Aircraft with an engine support structure
An aircraft with an engine support structure, the aircraft including at least an engine wherein the at least engine is top mounted to an aircraft, a main body, and an engine support structure including a plurality of hoop structures, wherein at least one horseshoe structure is located forward of the center of gravity to the at least engine.
1. An aircraft with an engine support structure, the aircraft comprising:
at least an engine wherein the at least engine is top mounted to an aircraft;
a main body; and
an engine support structure comprising a plurality of hoop structures, wherein each hoop structure of the plurality of hoop structures comprises:
a horseshoe structure, wherein the horseshoe structure is configured to provide a vertical engine mount, wherein the horseshoe structure comprises a first half and a second half connected by a beam, and wherein the engine support structure is suspended from the beam.
2. The aircraft of claim 1 , wherein the horseshoe structure comprises a plurality of horseshoe structures.
3. The aircraft of claim 2 , wherein at least one horseshoe structure of the plurality of horseshoe structures is located forward of a center of gravity of an engine assembly of the at least an engine.
4. The aircraft of claim 1 , wherein the engine support structure is mounted to the top of the main body.
5. The aircraft of claim 1 , wherein the engine support structure comprises two horseshoe structures, wherein each of the two horseshoe structures are located forward of a center of gravity of an engine assembly of the at least an engine.
6. The aircraft of claim 5 , wherein the engine support structure comprises a third horseshoe structure, wherein the third horseshoe structure is located aft of the center of gravity of an engine assembly the at least an engine.
7. The aircraft of claim 5 , wherein the configuration of the two horseshoe structures permits a thrust reversal mechanism.
8. The aircraft of claim 1 , wherein the aircraft comprises a blended wing body.
9. The aircraft of claim 1 , wherein the at least an engine comprises a turbofan.
10. The aircraft of claim 1 , further comprising a first engine support structure and a second engine support structure.
11. The aircraft of claim 10 , further comprising a first engine and a second engine.
12. The aircraft of claim 11 , wherein the first engine support structure is attached to the first engine and the second engine support structure is attached to the second engine.
13. The aircraft of claim 1 , wherein the plurality of hoop structures mount the at least engine to a plurality of ribs of the aircraft by attachment of one side of the engine support structure to a first rib of the aircraft and a second side to a second rib of the aircraft.
14. The aircraft of claim 13 , wherein the at least an engine is located aft of a rear spar of the main body.
15. The aircraft of claim 13 , further comprising a main gear, wherein the main gear is located aft of a rear spar of the main body.
16. The aircraft of claim 1 , wherein the main body comprises a single deck.
17. The aircraft of claim 16 , further comprising a main gear, wherein the main gear is located within a gear housing when the main gear is retracted.
18. The aircraft of claim 17 , wherein the gear housing is located in a position that intersects with a plane coincident with the single deck.
19. The aircraft of claim 16 , further comprising a front gear, wherein the front gear is located forward of the single deck.
20. The aircraft of claim 13 , wherein the main body further comprises a rear spar, wherein the first rib and the second rib are attached to the rear spar.