IP Library Patent Application 14650043
Patent Application
App. No. 14/650,043

A METHOD OF BALANCING A TURBINE ENGINE ROTOR, AND A ROTOR BALANCED BY SUCH A METHOD

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Quick Facts
Patent No.
US None
App. No.
14/650,043
Abstract

A method of balancing a turbine engine rotor, the method including mounting screws forming balance weights on the rotor in order to form a balance configuration, each screw possessing a predetermined weight and a screw head having a visual characteristic previously associated with its weight. A rotor balanced by such a method is also disclosed.

Claims (13)

1 - 12 . (canceled)

13 . A method of balancing a turbine engine rotor, the method comprising mounting screws forming balance weights on the rotor in order to form a balance configuration, each screw possessing a predetermined weight and a screw head having a visual characteristic previously associated with its weight.

14 . A method according to claim 13 , including a prior step of establishing a table in which each particular visual characteristic of a screw head is associated with a predetermined screw weight.

15 . A method according to claim 13 , wherein the visual characteristics of the screw heads include particular shapes and/or colors.

16 . A method according to claim 13 , wherein the balance configuration is stored in a memory of an electronic computer of the turbine engine and is then transmitted automatically to a database of a maintenance center.

17 . A method according to claim 16 , wherein the installed balance configuration is transmitted to a technician during an operation of replacing the electronic computer.

18 . A method according to claim 16 , wherein a balance recommendation is calculated by the maintenance center in the event of vibration being detected in operation, and the recommendation is transmitted to a technician.

19 . A turbine engine rotor including screws forming balance weights that are mounted on the rotor, each screw possessing a predetermined weight and a screw head having a visual characteristic previously associated with its weight.

20 . A rotor according to claim 19 , wherein the screw heads are of different shapes.

21 . A rotor according to claim 20 , wherein the screw head shapes are selected from square, round, hexagonal, cross-shaped, star-shaped, and ring-shaped.

22 . A rotor according to claim 19 , wherein the screw heads are of different colors.

23 . A rotor according to claim 19 , said rotor forming a fan.

24 . A turbine engine having a rotor according to claim 19 .

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 5, 2015
From: NICQ, GEOFFROY
To: SNECMA
Reel/Frame 035793/0838 →