Turbofan nacelle including a reverser flap

Patent metadata

Field	Value
Publication number	US-10655563-B2
Application number	US-201715823053-A
Country	US
Kind code	B2
Filing date	Nov 27, 2017
Priority date	Nov 28, 2016
Publication date	May 19, 2020
Grant date	May 19, 2020

Abstract

A nacelle has a fixed cowl and a mobile cowl, which is movable along a translation path between closing and opening positions, a window delimited by the fixed cowl and the mobile cowl and open between an airflow and exterior of the nacelle, a reverser flap rotatably mounted to move between closed and open positions, and a drive mechanism configured to control passage of the reverser flap between the closed and open positions as the mobile cowl moves between the closed and open positions. From the closing/closed positions, the drive mechanism assures a translation of the mobile cowl and a rotation of the reverser flap toward their respective opening/open positions. From the open/opening positions, the drive mechanism assures a rotation of the reverser flap and a translation of the mobile cowl toward their respective closed/closing position. In some embodiments, the nacelle further includes an additional, or second, flap.

First claim

The invention claimed is:

1. A nacelle for a turbofan, the nacelle comprising:
a fixed cowl and a mobile cowl, the mobile cowl being mobile along a translation path between a closing position, in which the mobile cowl is adjacent to the fixed cowl, and an opening position, in which the mobile cowl is far aft of the fixed cowl;
a window, which is delimited, on an upstream side thereof, by the fixed cowl and, on a downstream side thereof, by the mobile cowl, wherein the window is open between an airflow of a secondary flow and an exterior of the nacelle;
a reverser flap which is mounted in a manner rotatable about a rotation axis between a closed position, in which the window is obstructed, and an open position, in which the window is not obstructed;
a second flap, which is configured to rotate about a rotation axis between a retracted position, in which the second flap is not positioned in the airflow, and an active position, in which the second flap is positioned across the airflow, and extends from the reverser flap in the open position in the airflow; and
a drive mechanism comprising:
a motor element with a mobile part secured to the mobile cowl to drive the mobile part in translation;
a guide, which is secured to the mobile cowl and comprises a slide part, an axis of which is parallel to the translation path of the mobile cowl, and a rotation part that extends forward from the slide part and is offset relative to the slide part;
a slider accommodated in the guide;
a first link articulated between the slider and the reverser flap;
a second link articulated between the slider and the second flap; and
an abutment configured to move the slider from the rotation part toward the slide part when the reverser flap is in the closed position, the second flap is in the retracted position, and the mobile cowl is moved from the opening position to the closing position;

wherein the drive mechanism is configured to control passage of the reverser flap between and including the closed position to the open position, respectively, along with a passage of the mobile cowl between and including the closing position and the opening position, configured for a first combination assuring, from the closed position and from the closing position:
an aft translation of the mobile cowl along the translation path to move the mobile cowl from the closing position to the opening position, and
a rotation of the reverser flap about the rotation axis to move the reverser flap from the closed position to the open position, and

wherein the drive mechanism is also configured for a second combination assuring, from the open position and from the opening position:
a rotation of the reverser flap in a reverse direction about the rotation axis to move the reverser flap from the open position to the closed position, and
a forward translation of the mobile cowl along the translation path to move the mobile cowl from the opening position to the closing position, and

wherein the drive mechanism is configured to coordinate passage of the second flap from the retracted position to the active position along with the passage of the reverser flap between and including the closed position and the open position.

2. The nacelle of claim 1 , wherein the second flap carries a seal that is positioned between the reverser flap and the second flap when the reverser flap is in the open position and the second flap is in the active position.

3. The nacelle of claim 1 , comprising at least one deflector that is disposed around the airflow at a level of an entry of the window.

4. The nacelle of claim 1 , wherein the drive mechanism is configured to move the reverser flap and the mobile cowl simultaneously.

5. The nacelle of claim 1 , wherein the drive mechanism is configured to cause a delayed movement of the reverser flap in the first combination and a delayed movement of the mobile cowl in the second combination.

6. A turbofan comprising:
an engine; and
a nacelle according to claim 1 ,
wherein the nacelle is configured to surround the engine, and
wherein the airflow of the secondary flow is delimited between the nacelle and the engine.

7. An aircraft comprising at least one turbofan according to claim 6 .

Assignees

• Airbus Operations Sas
• Airbus Sas

Inventors

• Surply Thierry
• Porte Alain
• Oberle Patrick
• Haramburu Eric
• Sauvalle Thomas
• Letay Benoit
• Piard Frédéric
• Billerot Vincent
• Oundjian Franck

Classifications

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F02K1/70 Primary

  using thrust reverser flaps or doors mounted on the fan housing · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F02K1/763

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title

• F05D2250/42

  with two degrees of freedom · CPC title