MD3510G2 - Aircraft-control gear - Google Patents

Aircraft-control gear

Info

Publication number
MD3510G2
MD3510G2 MDA20060036A MD20060036A MD3510G2 MD 3510 G2 MD3510 G2 MD 3510G2 MD A20060036 A MDA20060036 A MD A20060036A MD 20060036 A MD20060036 A MD 20060036A MD 3510 G2 MD3510 G2 MD 3510G2
Authority
MD
Moldova
Prior art keywords
joined
aircraft
gear unit
onto
satellite gear
Prior art date
Application number
MDA20060036A
Other languages
Romanian (ro)
Russian (ru)
Other versions
MD20060036A (en
MD3510F2 (en
Inventor
Ион БОСТАН
Флорин ИОНЕСКУ
Валериу ДУЛГЕРУ
Раду ЧОБАНУ
Юлиан МАЛКОЧ
Original Assignee
Технический университет Молдовы
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 Технический университет Молдовы filed Critical Технический университет Молдовы
Priority to MDA20060036A priority Critical patent/MD3510G2/en
Publication of MD20060036A publication Critical patent/MD20060036A/en
Publication of MD3510F2 publication Critical patent/MD3510F2/en
Publication of MD3510G2 publication Critical patent/MD3510G2/en

Links

Landscapes

  • Retarders (AREA)
  • Non-Deflectable Wheels, Steering Of Trailers, Or Other Steering (AREA)
  • Transmission Devices (AREA)
  • Braking Arrangements (AREA)

Abstract

The invention relates to the aircraft designing and may be used in the aircraft control and braking systems.The aircraft-control gear includes two turntable sections (1) and (2), installed onto the backside of the wing. The turntable sections (1) and (2) are mounted onto a common axis (5), in the middle of which it is placed an electric motor (7) with two hollow output shafts (8) and (9), one of which (8) is rigidly joined with a hollow inclined shaft (10), onto which it is installed a toothed two-crown (12, 13) satellite gear unit (11), on one side of which there are placed two fixed gearwheels (14) and (15) with a different number of teeth, alternately joined with a lateral fixed cover (18) by means of two couplings (16) and (17). On the other side of the satellite gear unit (11) it is installed a movable gearwheel (20), joined by a hinge (3) with one of the turntable sections (1). The second hollow output shaft (9) is rigidly joined with the second hollow inclined shaft (21), onto which it is installed the second toothed two-crown (23, 24) satellite gear unit (22), on one side of which it is placed a fixed gearwheel (25), joined with the second lateral fixed cover (29) by means of another coupling (26). On the other side of the satellite gear unit (22) it is placed another movable gearwheel (31), joined by a hinge (4) with the second turntable section (2).
MDA20060036A 2006-01-18 2006-01-18 Aircraft-control gear MD3510G2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
MDA20060036A MD3510G2 (en) 2006-01-18 2006-01-18 Aircraft-control gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
MDA20060036A MD3510G2 (en) 2006-01-18 2006-01-18 Aircraft-control gear

Publications (3)

Publication Number Publication Date
MD20060036A MD20060036A (en) 2007-08-31
MD3510F2 MD3510F2 (en) 2008-02-29
MD3510G2 true MD3510G2 (en) 2008-09-30

Family

ID=38477225

Family Applications (1)

Application Number Title Priority Date Filing Date
MDA20060036A MD3510G2 (en) 2006-01-18 2006-01-18 Aircraft-control gear

Country Status (1)

Country Link
MD (1) MD3510G2 (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2147544C1 (en) * 1998-01-19 2000-04-20 Нурмухаметов Искандер Рифович Wing
RU2184681C2 (en) * 2000-08-04 2002-07-10 Буданов Станислав Васильевич Device for motion in air medium
RU2186711C2 (en) * 2000-05-11 2002-08-10 Дудник Виталий Владимирович Singler-rotor helicopter multi-functional tail unit
RU2189334C2 (en) * 2000-05-04 2002-09-20 Буданов Станислав Васильевич Vehicle for motion in air medium
RU2002119450A (en) * 2002-07-23 2004-04-27 Закрытое акционерное общество "Отделение морских систем ОКБ им. П.О. Сухого" AIR BRAKE
SU1517264A1 (en) * 1987-06-22 2005-04-10 Н.С. Кирпичев WHEEL DIRECTION OF THE AIRCRAFT AND THE METHOD OF ITS MANUFACTURE

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1517264A1 (en) * 1987-06-22 2005-04-10 Н.С. Кирпичев WHEEL DIRECTION OF THE AIRCRAFT AND THE METHOD OF ITS MANUFACTURE
RU2147544C1 (en) * 1998-01-19 2000-04-20 Нурмухаметов Искандер Рифович Wing
RU2189334C2 (en) * 2000-05-04 2002-09-20 Буданов Станислав Васильевич Vehicle for motion in air medium
RU2186711C2 (en) * 2000-05-11 2002-08-10 Дудник Виталий Владимирович Singler-rotor helicopter multi-functional tail unit
RU2184681C2 (en) * 2000-08-04 2002-07-10 Буданов Станислав Васильевич Device for motion in air medium
RU2002119450A (en) * 2002-07-23 2004-04-27 Закрытое акционерное общество "Отделение морских систем ОКБ им. П.О. Сухого" AIR BRAKE

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Mecanism de dirijare a aparatului de zbor: www.buran.ru/htm/tail.htm [regăsită 2007.12.11] *

Also Published As

Publication number Publication date
MD20060036A (en) 2007-08-31
MD3510F2 (en) 2008-02-29

Similar Documents

Publication Publication Date Title
WO2008125364A3 (en) Transfer case for motor vehicles
BRPI1008604A2 (en) gearbox with epicyclic gear train and turbomachine, in particular of an airplane engine.
WO2007000151A3 (en) Clutch unit
WO2014011252A3 (en) Geared architecture with speed change device for gas turbine engine
EP2463550A3 (en) Dual clutch transmission
TW200806386A (en) Connection device, and kneading facility having kneading device and drive device connected to each other by the connection device
WO2007082594A3 (en) Drive unit comprising an electric rotating actuator and a wave gear speed reducer
BRPI0814351A2 (en) ENGINE WITH REDUCTION GEAR MECHANISM
GB2438046B (en) Epicyclic gear transmission for rotary wing aircraft
GB2451759B (en) Split torque geared power transmissions with composite output shafts
ATE333977T1 (en) GEARBOX FOR A TWIN SCREW EXTRUDER
ATE517281T1 (en) SHIFT UNIT FOR A MANUAL TRANSMISSION OF A MOTOR VEHICLE
UA98663C2 (en) Mechanical forming press
WO2013020695A8 (en) Adjustment unit for a motor vehicle and method for assembling said adjustment unit
UA105177C2 (en) Transmission and differential device
WO2009156267A3 (en) Actuator
PL2165819T3 (en) Extruder arrangement
MD3510G2 (en) Aircraft-control gear
WO2009016313A3 (en) Power unit for a ship
GB2474591A (en) Multiple output transmission systems
WO2007000269A3 (en) Twin-clutch transmission for a motor vehicle
CN202746500U (en) Simple, compact and easily-controlled power distribution box
RS50716B (en) Fitting transmission for a window, a door or the like, and method for actuating the transmission
SE0700661L (en) Transmission for motor vehicles
EP1965097A3 (en) Manual transmission and vehicle having transverse-mount engine and transmission arranged in tandem

Legal Events

Date Code Title Description
KA4A Patent for invention lapsed due to non-payment of fees (with right of restoration)
MM4A Patent for invention definitely lapsed due to non-payment of fees