High-lift system

Patent metadata

Field	Value
Publication number	US-10272989-B2
Application number	US-201514948765-A
Country	US
Kind code	B2
Filing date	Nov 23, 2015
Priority date	Nov 26, 2014
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A high-lift system for an aircraft includes a high-lift flap which is arranged on the wing of the aircraft and is mounted on a carriage coupled to the wing, the carriage being displaceably mounted on a track by means of a high-lift bearing. The high-lift bearing includes a plain bearing.

First claim

What is claimed is:

1. A high lift system for an aircraft, comprising:
a wing;
a carriage coupled to the wing;
a high lift flap arranged on the wing and mounted to the carriage;
a track on which the carriage is displaceably mounted; and
a high lift bearing for mounting the track;
wherein the high lift bearing comprises a plurality of slide blocks in sliding contact with surfaces of the track;
wherein the slide blocks are trapezoidal, an angle on a side facing the track being an acute angle;
wherein the track comprises opposing flanges comprising a first flange and a second flange;
wherein the carriage comprises:
a joint, coupled to the high lift flap, and having a point of rotation;
a guide shoe overlying and flanking the flanges, and the guide shoe comprising four ends extending away from the joint; and
retaining structures arranged at opposite sides of the track, each retaining structure coupled to a respective one of the four ends of the guide shoe, and each retaining structure comprising two slide blocks arranged to be in sliding contact with surfaces of the track to accommodate movement of the carriage along the track;

wherein the two slide blocks of each retaining structure include a first slide block located to slide on an underside of a respective one of the flanges, and a second slide block located to slide on a lateral surface of the respective one of the flanges.

2. A high lift system according to claim 1 , wherein the slide blocks contain a material having a low coefficient of friction.

3. A high lift system according to claim 2 , wherein the slide block comprises a support body having a material as a sliding layer on a contact surface facing the track.

4. A high lift system according to claim 3 , wherein the material is applied as a coat, a layer, a coating or layer.

5. A high lift system according to claim 4 , wherein the material is selected from a group consisting of Teflon, fiber-reinforced Teflon, graphite, lead alloy, tin alloy, and sintered metal having lubricant imbedding in its pores.

6. A high-lift system for an aircraft, comprising:
a track arranged on a wing of the aircraft, the track having opposing flanges comprising a first flange and a second flange;
a high-lift flap arranged on the wing of the aircraft; and
a carriage coupled to the high-lift flap and displaceably mounted on the track, the carriage comprising:
a joint, coupled to the high-lift flap, and having a point of rotation;
a guide shoe overlying and flanking the flanges, and the guide shoe comprising four ends extending away from the joint; and
retaining structures arranged at opposite sides of the track, each retaining structure coupled to a respective one of the four ends of the guide shoe, and each retaining structure comprising two slide blocks arranged to be in sliding contact with surfaces of the track to accommodate movement of the carriage along the track;

wherein each of the slide blocks is trapezoidal, with an angle on a side facing the track being an acute angle; and
wherein the two slide blocks of each retaining structure include a first slide block located to slide on an underside of a respective one of the flanges, and a second slide block located to slide on a lateral surface of the respective one of the flanges.

7. The high-lift system according to claim 6 , wherein the slide blocks contain an engineering material having a low coefficient of friction.

8. The high-lift system according to claim 7 , wherein the slide blocks comprise a support body which is provided with the material as a sliding layer on a contact surface facing the track.

9. The high-lift system according to claim 7 , wherein the material is applied to the contact surface as a coat, a layer, a coating or a liner.

10. The high-lift system according to claim 7 , wherein the material having the low coefficient of friction is a material from the group consisting of Teflon, fibre-reinforced Teflon, graphite, lead alloy, tin alloy and sintered metal having lubricant embedded in the pores.

11. The high-lift system according to claim 7 , wherein the slide blocks are made of the material having a low coefficient of friction.

12. The high-lift system according to claim 6 , wherein the slide blocks comprise dirt guards which are arranged and formed such that dirt on the track is wiped off during operation.

13. The high-lift system according to claim 12 , wherein each of the dirt guards contains a brush or a rubber element.

14. The high-lift system according to claim 12 , wherein the dirt guard is trapezoidal, an angle on the side which faces the track being acute.

15. The high-lift system according to claim 6 , wherein a slide block comprises an abrasive-wear detection system.

16. The high-lift system according to claim 15 , wherein the abrasive-wear detection system comprises a graphite region which can be exposed once the slide block has been worn down by a predetermined thickness.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Havar Tamas
• Meyer Meinhard
• Fietzek Heiko

Classifications

• F16C33/26

  made from wire coils; made from a number of discs, rings, rods, or other members · CPC title

• B64C9/16 Primary

  at the rear of the wing · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• B64C9/14 Primary

  forming slots · CPC title

• F16C29/02

  Sliding-contact bearings · CPC title