоль хорды крыла / имеет целью увеличение скорости обтекапи осиовного профил ры,ча за счет динамического напора и получени профи.т несущей новерхности, соответствующего скорости полета.Regulated gap widths: between profiles 2 and 3 of the slat and rearrangement of profiles along the wing chord / has the aim of increasing the velocity of the axial profile, around 15 due to the dynamic head and obtaining a profile of the carrier surface corresponding to the flight speed.
Предмет и з о б р е т е н и Subject and title
Несуща поверхность салюлета, имеюща предкрылки, в которых распо.тожеиа мааистраль, позвол юща производить дополнительный обдув несущей поверхности .воздухом или газом с помощью специальной установки, с целью увеличени подъемной силы и улучшени взлетно-цосадочпых свойств самолета, о тл и ч щ а ЯС , что,The bearing surface of the salulet, having slats in which the same maistrale is located, allows additional airflow of the bearing surface with air or gas using a special installation, in order to increase the lifting force and improve the take-off and landing properties of the aircraft, about 10 , what,
с целью увеличени скорости обтекани ; основного профил за счет динамического напора и получени профдал несущей новерхности, соответствующего скорости полета, предкрылок выполнен из двух профилей с возможностью регулиров1акк величины щелевидного зазора между ними и нерестановюи профилей вдоль хорды крыла.in order to increase the flow rate; the main profile due to the dynamic head and obtaining a professional profile of the carrier surface corresponding to the flight speed; the slat is made of two profiles with the possibility of adjusting the size of the slit-like gap between them and the non-stopping of the profiles along the wing chord.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU11345A SU73281A1 (en) | 1947-08-27 | 1947-08-27 | Aircraft bearing surface having slats |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU11345A SU73281A1 (en) | 1947-08-27 | 1947-08-27 | Aircraft bearing surface having slats |
Publications (1)
Publication Number | Publication Date |
---|---|
SU73281A1 true SU73281A1 (en) | 1947-11-30 |
Family
ID=48249363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU11345A SU73281A1 (en) | 1947-08-27 | 1947-08-27 | Aircraft bearing surface having slats |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU73281A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013137771A1 (en) * | 2012-07-31 | 2013-09-19 | Ilyin Aleksey Valentinovich | Method for increasing and controlling the lift of an aerodynamic airfoil, primarily an aircraft wing, and aerodynamic airfoil, primarily an aircraft wing |
-
1947
- 1947-08-27 SU SU11345A patent/SU73281A1/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013137771A1 (en) * | 2012-07-31 | 2013-09-19 | Ilyin Aleksey Valentinovich | Method for increasing and controlling the lift of an aerodynamic airfoil, primarily an aircraft wing, and aerodynamic airfoil, primarily an aircraft wing |
RU2527628C2 (en) * | 2012-07-31 | 2014-09-10 | Алексей Валентинович Ильин | Method of increasing aircraft wing lift |
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