Turbo-jet equipped with inclined balancing disks within the roto

Details Turbo-jet equipped with inclined balancing disks within the roto Turbo-jet equipped with inclined balancing disks within the roto

1994-09-30

1996-12-03

Thorpe, Timothy S.

Power plants

Combustion products used as motive fluid

Combustion products generator

60 3975, 60269, F02C 100

Patent

active

055796443

ABSTRACT:
A method and apparatus for maintaining or holding the rotor of a high pressure compressor of a very rigid turbojet during turbojet operation. The interior of the rotor of the high pressure compressor comprises upstream-inclined balancing disks (13) which are free of fly-weights. The centrifugal force applied to such balancing disks creates a load or stress on the disks having a radial component rending to compensate for the stresses towards the outside due to the blades, in front of which are positioned the balancing disks. The process for the production of such an exhaust cone is made easier, particularly with respect to the blank to be supplied for obtaining such a part.

REFERENCES:
patent: 2497151 (1950-02-01), Clark et al.
patent: 2548886 (1951-04-01), Howard
patent: 2869820 (1959-01-01), Merchant et al.
patent: 2922618 (1960-01-01), Paulson
patent: 4127988 (1978-12-01), Becker
patent: 4743165 (1988-05-01), Ulrich
patent: 5213475 (1993-05-01), Peterson et al.

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