Deflection limiter for a cascade assembly of a thrust reverser

Patent metadata

Field	Value
Publication number	US-10428764-B2
Application number	US-201615040274-A
Country	US
Kind code	B2
Filing date	Feb 10, 2016
Priority date	Feb 10, 2016
Publication date	Oct 1, 2019
Grant date	Oct 1, 2019

Abstract

A cascade assembly of a nacelle for a turbofan engine includes a cascade concentrically disposed about an centerline, and a translating sleeve constructed and arranged to move between a forward position and an aft position along the centerline. A deflection limiter of the cascade assembly includes a first surface facing at least in-part in a radial direction and a second surface facing at least in-part in an opposite radial direction. The first surface is carried by one of the cascade and the translating sleeve and the second surface is carried by the other of the cascade and the translating sleeve. The first and second surfaces oppose one-another for limiting deflection when the translating sleeve is in the aft position and are spaced axially apart when the translating sleeve is in the forward position.

First claim

I claim:

1. A cascade assembly of a nacelle for a turbofan engine comprising:
a cascade centered to and extending about a centerline;
a translating sleeve constructed and arranged to move between a forward position and an aft position along the centerline; and
a deflection limiter including a first surface facing at least in-part in a radial direction and carried by one of the cascade and the translating sleeve and a second surface facing at least in-part in an opposite radial direction and carried by the other of the cascade and the translating sleeve, and wherein the first and second surfaces oppose one-another for limiting deflection when the translating sleeve is in the aft position and are spaced axially apart when the translating sleeve is in the forward position;
wherein the cascade is a translating cascade constructed and arranged to move between a stowed state and a deployed state along the centerline, and wherein the deflection limiter is mated for transferring load when the translating sleeve is in the aft position and the translating cascade is in the deployed state, and is un-mated when the translating sleeve is in the forward position and the translating cascade is in the stowed state;
wherein the first surface is carried by a first catch of the deflection limiter fixed to the translating sleeve and the second surface is carried by a second catch of the deflection limiter fixed to the cascade, and wherein the first and second catches are constructed and arranged to mate when the translating sleeve is in the aft position and is un-mated when the translating sleeve is in the forward position; and
a fixed structure;
a hook device including a third catch fixed to the fixed structure and a fourth catch fixed to a forward portion of the cascade, and wherein the third catch is mated to the fourth catch for translating load when the translating cascade is in the deployed state and the translating sleeve is in the aft position; and
wherein the second surface is carried by an aft portion of the cascade disposed axially rearward of the forward portion.

2. The cascade assembly set forth in claim 1 , wherein the translating cascade is a one-piece cascade.

3. The cascade assembly set forth in claim 1 , wherein the aft portion is a cascade hoop.

4. The cascade assembly set forth in claim 1 , wherein the fixed structure includes a fan case.

5. The cascade assembly set forth in claim 1 , wherein the first catch is axially spaced forward of the second catch when the translating sleeve is in the forward position, and wherein during deployment the first catch is mated to the second catch when the translating sleeve is moving from a mid-position to the aft position.

6. A cascade assembly of a nacelle for a turbofan engine comprising:
a cascade centered to and extending about a centerline;
a translating sleeve constructed and arranged to move between a forward position and an aft position along the centerline; and
a deflection limiter including a first surface facing at least in-part in a radial direction and carried by one of the cascade and the translating sleeve and a second surface facing at least in-part in an opposite radial direction and carried by the other of the cascade and the translating sleeve, and wherein the first and second surfaces oppose one-another for limiting deflection when the translating sleeve is in the aft position and are spaced axially apart when the translating sleeve is in the forward position;
wherein the cascade is a translating cascade constructed and arranged to move between a stowed state and a deployed state along the centerline, and wherein the deflection limiter is mated for transferring load when the translating sleeve is in the aft position and the translating cascade is in the deployed state, and is un-mated when the translating sleeve is in the forward position and the translating cascade is in the stowed state;
wherein the first surface is carried by a first catch of the deflection limiter fixed to the translating sleeve and the second surface is carried by a second catch of the deflection limiter fixed to the cascade, and wherein the first and second catches are constructed and arranged to mate when the translating sleeve is in the aft position and is un-mated when the translating sleeve is in the forward position;
wherein the cascade includes a forward portion and an aft portion located axially rearward of the forward portion and the second catch is fixed to the aft portion;
wherein the first catch is axially spaced forward of the second catch when the translating sleeve is in the forward position, and wherein during deployment the first catch is mated to the second catch when the translating sleeve is moving from a mid-position to the aft position; and
wherein the first catch includes a first portion projecting radially inward from the translating sleeve and at a pin-like second portion projecting axially rearward from the first portion, and wherein the second catch includes a first segment projecting radially outward from the aft portion of the translating cascade and defining a hole for receipt of the pin-like second portion when the deflection limiter is mated.

7. The cascade assembly set forth in claim 1 , wherein the third catch includes a first portion projecting radially outward from the fixed structure and a second portion projecting axially forward from the first portion, the first and second portions defining at least in-part a channel, and wherein the fourth catch includes a first segment projecting radially inward from the translating cascade and a second segment projecting axially aft of the first segment such that the second segment is disposed in the channel when the translating cascade is in the deployed state.

8. The cascade assembly set forth in claim 7 , wherein the fixed structure includes a shear web projecting at least in-part axially rearward and the first portion of the third catch is attached to the shear web.

9. The cascade assembly set forth in claim 1 , wherein the fixed structure includes a shear web projecting at least in-part axially rearward and the third catch is attached to the shear web.

Assignees

• Rohr Inc

Inventors

• Crawford Sara Christine

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

• F02K1/72 Primary

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F04D29/522

  especially adapted for elastic fluid pumps · CPC title

• F02K1/766

  with blocking systems or locking devices; Arrangement of locking devices for thrust reversers · CPC title

• F01D25/28

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