Apparatus and methods for actuating a double-slotted flap using a slave screw

Patent metadata

Field	Value
Publication number	US-11046425-B2
Application number	US-201716302869-A
Country	US
Kind code	B2
Filing date	Mar 18, 2017
Priority date	May 20, 2016
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

Apparatus and methods for actuating a double-slotted flap movably coupled to an aircraft wing are disclosed. An exemplary method comprises actuating a first panel of the double-slotted flap relative to a structure of the aircraft wing, using motion of the first panel to induce rotation of a slave screw, and using the rotation of the slave screw to actuate the second panel relative to the first panel.

First claim

What is claimed is:

1. An apparatus for actuating a double-slotted flap movably coupled to an aircraft wing where the double-slotted flap comprises a first panel and a second panel movable relative to the first panel, the apparatus comprising:
an actuator configured to actuate the first panel of the double-slotted flap relative to a structure of the aircraft wing; and
a slave-drive assembly comprising:
a slave screw; and
a drive screw drivingly coupled to the slave screw and actuating the second panel relative to the first panel;

wherein the slave screw is induced to rotate by motion of the first panel; and
wherein the drive screw is coupled to the second panel via a link comprising a primary connection and a secondary connection, wherein the primary connection comprises a shear pin; and
wherein the secondary connection allows a certain play with respect to the first connection so as to permit backlash between the drive screw and the second panel.

2. The apparatus as defined in claim 1 , wherein the slave screw and the drive screw are drivingly coupled in series via a universal joint.

3. The apparatus as defined in claim 1 , wherein the slave screw has a first thread pitch and the drive screw has a second thread pitch, and wherein the first thread pitch is greater than the second thread pitch.

4. The apparatus as defined in claim 1 , wherein an amount of backlash between the drive screw and the second panel is configured to cause a monitoring system to detect a fault.

5. The apparatus as defined in claim 1 , wherein the slave-drive assembly comprises a drive nut engaged with the drive screw for transferring rotary motion of the drive screw into motion of the second panel relative to the first panel.

6. The apparatus as defined in claim 1 , wherein the slave-drive assembly comprises:
a slave nut engaged with the slave screw and secured to the structure of the aircraft wing; and
a motion transfer device secured to the first panel of the double-slotted flap for converting motion of the first panel into motion of the slave screw through the slave nut to induce rotation of the slave screw.

7. An aircraft comprising the apparatus as defined in claim 1 .

Assignees

• Bombardier Inc

Inventors

• Wagner Paul
• Harris Richard
• Goldmann Matthew

Classifications

• F16H25/20

  Screw mechanisms (with automatic reversal F16H25/12) · CPC title

• B64C9/20 Primary

  by multiple flaps · CPC title

• Y02T50/30

  Wing lift efficiency · CPC title

• B64C13/28 Primary

  mechanical · CPC title

• B64C9/16

  at the rear of the wing · CPC title