IP Library › Granted Patent US 10,900,382
Granted Patent B2
US 10,900,382 · App. 15/745,788 · Granted Jan 26, 2021

Assembly comprising a locked securing stud

Inventors: Alain Dominique Gendraud (Vernou la Celle sur Seine, FR); Jean-Baptiste Vincent Desforges (Paris, FR); Arnaud Genilier (Bouray sur Juine, FR); Reda Oudyi (Lieusaint, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F01D25/243F16B39/24F16B2200/506
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Quick Facts
Patent No.
US 10,900,382
App. No.
15/745,788
Granted
Jan 26, 2021
Kind
B2
Abstract

An assembly includes a securing stud held by a locking key that rotates with the stud and is provided with bearing surfaces for sitting on an edge of one of the parts to be assembled.

Claims (12)

1. An assembly comprising:

a securing stud,

two superimposed flanges through which the stud passes,

a nut depending on one of the flanges and wherein one end of the securing stud is screwed,

a tightening nut screwed to an opposite end of the securing stud, and

a locking wrench tightened between the tightening nut and another of the flanges, the locking wrench comprising a main body provided with a bore, the bore having a non-circular cross-section and being occupied for a corresponding-cross-section portion of the stud,

wherein the main body is extended through a first portion extending beyond a border of said other flange in a direction perpendicular to the stud and then by a second portion projecting from the main body towards the stud and extending in front of said border, and

wherein said first portion is thinner than the main body, and is connected to the main body by a chamfer.

2. The assembly according to claim 1 , wherein the flanges belong to turbine cases assembled to each other by said flanges.

3. The assembly according to claim 1 , wherein the second portion projecting from the main body comprises a pair of separated journals on said other flange.

4. The assembly according to claim 3 , wherein the journals comprise rounded contours directed to said other case.

5. The assembly according to claim 3 , wherein the first portion which is an extension of the main body consists of two separated wings, each bearing one of the journals.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 18, 2018
From: GENDRAUD, ALAIN DOMINIQUE; DESFORGES, JEAN-BAPTISTE VINCENT; GENILIER, ARNAUD; OUDYI, REDA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 044653/0589 →
Priority Claims (1)
FR 15 56941 · Jul 22, 2015 · national
Continuity (1)
Related Publication 20180209302A1 · Jul 26, 2018
Cited By (3)
US 12,292,078 US 12,448,996 US 12,698,848