Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device

Patent metadata

Field	Value
Publication number	US-9382814-B2
Application number	US-201313860726-A
Country	US
Kind code	B2
Filing date	Apr 11, 2013
Priority date	Oct 11, 2010
Publication date	Jul 5, 2016
Grant date	Jul 5, 2016

Abstract

A device for connecting a thrust reverser front frame to a fan casing includes a crenulated flange secured to the front frame, an annular component to accept this flange secured to the fan casing, and a crenulated annulus of a shape that complements the flange and pivot-mounted on the annular component. The crenulated flange, the annular component and the crenulated annulus are designed in such a way that a rotation of the annulus with respect to the annular component has the effect of locking this flange against this annular component through the collaboration between the respective crenulations of the flange and of the annulus.

First claim

What is claimed is:

1. A device for connecting a thrust reverser front frame to a fan casing, said device comprising:
a crenulated flange annular in shape and having radially outward extending teeth with notches in between the teeth, the crenlated flange secured to said thrust reverser front frame;
an annular component to accept said crenulated flange, secured to said fan casing; and
a crenulated annulus having radially inward extending teeth with notches between the teeth shaped to compliment the radially outward extending teeth of said crenulated flange, the crenulated annulus pivot-mounted on and slidable about said annular component,
wherein said crenulated flange, said annular component, and said crenulated annulus are configured so that the crenulated flange slides axially into through the notches of the crenulated annulus and subsequent rotation of said crenulated annulus with respect to the relatively stationary annular component and crenulated flange has the effect of axially coupling said crenulated flange against said annular component through axial alignment of the teeth of said crenulated flange and the teeth of said crenulated annulus, and said annular component has a radial abutment lip against the notches of said crenulated flange, the radial abutment lip covered by said crenulated annulus.

2. The connecting device according to claim 1 , wherein said radial abutment lip has an i-shaped section.

3. The connecting device according to claim 1 , wherein said radial abutment lip has an L-shaped section.

4. The connecting device according to claim 3 , wherein said radial abutment lip and the notches of said crenulated flange have mutual cooperation surfaces inclined relative to a transverse plane.

5. The connecting device according to claim 4 , wherein an incline value of said mutual cooperation surfaces is approximately 30 degrees.

6. The connecting device according to claim 1 , wherein teeth of said crenulated flange have circumferential bevels.

7. The connecting device according to claim 1 , wherein said crenulated flange and said annular component have radial bevels.

8. The connecting device according to claim 1 , wherein the notches of said crenulated flange and said crenulated annulus have a larger circumferential length at a 12 o'clock position than at a six o'clock position.

9. The connecting device according to claim 1 , wherein said annular component includes a seal.

10. The connecting device according to claim 1 , wherein said crenulated annulus includes a slot, passed through by means for rotating said crenulated annulus.

11. The connecting device according to claim 10 , wherein said means comprise a pinion cooperating with a rack secured to said crenulated annulus.

12. The connecting device according to claim 10 , wherein said means comprise a control screw cooperating with a nut secured to said crenulated annulus.

13. A turbojet engine nacelle for an aircraft including the connecting device according to claim 1 .

Assignees

• Aircelle Sa

Inventors

• Bunel Serge
• Peyron Vincent
• Kioua Hazem
• Lescure Jerome

Classifications

• F01D25/243 Primary

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• F05D2260/50

  Kinematic linkage, i.e. transmission of position · CPC title

• F01D25/28 Primary

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F16B2/14

  using wedges · CPC title