IP Library › Granted Patent US 11,073,043
Granted Patent B2
US 11,073,043 · App. 16/733,855 · Granted Jul 27, 2021

Deflector for the fairing of a turbomachine pinion, associated gear box and turbomachine

Inventor: Maxence Gérard Claude Guillemont (Moissy Cramayel, FR)
Assignee: SAFRAN TRANSMISSION SYSTEMS
F01D25/24F04D29/06F04D29/5806
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Quick Facts
Patent No.
US 11,073,043
App. No.
16/733,855
Granted
Jul 27, 2021
Kind
B2
Abstract

A deflector for the fairing of a pinion, which includes a teething, a barrel and a wall positioned between the teething and the barrel, the deflector extending around an axis and including an envelope of which the shape and the dimensions are suited to surrounding at least one part of the teething of the pinion, the deflector including an oil injection circuit including a first portion provided on an outer surface of the envelope, a first injection hole provided in the envelope and communicating with the first portion of the oil injection circuit, the first injection hole emerging on an inner surface of the envelope so as to inject oil in the direction of the pinion, a second portion communicating with the first portion, the second portion including a second injection hole intended to be facing the inside of the barrel of the pinion.

Claims (12)

1. A deflector for the fairing of at least one turbomachine pinion, said at least one turbomachine pinion comprising a teething, a barrel and a wall positioned between the teething and the barrel, the deflector extending around an axis and comprising an envelope of which the shape and the dimensions are suited to surrounding at least one part of the teething of the at least one turbomachine pinion, the deflector comprising an oil injection circuit comprising:

a first portion provided on an outer surface of the envelope;

at least one first injection hole provided in the envelope and communicating with the first portion of the oil injection circuit, said at least one first injection hole emerging on an inner surface of the envelope so as to inject oil in the direction of the at least one turbomachine pinion, and

a second portion communicating with the first portion, said second portion comprising at least one second injection hole facing the inside of the barrel of the at least one turbomachine pinion.

2. The deflector according to claim 1 , wherein said at least one first injection hole is configured to emerge facing the teething of the at least one turbomachine pinion.

3. The deflector according to claim 1 , wherein said at least one first injection hole and said at least one second injection hole have a diameter comprised in the interval [0.5; 5 mm].

4. The deflector according to claim 1 , wherein the first portion and the second portion of the oil injection circuit form a pipe provided with a bend at a connecting junction between the first portion and the second portion.

5. The deflector according to claim 1 , wherein the envelope comprises a fastening flange having fastening orifices.

6. The deflector according to claim 5 , wherein the fastening flange is scalloped.

7. A turbomachine gear box comprising at least one turbomachine pinion, and the deflector according to claim 1 , said deflector fairing the at least one turbomachine pinion.

8. The turbomachine gear box according to claim 7 , wherein the at least one turbomachine pinion is conical.

9. A turbomachine comprising at least one deflector according to claim 1 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 4, 2020
From: GUILLEMONT, MAXENCE GÉRARD CLAUDE
To: SAFRAN TRANSMISSION SYSTEMS
Reel/Frame 052014/0336 →
Priority Claims (1)
FR 1900057 · Jan 4, 2019 · national
Continuity (1)
Related Publication 20200217222A1 · Jul 9, 2020
Cited By (1)
US 12,540,667