Fan cowl fairing restraining system

Patent metadata

Field	Value
Publication number	US-10611490-B2
Application number	US-201615341705-A
Country	US
Kind code	B2
Filing date	Nov 2, 2016
Priority date	Nov 2, 2016
Publication date	Apr 7, 2020
Grant date	Apr 7, 2020

Abstract

A nacelle tensioning arrangement may comprise a fairing located between a first fan cowl and a second fan cowl, and a flexible tensioning system configured to restrain at least a portion of the fairing from moving in a radial direction in response to at least one of the first fan cowl and the second fan cowl being in a closed position.

First claim

We claim:

1. A nacelle tensioning arrangement comprising:
a fairing located between a first fan cowl and a second fan cowl, and
a tensioning system comprising:
a first cable attachment member configured to be coupled to the first fan cowl; and
a cable configured to be extended between the first cable attachment member and the fairing;

wherein the first cable is configured to restrain at least a portion of the fairing from moving in a radial direction in response to at least one of the first fan cowl and the second fan cowl being in a closed position.

2. The nacelle tensioning arrangement of claim 1 , wherein the tensioning system further comprises:
a cable guidance system;
and
a second cable attachment member.

3. The nacelle tensioning arrangement of claim 2 , wherein
the second cable attachment member is configured to be coupled to the second fan cowl,
the cable guidance system is configured to be coupled to a forward edge of the fairing via a hinge beam stirrup, and
the cable is configured to extend between the first cable attachment member and the second cable attachment member, via the cable guidance system.

4. The nacelle tensioning arrangement of claim 3 , wherein an aft edge of the fairing is mounted to a pylon.

5. The nacelle tensioning arrangement of claim 4 , wherein a first end of the cable is coupled to the first cable attachment member and a second end of the cable is coupled to the second cable attachment member,
the first end of the cable configured to wrap around the first cable attachment member in response to the first fan cowl moving to the closed position, and
the second end of the cable configured to wrap around the second cable attachment member in response to the second fan cowl moving to the closed position.

6. The nacelle tensioning arrangement of claim 5 , wherein the cable guidance system comprises a plurality of rollers coupled to the forward edge of the fairing.

7. The nacelle tensioning arrangement of claim 6 , wherein the cable guidance system further comprises a roller coupled to an aft edge of a nacelle inlet and located radially inward from the plurality of rollers coupled to the forward edge of the fairing.

8. The nacelle tensioning arrangement of claim 1 , wherein the tensioning system further comprises:
a second cable;
the first cable attachment member coupled to a first hinge of the first fan cowl; and
a second cable attachment member coupled to a second hinge of the second fan cowl,
wherein the cable is coupled between the first cable attachment member and the fairing, and the second cable is coupled between the second cable attachment member and the fairing.

9. A nacelle for a turbine engine comprising:
a first fan cowl;
a second fan cowl;
a fairing located between the first fan cowl and the second fan cowl; and
a tensioning system comprising a cable;
the cable is coupled between the first fan cowl, a forward edge of the fairing, and the second fan cowl,
wherein the cable provides tension between the first fan cowl, the forward edge of the fairing, and the second fan cowl.

10. The nacelle of claim 9 , wherein the cable provides the tension in response to at least one of the first fan cowl and the second fan cowl rotating to a closed position, and the cable loses tension in response to at least one of the first fan cowl and the second fan cowl rotating to an open position.

11. The nacelle of claim 10 , wherein an aft edge of the fairing is mounted to a pylon.

12. The nacelle of claim 11 , wherein the tensioning system further comprises:
a cable guidance system;
a first cable attachment member; and
a second cable attachment member.

13. The nacelle of claim 12 , wherein
the first cable attachment member is configured to be coupled to the first fan cowl and the second cable attachment member is configured to be coupled to the second fan cowl,
the cable guidance system is configured to be coupled to the forward edge of the fairing, and
the cable is configured to extend between the first cable attachment member and the second cable attachment member, via the cable guidance system.

14. The nacelle of claim 13 , wherein a first end of the cable is coupled to the first cable attachment member and a second end of the cable is coupled to the second cable attachment member,
the first end of the cable configured to wrap around the first cable attachment member in response to the first fan cowl moving to the closed position, and
the second end of the cable configured to wrap around the second cable attachment member in response to the second fan cowl moving to the closed position.

15. The nacelle of claim 14 , wherein the cable guidance system comprises a plurality of rollers coupled to the forward edge of the fairing.

16. The nacelle of claim 15 , further comprising a nacelle inlet located forward of the fairing, the first fan cowl, and the second fan cowl.

17. The nacelle of claim 16 , wherein the cable guidance system further comprises a roller coupled to an aft edge of the nacelle inlet, the roller located radially inward from the plurality of rollers coupled to the forward edge of the fairing.

18. The nacelle of claim 9 , wherein the tensioning system comprises:
a first cable;
a second cable;
a first cable attachment member coupled to the first fan cowl; and
a second cable attachment member coupled to the second fan cowl,
wherein the first cable is coupled between the first cable attachment member and the fairing,
and the second cable is coupled between the second cable attachment member and the fairing.

19. A method for restraining a forward edge of a nacelle fairing comprising:
rotating a fan cowl from an open position to a closed position; and
generating tension, via a cable of a tensioning system, between the nacelle fairing and the fan cowl, in response to the rotation.

20. The method of claim 19 , further comprising:
wrapping the cable around a cable attachment member in response to the rotation, the tensioning system comprising the cable, and the cable attachment member coupled to a hinge of the fan cowl.

Assignees

• Rohr Inc

Inventors

• Paolini Thomas
• Schommer Marc

Classifications

• B64D29/06 Primary

  Attaching of nacelles, fairings or cowlings · CPC title

• B64D27/16

  of jet type · CPC title