초록 ▼

The invention includes an aircraft engine mounting system for mounting an aircraft engine to an aircraft. The mounting system includes a yoke member having a first end and a second end, with an aircraft attachment between the first end and the second end, the aircraft attachment for interfacing the

The invention includes an aircraft engine mounting system for mounting an aircraft engine to an aircraft. The mounting system includes a yoke member having a first end and a second end, with an aircraft attachment between the first end and the second end, the aircraft attachment for interfacing the yoke member with the aircraft, the yoke member having a yoke member length (YL) from the first end to the second end. The mounting system preferably includes a first engine mount, the yoke member first end contained by the first engine mount, with the first engine mount having first engine mount housing grounded to the aircraft engine. The mounting system preferably includes a second engine mount, the yoke member second end contained by the second engine mount, with the second engine mount having a second engine mount housing grounded to the aircraft engine.

대표청구항 ▼

1. An aircraft engine mounting system (20) for mounting an aircraft engine (22) to an aircraft (24), said aircraft engine mounting system (20) comprising: a yoke member (26) having a first end (28) and a second end (30), with an aircraft attachment (34) between said first end (28) and said second en

1. An aircraft engine mounting system (20) for mounting an aircraft engine (22) to an aircraft (24), said aircraft engine mounting system (20) comprising: a yoke member (26) having a first end (28) and a second end (30), with an aircraft attachment (34) between said first end (28) and said second end (30), said aircraft attachment (34) for interfacing said yoke member (26) with said aircraft (24), said yoke member (26) having a yoke member length YL from said first end (28) to said second end (30);a first engine mount (36), said yoke member (26) first end (28) contained by said first engine mount (36), with said first engine mount (36) having an outer engine mount housing (38) grounded to said aircraft engine (22);a second engine mount (40), said second end (30) contained by said second engine mount (40), with said second engine mount having an outer engine mount housing (42) grounded to said aircraft engine (22);said first engine mount (36) and said second engine mount (40) grounded to said aircraft engine (22) with a mounts spacing (MS) between said first engine mount (36) and said second engine mount (40) interlocking said yoke member between said first engine mount (36) and said second engine mount (40); andwherein said yoke member (26) has an aircraft attachment width dimension (AAWD2), a first engine end width dimension (FEEWD2), and a second engine end width dimension (SEEWD2), with AAWD2>FEEWD2 and AAWD2>SEEWD2. 2. A system as claimed in claim 1 including a fastener (58), said fastener (58) inhibiting a relative sliding interface between said yoke member (26) and said first end (28). 3. A system as claimed in claim 1 including a first bushing (60) and a second bushing (62), said second bushing (62) adjacent said first bushing (60) wherein said first bushing (60) is slidable a sliding distance relative to said second bushing (62). 4. A system as claimed in claim 1 wherein said first engine mount (36) includes an alignment boss (64). 5. A method of attaching an aircraft engine (22) to an aircraft (24), said method comprising: providing a yoke member (26) having a first end (28) and a second end (30), with an aircraft attachment point (34) between said first end (28) and said second end (30), said yoke member (26) having a yoke member YL from said first end (28) to said second end (30), said yoke member (26) having an aircraft attachment width dimension (AAWD2), a first engine end width dimension (FEEWD2), and a second engine end width dimension (SEEWD2), with AAWD2>FEEWD2 and AAWD2>SEEWD2;providing a first engine mount (36);providing a second engine mount (40);providing an aircraft engine (22), said aircraft engine (22) having a first engine mounting mate (66) for mating with an alignment boss (64) carried by said first engine mount (36);said aircraft engine (22) having a second mounting mate (66) for mating with said second engine mount (40), said first engine mounting mate (66) spaced from said second engine mounting mate (66) to provide a mounting mate spacing MMS);connecting said yoke member (26) to said aircraft engine (22) with said first engine mount (36) and said second engine mount (40) wherein said first engine mounting mating (66) mates with said first engine mount (36) and said second engine mounting mating member (66) mates with said second engine mount (40), wherein said first end (28) and second end (30) of said yoke member (26) are contained by the respective first and second engine mounts, with said yoke member (26) interlocked between said first engine mount (36) and said second engine mount (40). 6. A method as claimed in claim 5, wherein connecting said yoke member (26) to said aircraft engine (22) with said first engine mount (36) and said second engine mount (40) includes, movably attaching said first engine mount (36) on said yoke member (26) first end (28). 7. A method as claimed in claim 6, including fixedly fastening said movably attached first engine mount (36) with said yoke member (26) first engine end (28) after said first mounting mating (66) is mated with said alignment boss (64) of said first engine mount (36). 8. A method as claimed in claim 5, wherein providing a first engine mount (36) includes providing a first engine mount (36) with first engine mount housing (38) for receiving and containing said yoke member (26) first end (28). 9. A method as claimed in claim 5, wherein providing a first engine mount (36) includes providing a first engine mount (36) with first engine mount housing (38) for receiving and containing said yoke member (26) first end (28) and providing a second engine mount (40) includes providing a second engine mount (40) with second engine mount housing (42) for receiving and containing said yoke member (26) second end (30). 10. A method as claimed in claim 5, wherein providing a first engine mount (36) includes providing a first engine mount (36) with a first engine mount housing (38) having an inner member (73) configured to receive the first end 28 of said yoke member (26). 11. A method as claimed in claim 5, wherein providing a first engine mount (36) includes providing a first engine mount (36) with at least one damping component (44). 12. A method as claimed in claim 5, wherein including providing a first bushing (60) and a second bushing (62), said second bushing (62) adjacent said first bushing (60) wherein said first bushing (60) is slidable a sliding distance relative to said second bushing (62).