초록 ▼

A rotorcraft (1) having a feed unit for feeding fuel to a power plant (13) of the rotorcraft (1). A middle floor (12b) is securely engaged with at least two frames (9a, 9b) of the fuselage, and being load-bearing relative to general forces supported by the fuselage. A bottom compartment (7) of the r

A rotorcraft (1) having a feed unit for feeding fuel to a power plant (13) of the rotorcraft (1). A middle floor (12b) is securely engaged with at least two frames (9a, 9b) of the fuselage, and being load-bearing relative to general forces supported by the fuselage. A bottom compartment (7) of the rotorcraft (1) does not have the load-bearing covering (8) of the fuselage, the bottom face of the fuselage being open to the outside providing the bottom compartment (7) with a bottom (17) open to the outside of the rotorcraft. The bottom face of the middle floor (12b) forms an anchor member for suspending at least one fuel tank (25, 26) that is accessible from outside the fuselage via said open bottom (17).

대표청구항 ▼

1. A rotorcraft having a fuel feed unit for a power plant of the rotorcraft, the power plant including at least one fuel-burning engine, the rotorcraft including a fuselage extending longitudinally between the front and the rear of the rotorcraft and made up of members stiffening a covering and comp

1. A rotorcraft having a fuel feed unit for a power plant of the rotorcraft, the power plant including at least one fuel-burning engine, the rotorcraft including a fuselage extending longitudinally between the front and the rear of the rotorcraft and made up of members stiffening a covering and comprising at least: a longitudinal succession of transverse frames locally defining a transverse profile of the fuselage, together with longitudinal stiffeners for stiffening the covering; anda top floor securely engaged with at least two of the frames, referred to as middle frames, forming part of a middle segment of the fuselage located between a cockpit and a tail boom, the top floor carrying at least one main rotor of substantially vertical axis for providing the rotorcraft at least with lift;the fuel feed unit including at least one assembly for feeding the engine of the power plant with fuel, the at least one fuel feed assembly comprising at least:a fuel tank installed inside at least one bottom compartment of the fuselage situated under a middle floor separating the bottom compartment from at least one top compartment forming cabin space of the rotorcraft; anda feeder immersed in the tank, said feeder having at least one supply circuit for supplying the feeder with fuel from the tank and having a feed circuit for feeding the at least one engine with fuel from the feeder to the at least one engine associated with the fuel feed assembly;wherein the middle floor is a load-bearing floor securely engaged with at least the two middle frames, the bottom compartment being free of the covering over a bottom face of the fuselage, which is open to the outside, thereby providing the bottom compartment with an open bottom that is open to the outside of the fuselage, the tank being suspended from the bottom face of the middle floor that forms a suspension anchor member for the tank, the tank being accessible from outside the fuselage via the open bottom, wherein the bottom compartment is fitted with stabilizer means for stabilizing the suspended support of the tank by the middle floor, the stabilizer means being formed by transverse plates formed at the bases of at least one pair of the frames and engaged in slots formed in the top wall of the tank. 2. The rotorcraft according to claim 1, wherein the bottom compartment is defined between the middle floor and a side skirt arranged in a substructure of the fuselage to extend the covering, the open bottom being defined between the free bottom edges of the skirt. 3. The rotorcraft according to claim 1, wherein the slots are formed in the top wall of the tank providing vertical partitioning of the tank to separate its inside volume of the tank into a plurality of longitudinally successive chambers, passages for passing fuel between two adjacent chambers of a given tank being provided at the bottom of the tank at the bases of the partitioning. 4. The rotorcraft according to claim 3, wherein the feeder is placed in a longitudinally middle chamber of the tank arranged between two adjacent frames. 5. The rotorcraft according to claim 1, wherein the fuel feed unit comprises a plurality of the fuel feed assemblies, and the respective tanks of the fuel feed assemblies are in fluid flow communication with one another via a fuel transfer circuit extending transversely between the tanks and provided between two adjacent frames. 6. The rotorcraft according to claim 4, wherein the fuel feed unit comprises a plurality of the fuel feed assemblies, and the respective tanks of the fuel feed assemblies are in fluid flow communication with one another via a fuel transfer circuit extending transversely between the tanks and provided between two adjacent frames, and wherein the fuel transfer circuit is arranged between the respective feeders of the fuel feed assembly. 7. The rotorcraft according to claim 1, wherein the tank includes a bottom wall incorporating slopes for draining fuel by gravity towards an opening of the supply circuit through which the fuel is taken for delivery to the feeder. 8. The rotorcraft according to claim 7, wherein the slopes are arranged by incorporating blocks of cellular material in the tank, which blocks impart a locally sloping shape to the bottom wall. 9. The rotorcraft according to claim 1, wherein the bottom wall of the fuselage in the zone of the bottom compartment is formed at least in part by a bottom wall of the tank closing the open bottom. 10. The rotorcraft according to claim 1, wherein the bottom wall of the fuselage in the zone of the bottom compartment is formed at least in part by a removable wall for shutting the open bottom. 11. The rotorcraft according to claim 1, wherein the middle floor constitutes a shield for protecting the top compartment against intrusion of the tank. 12. The rotorcraft according to claim 1, wherein means for anchoring the tank in suspension are formed by attachment members secured to the middle floor and co-operating with straps fitted to the tanks. 13. The rotorcraft according to claim 12, wherein the anchor means are rupturable breaking the co-operation between the anchor members and the straps, thereby allowing the tank to be jettisoned in the event of the rotorcraft crashing. 14. A rotorcraft having a fuel feed unit for a power plant of the rotorcraft, the power plant including a fuel-burning engine, the rotorcraft including a fuselage extending longitudinally between the front and the rear of the rotorcraft and comprising a covering and members for stiffening the covering, the rotorcraft comprising: a longitudinal succession of transverse frames locally defining a transverse profile of the fuselage, together with longitudinal stiffeners for stiffening the covering; andan upper floor securely engaged with at least two of the frames, forming at least part of a middle segment of the fuselage located between a cockpit and a tail boom, the upper floor carrying at least one main rotor for providing the rotorcraft at least with lift;the fuel feed unit including a fuel feed assembly for feeding the engine with fuel,the fuel feed assembly comprising:a fuel tank suspended by at least one load-bearing attachment member inside a lower compartment of the fuselage situated under a middle floor separating the lower compartment from an upper compartment forming cabin space of the rotorcraft therebetween; anda feeder immersed in the tank, the feeder having at least one supply circuit for supplying the feeder with fuel from the tank and having a feed circuit for feeding the engine with fuel from the feeder;wherein the lower compartment is fitted with at least one non-load-bearing plates for stabilizing the suspended support of the tank by the middle floor and serving as a reinforcing element to stiffen the tank and prevent deformation in shape;wherein the middle floor is a load-bearing floor securely engaged with the at least two of the frames, the lower compartment being free of the covering over a lower face of the fuselage, which is open to an exterior of the fuselage, thereby providing the lower compartment with an open bottom that associates the exterior with an interior of the fuselage, the tank being suspended interiorly from a lower face of the middle floor that forms a suspension anchor member for the tank, the tank being located within the lower compartment and accessible from the exterior of the fuselage via the open bottom. 15. The rotorcraft of claim 14, wherein the middle floor further comprises load-bearing panels carried by load-bearing cross-members securely engaged with the transverse frames, the panels being embedded in channels formed at least in the cross members. 16. A rotorcraft having a fuel feed unit for a power plant of the rotorcraft, the power plant including a fuel-burning engine, the rotorcraft including a fuselage extending longitudinally between the front and the rear of the rotorcraft and having a covering, the rotorcraft comprising: a longitudinal succession of transverse frames locally defining a transverse profile of the fuselage, together with longitudinal stiffeners for stiffening the covering; andan upper floor securely engaged with at least two middle frames of the succession of transverse frames to form at least part of a middle segment of the fuselage located between a cockpit and a tail boom, the upper floor carrying at least one main substantially vertical rotor;the fuel feed unit including a fuel feed assembly for feeding the engine with fuel, the fuel feed assembly comprising:a fuel tank suspended by at least one attachment member inside at least one lower compartment of the fuselage situated under a middle floor separating the at least one lower compartment from at least one upper compartment forming cabin space of the rotorcraft therebetween; anda feeder disposed in the tank, the feeder having at least one supply circuit for supplying the feeder with fuel from the tank and having a feed circuit for feeding the engine with fuel from the feeder;a plurality of plates cooperating with the transverse frames and an upper wall of the tank to inhibit relative movement of the fuselage and the tank;wherein the middle floor is a load-bearing floor securely engaged with the at least two middle frames, the lower compartment being free of the covering over a lower face of the fuselage, which is open to the outside, thereby providing the lower compartment with an open bottom that is open to the outside of the fuselage, the tank being suspended from the lower face of the middle floor that forms a suspension anchor member for the tank, the tank being accessible from outside the fuselage via the open bottom. 17. The rotorcraft of claim 16, wherein the plurality of plates comprises transverse plates extending from the transverse frames and engaged in slots, the slots formed by folds in the upper wall of the tank. 18. The rotorcraft of claim 17, wherein the transverse plates extend to the bases of the transverse frames and provide vertical partitioning to separate the inside volume of the tank into a plurality of longitudinally successive chambers, with fuel allowed to pass between adjacent chambers of the tank through orifices or ducts in the plates. 19. The rotorcraft according to claim 14, wherein the lower compartment is defined between the middle floor and a side skirt arranged in a substructure of the fuselage to extend the covering, the open bottom being defined between the free bottom edges of the skirt. 20. The rotorcraft according to claim 16, wherein the lower compartment is defined between the middle floor and a side skirt arranged in a substructure of the fuselage to extend the covering, the open bottom being defined between the free bottom edges of the skirt.