Structural frame for an aircraft fuselage

1. frame frames of the fuselage, characterized in that it comprises a lower arch (1) and crossmember (2), the retaining element (3) of the present and the trusses (4) connecting the lower arc (1) and crossmember (2). 2. Fuselage frames frame according to claim 1, characterized in that the connecting lattice girder (4) consists of rods (4a, 4b), the ends of which are connected with the transverse beam plates (2) and the lower arc (1) .3. Fuselage frames frame according to claim 2, characterized in that the rods (4) are the crossbars, made of composite materials and having a cross section shaped U.4. Frame fuselage frames according to any one of claims 1-3, characterized in that the element includes an upper bulkhead (5) with the arms (6a, 6b, 7a, 7b), providing connection to the transverse beam (2) and the lower arch (1 ), which together with the lower arc (1) forms a frame fyuzelyazha.5. Fuselage frames frame according to claim 4, characterized in that the retaining shoulders (6a, 6b, 7a, 7c) at each edge of the upper part of the frame (5) form a forked piece, the lower arch (1) and crossmember (2) are fastened the shoulders (6a, 6b, 7a, 7b) by a fork nakladkami.6 compound. Frame fuselage frames according to any one of claims 1-3, characterized in that the lower arc (1) is a beam with ribs provided with holes (10) through which the longitudinal stringers (8) .7. Fuselage frames frame according to claim 4, characterized in that the lower arc (1) is a beam with ribs provided with holes (10) through which the longitudinal stringers (8) .8. Frame fuselage frames according to any one of claims 1-3, characterized in that the lower arc (1) is made of a metal arc, while between the ends of the rods (4a, 4b) and the lower surface of the arc (1) is placed a layer of glass (9 ).9. Fuselage frames frame according to claim 4, characterized in that the lower arc (1) is made of a metal arc, while between the ends of the rods (4a, 4b) and the lower surface of the arc (1) is placed a layer of glass (9) .10. Fuselage frames frame according to claim 6, characterized in that the lower arc (1) is made of a metal arc, while between the ends of the rods (4a, 4b) and the lower surface of the arc (1) is placed a layer of glass (9) .11. Frame fuselage frames according to any one of claims 1-3, characterized in that the lower arch (1) made of composite materialov.12. Fuselage frames frame according to claim 4, characterized in that the lower arch (1) made of composite materialov.13. Fuselage frames frame according to claim 6, characterized in that the lower arch (1) made of composite materialov.14. Fuselage frames frame according to claim 5, characterized in that the lower edge (1) and crossmember (2) are attached to the arms (6a, 6b, 7a, 7b) of each fork parts butt connection method nakladkami.15. Frame fuselage frames according to any one of claims 1-3, characterized in that it has a mixed structure consisting of parts made from metal and composite materials.