A variable geometry turbocharger assembly (90) employing the present invention includes a center housing (92), a compressor housing attached to one side of the center housing, and a turbine housing (94) attached to another side of the center housing.

This device can include a central housing, a pump disposed in the central housing and at least one display disposed in the central housing.

A gas turbine engine includes a core housing providing a core flowpath.

A turbocharger (62) comprises a center housing (64) interposed between a compressor housing (68) and a turbine housing (66) .

The front axle case has a central case molded body (70) and has left and right case molded bodies (71) whose base end sections are connected to left and right end sections of the central case molded body.

A gas turbine engine includes a core housing that includes an inlet case and an intermediate case that respectively provide an inlet case flow path and an intermediate case flowpath.

The actuator (22) is provided to the center housing (17).

A turbine housing (215) is connected to the center housing (202) and disposed around the turbine wheel (212).

A first gasket (31) is interposed between the flange part (6a) of the front housing (6) and the center housing (5).

According to the invention, therefore, the casing of the motor is divided into a main central casing (10) and the front and rear end casings (12, 14).

The so-formed stator (30) is disposed within a motor housing (24) and together, the stator (30) and motor housing (24), facilitate placement center housing (20) axial end therein to minimize turbocharger axial length.

The turbine engine includes structural means (72) for stiffening the central casing, surrounded by the shell (56) and extending backward between the upstream shroud (54) and the central casing (18) on which said means (72) are mounted.

The invention relates to a turbine engine for an aircraft, including shell means (36) arranged as a rear extension of an inner shroud (22) of an intermediate casing and provided around a central casing (18).

A variable-nozzle turbocharger includes a cartridge containing a variable vane mechanism connected between the center housing and the turbine housing.

A variable-nozzle turbocharger includes a cartridge (50) containing a variable vane mechanism connected between the center housing (20) and the turbine housing (24).