SU73281A1 - Aircraft bearing surface having slats - Google Patents

Aircraft bearing surface having slats

Info

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
Application number
SU11345A
Other languages
Russian (ru)
Inventor
И.Е. Турчан
Original Assignee
И.Е. Турчан
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by И.Е. Турчан filed Critical И.Е. Турчан
Priority to SU11345A priority Critical patent/SU73281A1/en
Application granted granted Critical
Publication of SU73281A1 publication Critical patent/SU73281A1/en

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.

SU11345A 1947-08-27 1947-08-27 Aircraft bearing surface having slats SU73281A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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