초록 ▼

A thrust reverser for a jet engine of a mobile platform. The thrust reverser includes a hinge beam defining a first track and a latch beam defining a second track. The thrust reverser also includes at least one cascade support ring having an upper end portion and a lower end portion. A first fitting

A thrust reverser for a jet engine of a mobile platform. The thrust reverser includes a hinge beam defining a first track and a latch beam defining a second track. The thrust reverser also includes at least one cascade support ring having an upper end portion and a lower end portion. A first fitting is disposed at the upper end portion of the cascade support ring. The first fitting includes an engagement portion slidably positioned within the first track. A second fitting is disposed at the lower end portion of the cascade support ring. The second fitting includes an engagement portion slidably positioned within the second track.

대표청구항 ▼

1. A thrust reverser for a jet engine of a mobile platform, the thrust reverser comprising:at least one cascade support ring; at least one track defined by one of the cascade support ring and another portion of the thrust reverser; and at least one engagement portion defined by the other one of said

1. A thrust reverser for a jet engine of a mobile platform, the thrust reverser comprising:at least one cascade support ring; at least one track defined by one of the cascade support ring and another portion of the thrust reverser; and at least one engagement portion defined by the other one of said cascade support ring and said another portion of the thrust reverser, the engagement portion being sized to be disposed within the track to couple the cascade support ring to the thrust reverser. 2. The thrust reverser of claim 1, wherein the engagement portion is sized to be slidably received within the track.3. The thrust reverser of claim 1, wherein the track comprises a substantially c-shaped cross section, and wherein the engagement portion comprises a substantially circular cross section.4. The thrust reverser of claim 1, wherein the engagement portion is integral to the cascade support ring.5. The thrust reverser of claim 1, wherein the engagement portion is attached to the cascade support ring.6. The thrust reverser of claim 1, wherein the track is integral to the thrust reverser.7. The thrust reverser of claim 1, wherein the track is attached to the thrust reverser.8. The thrust reverser of claim 1, wherein the at least one track comprises a first track and a second track, and wherein the at least one engagement portion comprises a first engagement portion sized to be disposed within the first track, and a second engagement portion sized to be disposed within the second track.9. The thrust reverser of claim 1, wherein:the thrust reverser includes a hinge beam defining the first track, and a latch beam defining the second track; and the cascade support ring includes an upper end portion defining the first engagement portion, and a lower end portion defining the second engagement portion. 10. The thrust reverser of claim 1, further comprising a wear-resistant material lining an inner surface of the track.11. The thrust reverser of claim 1, further comprising a wear-resistant material lining an outer surface of the engagement portion.12. A mobile platform, comprising:a jet engine for generating thrust; a thrust reverser for reversing direction of the thrust; at least one cascade support ring; at least one track defined by one of the thrust reverser and the cascade support ring; and at least one engagement portion defined by the other one of said thrust reverser and said cascade support ring, the engagement portion being disposed within the track to couple the cascade support ring to the thrust reverser. 13. The mobile platform of claim 12, wherein the engagement portion is sized to be slidably received within the track.14. The mobile platform of claim 12, wherein the mobile platform comprises an aircraft.15. The mobile platform of claim 12, wherein:the thrust reverser includes a hinge beam defining a first track, and a latch beam defining the second track; and the cascade support ring includes an upper end portion defining a first engagement portion sized disposed within the first track, and a lower end portion defining a second engagement portion disposed within the second track. 16. Apparatus for mounting a cascade support ring to a thrust reverser of a jet engine, the apparatus comprising:at least one track defined by one of the thrust reverser and the cascade support ring; and at least one engagement portion defined by the other one of said thrust reverser and said cascade support ring, the engagement portion being sized to be disposed within the track. 17. The apparatus of claim 16, wherein the engagement portion is sized to be slidably received within the track.18. The apparatus of claim 16, wherein the track comprises a substantially c-shaped cross section, and wherein the engagement portion comprises a substantially circular cross section.19. The apparatus of claim 16, wherein the engagement portion is integral to the cascade support ring.20. The apparatus of claim 16, wherein the engagement portion is attached to the cascade support ring.21. The apparatus of claim 16, wherein the track is integral to the thrust reverser.22. The apparatus of claim 16, wherein the track is attached to the thrust reverser.23. The apparatus of claim 16, further comprising a wear-resistant material lining an inner surface of the track.24. The apparatus of claim 16, further comprising a wear-resistant material lining an outer surface of the engagement portion.25. Apparatus for mounting a cascade support ring to a thrust reverser of a jet engine, the apparatus comprising:at least one engagement portion defined by one of said thrust reverser and said cascade support ring; and means for receiving the engagement portion therein to couple the cascade support ring to the thrust reverser wherein said means is defined by the other one of said thrust reverser and said cascade support ring. 26. A method of mounting a cascade support ring to a thrust reverser for a jet engine of a mobile platform, the method comprising positioning at least one engagement portion defined by one of said thrust reverser and said cascade support ring within at least one track defined by the other one of said thrust reverser and said cascade support ring.27. The method of claim 26, wherein the positioning includes slidably positioning the engagement portion within the track.28. The method of claim 26, further comprising mounting a fitting defining the engagement portion to the cascade support ring.29. The method of claim 26, wherein the positioning includes:slidably positioning a first engagement portion defined by one of said thrust reverser and said cascade support ring within a first track defined by the other one of said thrust reverser and said cascade support ring; and slidably positioning a second engagement portion defined by one of said thrust reverser and said cascade support ring within a second track defined by the other one of said thrust reverser and said cascade support ring. 30. The method of claim 29, wherein:the first track is defined by a hinge beam of the thrust reverser; the second track is defined by a latch beam of the thrust reverser; the first engagement portion is defined by an upper end portion of the cascade support ring; and the second engagement portion is defined by a lower end portion of the cascade support ring.