IP Library Granted Patent US 9,039,567
Granted Patent B2
US 9,039,567 · App. 14/321,956 · Granted May 26, 2015

Device with multiple reduction gear transmission between a drive shaft and a pair of propellers coaxial with this shaft

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Quick Facts
Patent No.
US 9,039,567
App. No.
14/321,956
Granted
May 26, 2015
Kind
B2
Abstract

A transmission to drive two propellers through a single shaft comprises several, generally three planetary gear systems, each of which comprises one principal element directly supported on fixed surrounding structures that resist cantilever forces, support the rotating bodies and carry fluid and electrical cable ducts to control the operation of the downstream propeller elsewhere than through the central shaft of the machine in which the volume is reduced.

Claims (12)

1. Aircraft propulsion device comprising a drive shaft, a pair of propellers coaxial with the drive shaft, and a transmission between the drive shaft and the pair of propellers, the transmission including a planetary gearing speed reduction device for the drive shaft, the reduction device comprising a plurality of planetary gear systems each comprising a toothed sun gear, a toothed ring gear and toothed planet gears mounted on a planet gear carrier and each engaged with the sun gear and the ring gear, the sun gear, the ring gear and the planet gear carrier forming three principal elements of each planetary gear system, one of the principal elements of two of the planetary gear systems being fixed to one of the propellers, wherein there are three planetary gear systems, one of the principal elements of a first of said three planetary gear systems is fixed to the drive shaft, a second and a third of said three planetary gear systems comprise the principal elements fixed to the propellers, and one of the principal elements of each of the planetary gear systems is fixed to a fixed structure surrounding the drive shaft.

2. Device according to claim 1 , wherein the elements fixed to the fixed structure are the planet gear carrier in the first planetary gear system, the planet gear carrier in the second planetary gear system and the ring gear in the third planetary gear system.

3. Device according to claim 2 , wherein the ring gear in the first planetary gear system, the sun gear in the second planetary gear system and the sun gear in the third planetary gear system are fixed to each other and form a rotating assembly.

4. Device according to claim 1 , wherein the principal elements fixed to the fixed structure are the ring gear in the first planetary gear system, the planet gear carrier in the second planetary gear system and the ring gear in the third planetary gear system.

5. Device according to claim 2 , wherein the principal elements fixed to the propellers are the ring gear in the second planetary gear system and the planet gear carrier in the third planetary gear system.

6. Device according to claim 1 , wherein the principal elements fixed to the fixed structure are the ring gear in the first planetary gear system, the planet gear carrier in the second planetary gear system and the planet gear carrier in the third planetary gear system.

7. Device according to claim 4 , wherein in that the planet gear carrier in the first planetary gear system, the sun gear ( 35 ) in the second planetary gear system and the sun gear in the third planetary gear system are fixed to each other and form a rotating assembly.

8. Device according to claim 6 , wherein the principal elements fixed to the propellers are the ring gear in the second planetary gear system and the ring gear in the third planetary gear system.

9. Device according to claim 1 , wherein it comprises propeller control modules, and networks for supplying said modules, said networks extending along said fixed structure.

10. Device according to claim 9 , wherein propeller control modules are placed adjacent to each other on the fixed structure.

11. Device according to claim 4 , wherein the principal elements fixed to the propellers are the ring gear in the second planetary gear system and the planet gear carrier in the third planetary gear system.

12. Device according to claim 6 , wherein the planet gear carrier in the first planetary gear system, the sun gear in the second planetary gear system and the sun gear in the third planetary gear system are fixed to each other and form a rotating assembly.

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 Aug 6, 2014
From: FABRE, ADRIEN JACQUES PHILIPPE
To: SNECMA
Reel/Frame 033472/0048 →