That propulsion system used recip P&W engines. It should be obvious that different propulsion systems require different mounting structures and methods.Yes, but a C97 didn't have such thing.
It is not a purposely weakened bolt. Any bolt, solid or hollowed out, has a load limit. Fuse pins or bolts are designed to break (shear) at predetermined loads.I just find it very strange that a purposely weakened bolt would be used to transmit incredible amounts of thrust to the airframe and also carry the G loads for huge engines that weigh around 7 tons or more. Purposely weakened bolts that could form stress cracks and then fuse when they should not be fusing.
See post #7 https://bobistheoilguy.com/forums/threads/molakule-q-a-on-aircraft-structures-iii.395792/
"The Pylon, also called an engine mount, is a structure positioned between the engine and the wing or fuselage.
It is designed to not only carry the dead weight of the engine, but also torque and engine thrust, both forward and reverse.
The pylon attaches to the engine "case" via two or more attachment points. The pylon attaches to the wing or fuselage via two or more attachment points as well.
The pylon not only has to resist various loads, but also acts as a conduit for systems such as hydraulics, electrical, and engine bleed. Below are diagrams for a pylon, the first being a general description and the second being a more detailed diagram.
Items called Fuse pins and hollow "Fuse" bolts are also incorporated into the pylon structure.
The second part of this question is: What is the purpose of Fuse pins and hollow "Fuse" bolts?
Last edited: May 20, 2025"
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