Installing or removing aircraft engines

Patent metadata

Field	Value
Publication number	US-2016376015-A1
Application number	US-201514747521-A
Country	US
Kind code	A1
Filing date	Jun 23, 2015
Priority date	Jun 23, 2015
Publication date	Dec 29, 2016
Grant date	—

Abstract

A nacelle may include a thrust reverser. The inner fixed structure may include an IFS support and movable portions which hinge open at hinges between the IFS support and the movable portions. The IFS support may be coupled to the engine core. Standard ground support equipment may be coupled to attachment features on the IFS support to attach or remove an engine from an aircraft wing with the IFS attached to the engine.

First claim

I claim:

1 . A method of installing an aircraft engine comprising:
coupling a first cable to a forward hoist and a forward attachment feature on an IFS support, wherein the IFS support is coupled to an engine core; coupling a second cable to an aft hoist and an aft attachment feature on the IFS support; raising the aircraft engine to a pylon using the first cable and the second cable; and coupling an engine mount to a pylon mount.

2 . The method of claim 1 , wherein the IFS support and at least one movable portion form an inner fixed structure.

3 . The method of claim 2 , wherein the inner fixed structure remains coupled to the aircraft engine during the raising.

4 . The method of claim 2 , further comprising hinging a translating sleeve closed to form a bypass duct between the translating sleeve and the inner fixed structure.

5 . The method of claim 1 , further comprising removing the forward hoist and the aft hoist from the pylon.

6 . The method of claim 4 , wherein the aircraft engine comprises a bifurcation panel which is formed separately from a movable portion of the inner fixed structure.

7 . The method of claim 1 , wherein the engine mount is coupled to the IFS support.

8 . The method of claim 2 , wherein the inner fixed structure forms a fire barrier around the engine core.

9 . A method of assembling an aircraft propulsion engine comprising:
attaching an inner fixed structure (“IFS”) support to an engine core; mounting a first movable portion to the IFS support, wherein the first movable portion is movable relative to the IFS support, the first movable portion and the IFS support together helping to define a fire-sealed space around the engine core; mounting ground support lifting equipment to at least one attachment feature on the IFS support; and and lifting the engine into position for attachment to an engine mount on an aircraft.

10 . The method of claim 9 , wherein the IFS support and the first movable portion form an inner fixed structure.

11 . The method of claim 10 , wherein the inner fixed structure remains coupled to the engine during the lifting.

12 . The method of claim 10 , further comprising hinging a translating sleeve open to access the IFS support.

13 . The method of claim 9 , further comprising coupling a forward hoist and an aft hoist to a pylon, wherein a plurality of cables couple the forward hoist and the aft hoist to the at least one attachment feature.

14 . The method of claim 12 , wherein the engine comprises a composite bifurcation panel and a metallic inner fixed structure.

15 . The method of claim 9 , further comprising closing a translating sleeve around the IFS support and the first movable portion.

Assignees

• Rohr Inc

Inventors

• Lacko Anthony J

Classifications

• B64F5/50

  Handling or transporting aircraft components · CPC title

• B64D29/06

  Attaching of nacelles, fairings or cowlings · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B64D27/402

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• B64D27/18 Primary

  within, or attached to, wings · CPC title