# US 10,501,163 B2 · Pressure bulkhead for an aircraft fuselage, and an aircraft comprising such a pressure bulkhead > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,501,163 B2 - Document ID: US10501163B2 - Status: Granted - Kind: B2 - Application number: 15/158,994 - Filed: 2016-05-19 - Published: 2016-11-24 - Granted: 2019-12-10 - Earliest claimed: 2015-05-20 - Assignees: Airbus Operations GmbH - Applicants: Airbus Operations GmbH - Inventors: Paul Jörn; Markus Müller - Web page: https://patentgrep.com/patent/US10501163B2 ## CPC - B64C 1/10: Bulkheads - B64C: AEROPLANES; HELICOPTERS ## Abstract A pressure bulkhead for an aircraft fuselage including a sandwich structure defining a central axis and extending between a circumferential border area, the sandwich structure including an inner face sheet and an outer face sheet extending transverse to the central axis, and a core assembly sandwiched between the inner face sheet and the outer face sheet. The pressure bulkhead can receive pressure loads and can be used as a structural bearing element for receiving loads introduced by other structural parts. The inner face sheet and/or the outer face sheet has a corrugated shape. The distance between the outer face sheet and the inner face sheet increases and subsequently decreases from the border area to a central area about the central axis, forming a thickened area where the distance between the outer face sheet and the inner face sheet has a peak. ## Claims ### Claim 1 A pressure bulkhead for an aircraft fuselage, comprising: a sandwich structure defining a central axis and extending between a circumferential border area which is configured for being mounted to a fuselage shell; the sandwich structure comprising: an inner face sheet extending transverse to the central axis; an outer face sheet opposite the inner face sheet, extending transverse to the central axis; and a core assembly sandwiched between the inner face sheet and the outer face sheet; wherein the inner face sheet or the outer face sheet, when viewed in a radial cross section through the central axis, has a corrugated shape, wherein a distance between the outer face sheet and the inner face sheet increases and subsequently decreases from the border area to a central area about the central axis, thereby forming a thickened area where the distance between the outer face sheet and the inner face sheet has a peak. ### Claim 2 (depends on 1) The pressure bulkhead according to claim 1, wherein, when viewed in the radial cross section through the central axis, the inner face sheet has an even shape and the outer face sheet has the corrugated shape. ### Claim 3 (depends on 1) The pressure bulkhead according to claim 1, wherein, when viewed in the radial cross section through the central axis, the inner face sheet and the outer face sheet both have the corrugated shape. ### Claim 4 (depends on 1) The pressure bulkhead according to claim 1, wherein, due to the corrugated shape, the distance between the outer face sheet and the inner face sheet, after increasing and subsequently decreasing, increases again in a direction oriented from the border area towards the central area about the central axis. ### Claim 5 (depends on 1) The pressure bulkhead according to claim 1, wherein the outer face sheet and/or the inner face sheet, when viewed in the radial cross section through the central axis, has a tangent continuous developing from the border area to the central area about the central axis. ### Claim 6 (depends on 1) The pressure bulkhead according to claim 1, wherein the outer face sheet or the inner face sheet, when viewed in the radial cross section through the central axis, has a kinked shape developing from the border area to the central area about the central axis. ### Claim 7 (depends on 1) The pressure bulkhead according to claim 1, wherein the radial cross section is a first radial cross section through the central axis, and wherein a second radial cross section through the central axis is defined perpendicularly with respect to the first radial cross section. ### Claim 8 (depends on 7) The pressure bulkhead according to claim 7, wherein the inner face sheet and/or the outer face sheet, when viewed in the second radial cross section through the central axis, has a corrugated shape, wherein the distance between the outer face sheet and the inner face sheet increases and subsequently decreases from the border area to the central area about the central axis. ### Claim 9 (depends on 7) The pressure bulkhead according to claim 7, wherein the inner face sheet or the outer face sheet, when viewed in the second radial cross section through the central axis, has a convex shape, wherein the distance between the outer face sheet and the inner face sheet monotonously increases from the border area to the central area about the central axis. ### Claim 10 (depends on 1) The pressure bulkhead according to claim 1, wherein a structure element extends between the outer face sheet and the inner face sheet through the thickened area. ### Claim 11 (depends on 10) The pressure bulkhead according to claim 10, wherein the structure element comprises a connection member, which extends external to the outer and inner face sheets, and which is configured for being connected to a support element of a tail plane, an engine, a landing gear, a cargo fitting, or the fuselage shell. ### Claim 12 (depends on 1) The pressure bulkhead according to claim 1, wherein the inner face sheet and/or the outer face sheet comprise a metal material or a composite material, and wherein the core assembly comprises a honeycomb core, a folded core, a foam core, or a built core. ### Claim 13 (depends on 1) The pressure bulkhead according to claim 1, wherein a monolithic reinforcement area is provided at the border area, where the inner and outer face sheets are formed integrally and no core assembly is provided. ### Claim 14 (depends on 1) The pressure bulkhead according to claim 1, wherein a monolithic reinforcement area is provided at the central area about the central axis, where the inner and outer face sheets are formed integrally and no core assembly is provided. ### Claim 15 An aircraft comprising an aircraft fuselage and a pressure bulkhead which is installed in the aircraft fuselage, the pressure bulkhead comprising: a sandwich structure defining a central axis and extending between a circumferential border area which is configured for being mounted to a fuselage shell; the sandwich structure comprising: an inner face sheet extending transverse to the central axis; an outer face sheet opposite the inner face sheet, extending transverse to the central axis; and a core assembly sandwiched between the inner face sheet and the outer face sheet; wherein the inner face sheet or the outer face sheet, when viewed in a radial cross section through the central axis, has a corrugated shape, wherein a distance between the outer face sheet and the inner face sheet increases and subsequently decreases from the border area to a central area about the central axis, thereby forming a thickened area where the distance between the outer face sheet and the inner face sheet has a peak. ### Claim 16 (depends on 12) The pressure bulkhead according to claim 12, wherein the inner face sheet and/or the outer face sheet comprise one or more of an aluminum material, a carbon fiber reinforced plastic (CFRP) material, a glass fiber reinforced plastic (GFRP) material, or an aluminum-glass fiber-aluminum composite (GLARE®) material.