IP Library Granted Patent US 8,136,341
Granted Patent B2
US 8,136,341 · App. 11/732,026 · Granted Mar 20, 2012

Track beam for the cowling of jet engines

Assignee: FACC AG
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Quick Facts
Patent No.
US 8,136,341
App. No.
11/732,026
Granted
Mar 20, 2012
Kind
B2
Abstract

Track beams for the cowling of a jet engine for aircraft are formed of a base body with at least one slide for displaceably mounting a thrust reverser of the jet engine. A connection is provided for an inner engine cowling and fittings for detachably and pivotally attaching to a supporting structure or for connecting to another track beam. To provide such a track beam which has a particularly low weight yet, nevertheless, is sufficiently stiff, the base body is formed by a hollow profile section with a substantially closed cross-section. The hollow section is produced of a carbon-fiber-reinforced synthetic material by way of a resin-infusion process. Two flanges are provided on the hollow section of the base body of the track beam for providing a connection to the inner engine cowling.

Claims (30)

1. A track beam for the cowling of an aircraft jet engine, comprising:

a base body having at least one sliding device for displaceably mounting a thrust reverser of the jet engine;

said base body being formed as a hollow section with a closed cross-section, said hollow section being formed of a carbon-fiber-reinforced synthetic material by way of a resin-infusion process;

a connection for an inner engine cowling; and

fittings disposed in openings formed in said base body for a detachable and pivotable attachment to a supporting structure or for connection to another track beam.

2. The track beam according to claim 1 , wherein said hollow section is made of a carbon-fiber-reinforced synthetic material in a resin transfer molding process.

3. The track beam according to claim 1 , wherein said hollow section contains prefabricated carbon fabric parts.

4. A track beam for the cowling of an aircraft jet engine, comprising:

a base body having at least one sliding device for displaceably mounting a thrust reverser of the jet engine;

said base body being formed as a hollow section with a closed cross-section, said hollow section being formed of a carbon-fiber-reinforced synthetic material by way of a resin-infusion process;

a connection for an inner engine cowling; and

fittings for a detachable and pivotable attachment to a supporting structure or for connection to another track beam, said fittings being disposed in openings formed in said base body, said fittings being integrally formed with said hollow section of said base body in a unitary, single part.

5. The track beam according to claim 1 , wherein said fittings are formed of carbon-fiber-reinforced synthetic material in a resin infusion process and subsequently connected to said hollow section.

6. The track beam according to claim 5 , wherein said fittings are glued to said hollow section.

7. The track beam according to claim 1 , wherein said fittings are metal fittings connected to said hollow section.

8. The track beam according to claim 7 , wherein said metal fittings are glued to said hollow section.

9. The track beam according to claim 1 , wherein said hollow section contains reinforcing carbon fabric.

10. The track beam according to claim 9 , wherein said hollow section and said fittings contain reinforcing carbon fabric.

11. The track beam according to claim 9 , which comprises reactive materials integrated in said carbon fabric.

12. The track beam according to claim 11 , wherein said reactive materials include nylon sewed or woven into said carbon fabric.

13. The track beam according to claim 1 , wherein said hollow section includes two flanges defining connection devices for the inner engine cowling, formed such that an end of the inner engine cowling is insertible between said flanges.

14. The track beam according to claim 13 , wherein the inner engine cowling is glued to said hollow section.

15. The track beam according to claim 13 , wherein said flanges are formed with at least one bore for receiving therein a connecting element.

16. The track beam according to claim 15 , wherein said connecting element is a bolt or a screw.

17. The track beam according to claim 13 , which further comprises additional cover layers of fiber-reinforced synthetic material glued to the inner engine cowling and to said hollow section.

18. The track beam according to claim 1 , wherein said hollow section contains stiffening structures.

19. The track beam according to claim 1 , which comprises stiffening ribs integrated in said hollow section.

20. The track beam according to claim 1 , wherein said hollow section is formed with grooves forming said sliding devices for displaceably mounting the thrust reverser.

21. The track beam according to claim 20 , wherein said grooves are formed of carbon fabric integrated in a production process of said hollow section.

22. The track beam according to claim 20 , wherein said grooves are formed with a circular arc cross-section.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 27, 2011
From: STEPHAN, WALTER; ZEILLINGER, ROLAND; MAIER, ANDREAS
To: FISCHER ADVANCED COMPOSITE COMPONENTS AG
Reel/Frame 027133/0937 →
CHANGE OF NAME Recorded Feb 11, 2009
From: FISCHER ADVANCED COMPOSITE COMPONENTS AG
To: FACC AG
Reel/Frame 022240/0949 →
Priority Claims (1)
AT A 1065/2006 · Jun 23, 2006 · national
Continuity (1)
Related Publication 20070294996A1 · Dec 27, 2007