Turbomachine assembly for a sealed assembly of a front cone on a front virole
FR3053384A1
Fixing assembly of a distributor to a structural element of a turbomachine
FR3053387A1
Turbomachine housing
FR3052990A1
Cooling circuit of a turbomachine blade
FR3053074A1
PIECE AND METHOD FOR MANUFACTURING A REDUCED ROLLED ROLLED PIECE
FR3053078A1
Fuel dosing system and method comprising variability of fuel density
FR3053112A1
Method for measuring a turning angle of a turbomachine wheel blade
FR3053075A1
Turbomachine part coated with a thermal barrier and a coating for protecting against cmas and method for obtaining the same
FR3053076A1
Turbomachine part coated with a thermal barrier and a coating for protecting against cmas and method for obtaining the same
FR3053077A1
Accessories relay housing of a turbomachine
FR3052823A1
Aerodynamic bond in a turbomachine part
FR3052805A1
Improved monobloc aubing disk, rotating part of a turbomachine comprising such a disk and associated turbomachine
FR3052806A1
Method and device for integrity testing of a fluid flow control system for a turbomachine
FR3052863A1
Vein for turbomachine, comprising a device for measuring the characteristics of an air flow
FR3052839A1
Sealing device for turbomachine, sealing system comprising said sealing device, method for mounting a sealing device on a turbomachine part
FR3052488A1
Turbomachine exhaust case
GB201610276D0
A propulsion assembly for an aircraft having a turbojet with a non-ducted fan and an attachment pylon
FR3052502A1
Fired engine combustion chamber with variable composite fins
FR3052580A1
A contour extraction method and a geometric control method integrating this method; contour extraction device and geometric control device integrating the extraction device
