Suspension structure with variable geometry of a turboprop engine on a structural element of an aircraft

Patent metadata

Field	Value
Publication number	US-9738392-B2
Application number	US-201414762281-A
Country	US
Kind code	B2
Filing date	Jan 15, 2014
Priority date	Jan 21, 2013
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

A variable geometry suspension structure for suspending a turboprop from a structural element of an aircraft, the structure including a rear cradle for fastening to a structural element of an aircraft and a front cradle for supporting a front portion of the turboprop, the front cradle being connected to the rear cradle, firstly via a pivot connection configured to enable the front cradle to tilt vertically relative to the rear cradle, and secondly by a return spring configured to prevent the front cradle from tilting while thrust from the turboprop is below a predetermined threshold.

First claim

The invention claimed is:

1. A variable geometry suspension structure for suspending a turboprop from a structural element of an aircraft, the structure comprising:
a rear cradle for fastening to a structural element of an aircraft; and
a front cradle supporting a front portion of the turboprop,
the front cradle being connected to the rear cradle, firstly via a pivot connection configured to enable the front cradle to tilt vertically relative to the rear cradle, and secondly by a return spring configured to prevent the front cradle from tilting while thrust from the turboprop is below a predetermined threshold.

2. A structure according to claim 1 , further comprising means for preventing any lateral movement of the front cradle relative to the rear cradle.

3. A structure according to claim 2 , wherein the rear cradle includes at least one rod including a wheel configured to slide in an axial slot formed in the front cradle to prevent any lateral movement of the front cradle relative to the rear cradle.

4. A structure according to claim 3 , wherein the slot is closed at its axial ends to limit angular amplitude of the tilting of the front cradle.

5. A structure according to claim 3 , wherein the rod includes two branches forming a rearwardly-open V-shape, the wheel being positioned at an intersection between the branches of the rod.

6. A structure according to claim 3 , wherein the rear cradle includes two rods positioned angularly on either side of the return spring.

7. A structure according to claim 1 , wherein the return spring includes a hydraulic damper controlled by a valve to enable the position of the front cradle to be blocked on command of the pilot.

8. A structure according to claim 1 , wherein the return spring possesses stiffness that is calculated so that its return force is greater than thrust from the turboprop corresponding to the aircraft being in a stage of cruising flight, and less than turboprop thrust from the turboprop corresponding to the aircraft being in a takeoff and climb stage.

9. A structure according to claim 1 , wherein the rear cradle does not have means for supporting the turboprop.

10. A structure according to claim 1 , further comprising means for taking up the driving torque from the propeller of the turboprop.

11. A structure according to claim 10 , further comprising a torsion bar for taking up the drive torque, which torsion bar is connected at each of its ends to the rear cradle by connecting rods, and is for fastening to the underside of the turboprop.

12. An aircraft comprising at least one turboprop mounted on a structural element by a variable geometry suspension structure according to claim 1 .

Assignees

• Snecma

Inventors

• Hellegouarch Antoine
• Poisson Mathieu Ange
• Gallet Francois

Classifications

• B64D27/402

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• F02C7/20 Primary

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• B64D27/10

  of gas-turbine type  (jet aircraft B64D27/16) · CPC title

• B64D27/26 Primary

  Operations & Transport · mapped topic

• B64D27/14

  within, or attached to, fuselages · CPC title