Axial and radial holding system for the rotor vane of a turbojet

Details Axial and radial holding system for the rotor vane of a turbojet Axial and radial holding system for the rotor vane of a turbojet

1982-12-22

1984-10-02

Marcus, Stephen

Fluid reaction surfaces (i.e., impellers)

Specific working member mount

Blade received in well or slot

416220R, F04D 532

Patent

active

044745354

ABSTRACT:
A blade holding system including a block 13 formed of an elongated part 15 having a lengthwise slot 18 extending over virtually its entire length. The longitudinal sides 181, 182 have openings 23 that receive an axle 17 holding a flexible strip 16 partially lodged in the slot. The flexible strip has two shanks 25, 26. The end 29 of one of the shanks 26 rests on one end 21 of the elongated part 15, the end 28 of the other shank 25 juts out from the lower plane of the elongated part 15 and, when the block 13 is in place between the blade foot 6 and the dovetail groove 2, is able to rest against the bottom 14 of the groove 2.

REFERENCES:
patent: 3383095 (1963-05-01), Anderson
patent: 4102602 (1978-07-01), Rottenkolber
patent: 4208170 (1980-06-01), Tucker et al.
patent: 4265595 (1981-05-01), Bucy et al.

Affiliated with

Also associated with

Rating

Axial and radial holding system for the rotor vane of a turbojet does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Axial and radial holding system for the rotor vane of a turbojet, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Axial and radial holding system for the rotor vane of a turbojet will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-525057