FIELD: machine building.
SUBSTANCE: erection device of a suspension element on a casing of gas-turbine engine includes a fork including at least one eye lug and rigidly attached to the casing. The axis fixed on the above fork supports the above mentioned element by means of a ring enclosing the axis. The erection device includes a rotation locking device containing a lock plate connected to the eye lug. The plate and the axis include an assembly consisting of a pin and a slot or a hole, into which the above pin enters, thus providing axis rotation locking in the fork. The plate is locked against rotation in relation to the fork by means of a bolted connection. The other object of the invention is the gas-turbine engine casing containing the above described erection device, as well as a gas-turbine engine containing such a casing.
EFFECT: invention allows avoiding friction wear of eye lugs, sleeves and axes of the suspension.
5 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBINE ENGINE PROVIDED WITH MEANS OF ABSORBING STRESSES FROM THRUST OF ENGINE THEREOF | 2014 |
|
RU2677312C2 |
AIRCRAFT ENGINE WITH SUSPENSION APPLIANCES | 2005 |
|
RU2372256C2 |
ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT | 2014 |
|
RU2682206C2 |
GAS TURBINE ENGINE COMBUSTION CHAMBER | 2008 |
|
RU2498163C2 |
AIRCRAFT ENGINE SUPPORT COMPRISING TWO TIE RODS WITH TRANSVERSE JOINTING ELEMENT | 2007 |
|
RU2433068C2 |
AIRCRAFT ENGINE MOUNTING DEVICE | 2007 |
|
RU2422332C2 |
AIRCRAFT ENGINE SUSPENSION TO BE MOUNTED BETWEEN ENGINE AND ATTACHMENT BAR | 2006 |
|
RU2391259C2 |
TURBOJET COLD FLOW CHANNEL SUSPENSION AT EXHAUST HOUSING, USING RODS AND RADIAL FORKS | 2012 |
|
RU2618142C2 |
AIRCRAFT POWER PLANT | 2009 |
|
RU2499745C2 |
METHOD AND DEVICE FOR MOUNTING ENGINE ON AIRCRAFT PYLON | 2015 |
|
RU2690834C2 |
Authors
Dates
2013-08-10—Published
2008-11-07—Filed