# US 12,214,858 B2 · Removable cover for hatch > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,214,858 B2 - Document ID: US12214858B2 - Status: Granted - Kind: B2 - Application number: 18/172,531 - Filed: 2023-02-22 - Published: 2024-08-22 - Granted: 2025-02-04 - Earliest claimed: 2023-02-22 - Assignees: Gulfstream Aerospace Corporation - Applicants: Gulfstream Aerospace Corporation - Inventors: Patrick Leonard; Caleb Wright; Caroline Culjak; Matthew Sandusky; Omar Khan - Web page: https://patentgrep.com/patent/US12214858B2 ## CPC - B64C 1/14: Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens {accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers}(fairings movable in conjunction with undercarriage elements B64C25/16; bomb doors B64D1/06) - B64F 5/10: Manufacturing or assembling aircraft, e.g. jigs therefor - B64F 5/60: Testing or inspecting aircraft components or systems - E02D 29/14: Covers for manholes or the like; Frames for covers {(gully gratings E03F5/06)} - E05C 3/004: {about an axis perpendicular to the surface on which the fastener is mounted} - E05C 3/02: without latching action - B64C: AEROPLANES; HELICOPTERS - B64F: GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR - E02D: FOUNDATIONS; EXCAVATIONS; EMBANKMENTS (specially adapted for hydraulic engineering E02B); UNDERGROUND OR UNDERWATER STRUCTURES {(tunnels, tunnelling, mining E21)} - E05C: BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS (latching means for sideboard or tailgate structures for vehicles B62D, {B62D33/02}; fastening devices for constructional or engineering elements E04, F16B; locks, fastening devices structurally or operatively combined or having significant cooperation with locks E05B; means for operating or controlling wing fasteners in conjunction with mechanisms for moving the wing E05F) ## Abstract Removable covers and methods for covering emergency exit hatches are provided. An exemplary method includes removing the emergency exit enclosure from a hatch in a wall; pushing a removable cover from an interior of the wall into the hatch; and securing the removable cover in the hatch from the interior of the wall. ## Claims ### Claim 1 A method for removing an emergency exit enclosure, the method comprising: removing the emergency exit enclosure from a hatch in a wall; providing a removable cover having a body and a peripheral flange extending outward from the body; pushing the removable cover from an interior of the wall into the hatch by passing the peripheral flange through the hatch to an exterior of the wall; and securing the removable cover in the hatch from the interior of the wall by applying a compressive force to the wall with the peripheral flange, wherein: the wall is a fuselage wall that encloses a cabin of an aircraft; the emergency exit enclosure comprises a window and/or a door; the removable cover comprises an external portion and an internal portion; the external portion and internal portion are integral; the external portion includes a planar exterior surface extending from opposite annular edges forming the peripheral flange, the annular edges extending from the exterior surface at the peripheral flange to an abutment surface contacting the wall; and the internal portion includes an annular sidewall extending from the abutment surface to an internal surface. ### Claim 2 (depends on 1) The method of claim 1, wherein pushing the removable cover from the interior of the wall into the hatch comprises pushing an interior surface of the removable cover toward the exterior of the wall. ### Claim 3 (depends on 1) The method of claim 1, wherein adjustable tabs are located on an inner side of the wall, and wherein securing the removable cover in the hatch comprises engaging the adjustable tabs with the removable cover. ### Claim 4 (depends on 1) The method of claim 1, wherein: retractable tabs are located on an inner side of the wall; the body of the removable cover has an interior surface and a periphery; the interior surface of the body of the removable cover is formed with lugs located at the periphery; pushing the removable cover from the interior of the wall into the hatch comprises retracting the retractable tabs; and securing the removable cover in the hatch comprises engaging each retractable tab with a respective lug. ### Claim 5 (depends on 1) The method of claim 1, wherein: the removable cover has a tightening member; and securing the removable cover in the hatch comprises adjusting the tightening member to draw the peripheral flange toward the wall. ### Claim 6 (depends on 1) The method of claim 1, wherein: the body of the removable cover has a periphery, an exterior surface, and an interior surface; the removable cover includes tabs; and securing the removable cover in the hatch comprises extending the tabs beyond the periphery of the body and compressing the wall between the peripheral flange and the tabs. ### Claim 7 (depends on 1) The method of claim 1, wherein: the body of the removable cover has a periphery, an exterior surface, and an interior surface; the removable cover includes tabs and adjustment mechanisms; and securing the removable cover in the hatch comprises extending the tabs beyond the periphery of the body and adjusting the adjustment mechanisms to compress the wall between the peripheral flange and the tabs. ### Claim 8 (depends on 1) The method of claim 1, wherein: the body of the removable cover has a periphery, an exterior surface, and an interior surface; the removable cover comprises a handle on the interior surface of the removable cover; and pushing the removable cover from the interior of the wall into the hatch comprises grasping the handle. ### Claim 9 (depends on 1) The method of claim 1, wherein securing the removable cover in the hatch comprises pulling the removable cover toward the wall so that the peripheral flange abuts the wall. ### Claim 10 (depends on 1) The method of claim 1, wherein a handle is formed on the internal surface, and wherein securing the removable cover in the hatch from the interior of the wall by applying the compressive force to the wall with the peripheral flange comprises pulling on the handle. ### Claim 11 (depends on 10) The method of claim 10, wherein rotatable projections are mounted to the internal surface adjacent to the annular sidewall, and wherein the method further comprises: before pushing the removable cover from an interior of the wall into the hatch, positioning the rotatable projections toward the inner portion such that the rotatable projections do not extend outward from the annular sidewall; and while securing the removable cover in the hatch, rotating the rotatable projections to extend outward from the annular sidewall to engage the fuselage wall between the rotatable projections and the peripheral flange. ### Claim 12 (depends on 11) The method of claim 11, wherein each rotating projection is connected to the internal portion by an adjustment mechanism, wherein each rotatable tab is configured to rotate about a respective axis, and wherein each adjustment mechanism is configured to selectively apply a force to a respective rotatable tab in a direction of the respective axis. ### Claim 13 (depends on 12) The method of claim 12, further comprising tightening the rotatable projections to compress the fuselage wall between the abutment surface and the rotatable projections. ### Claim 14 (depends on 13) The method of claim 13, further comprising limiting application of a maximum force applied to the fuselage wall while tightening the rotatable projections to prevent damage to the fuselage wall.