IP Library Granted Patent US 9,429,073
Granted Patent B2
US 9,429,073 · App. 13/821,465 · Granted Aug 30, 2016

Hyperstatic truss comprising connecting rods

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Quick Facts
Patent No.
US 9,429,073
App. No.
13/821,465
Granted
Aug 30, 2016
Kind
B2
Abstract

A hyperstatic truss including connecting rods, used for suspension of a first ring, forming part of an engine case, inside a second ring concentric to the first ring, the connecting rods being secured at one end to the first ring and at the other end to the second ring. The tensile stiffness of the connecting rods is greater than the compressive stiffness thereof. The truss for example can be used for suspension of a ducted-fan turbine engine with an elongate bypass duct.

Claims (18)

1. A hyperstatic truss comprising:

connecting rods applied to suspending a first ring, that forms part of an engine casing, inside a second ring concentric with the first ring, the connecting rods being secured by a first end to the first ring and by a second end to the second ring,

wherein a tensile strength of the connecting rods is higher than a compressive strength of the connecting rods, said connecting rods comprising a set of one or more parts configured to transmit compressive and tensile loads between the ends of said connecting rods, and one or more other parts configured to cooperate with at least one part of said set of parts to transmit only tensile loads between the first a second ends of said connecting rods.

2. The truss as claimed in claim 1 , wherein the connecting rods comprise an internal rod and a shroud surrounding the internal rod, the internal rod configured to work in compression and in tension, the shroud working only in tension.

3. The truss as claimed in claim 2 , wherein the internal rod and the shroud of the connecting rods include a pair of mutually facing surfaces bearing against one another when tension is applied to the internal rod, the tensile loads then being transmitted between the two ends of the connecting rods by the internal rod and the shroud.

4. The truss as claimed in claim 3 , wherein the connecting rods comprise at least two pairs of bearing surfaces distributed at different axial locations along an axis of the internal rod.

5. The truss as claimed in claim 2 , wherein the connecting rods include a web which bears radially against an internal surface of the shroud, to prevent the internal rod from buckling when subjected to compressive stress.

6. The truss as claimed in claim 2 , wherein the internal rod is of cruciform cross section.

7. The truss as claimed in claim 2 , wherein the internal rod is threaded, with a plate that is axially movable and forms the bearing surface of the internal rod.

8. The truss as claimed in claim 2 , wherein the shroud of the connecting rods has an aerodynamic profile perpendicular to an axis of the connecting rods.

9. The truss as claimed in claim 1 , comprising six connecting rods arranged in a triangle tangentially to the first ring.

10. A front fan engine comprising:

an annular duct forming a bypass duct and an exhaust casing with a casing ring and a concentric ring in the shroud of the bypass duct,

the truss as claimed in claim 1 providing connection between the casing ring and concentric ring.

11. A hyperstatic truss comprising:

connecting rods applied to suspending a first ring, that forms part of an engine casing, inside a second ring concentric with the first ring, the connecting rods being secured by a first end to the first ring and by a second end to the second ring,

wherein a tensile strength of the connecting rods is higher than a compressive strength of the connecting rods, wherein the connecting rods include an internal rod and a shroud surrounding the internal rod, the internal rod working in compression and in tension, and the shroud working only in tension, and

wherein a first end of the shroud is secured to the internal rod, and a second end of the shroud includes a bearing surface which abuts a bearing surface provided on the internal rod when tension is applied to the internal rod such that tensile forces are transmitted between the first and second ends of the connecting rods by the internal rod and the shroud.

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 Mar 11, 2013
From: BELLABAL, FRANCOIS ROBERT; VINCENT, THOMAS ALAIN CHRISTIAN
To: SNECMA
Reel/Frame 029960/0638 →