초록 ▼

An apparatus operable to seal an opening in an aircraft fuel tank during a pressure test of the fuel tank is described. The apparatus includes a substantially dome shaped body having a perimeter. The body further includes a rim extending in an orthogonal direction about the perimeter and a flange ex

An apparatus operable to seal an opening in an aircraft fuel tank during a pressure test of the fuel tank is described. The apparatus includes a substantially dome shaped body having a perimeter. The body further includes a rim extending in an orthogonal direction about the perimeter and a flange extending in a normal direction from the rim and about the perimeter. The flange is sized to engage the fuel tank about the opening. The apparatus further includes a sealing gasket proximate an intersection of the rim and the flange, extending completely around the perimeter. The seal is oriented to provide a sealing function between the fuel tank and the body as pressure is increased within the fuel tank.

대표청구항 ▼

1. An apparatus operable to seal an opening in an aircraft fuel tank during a pressure test of the fuel tank, said apparatus comprising: a substantially dome shaped body comprising a perimeter, said body further comprising a rim extending in an orthogonal direction about the perimeter and a flange e

1. An apparatus operable to seal an opening in an aircraft fuel tank during a pressure test of the fuel tank, said apparatus comprising: a substantially dome shaped body comprising a perimeter, said body further comprising a rim extending in an orthogonal direction about the perimeter and a flange extending in a normal direction from said rim and about the perimeter, said body removably coupled to the fuel tank to provide selective access to an interior of the fuel tank;a sealing gasket proximate an intersection of said rim and said flange, extending completely around the perimeter, said sealing gasket oriented to provide a sealing function between the fuel tank and said body as pressure is increased within the fuel tank; andan indicator coupled to said rim and extending about said perimeter of said dome shaped body, said indicator separate from said sealing gasket and comprising at least one band oriented to provide a direct indication of a range of pressurization force within the fuel tank. 2. The apparatus according to claim 1 wherein said sealing gasket comprises a compression lip seal. 3. The apparatus according to claim 1, wherein said indicator comprises a plurality of indicators, each said indicator indicative of a respective pressure range within the fuel tank. 4. The apparatus according to claim 1 wherein said dome shaped body, said rim and said flange are integrally formed from composite materials. 5. The apparatus according to claim 1 wherein said dome shaped body, said rim and said flange are integrally formed from fiber-based composite materials. 6. The apparatus according to claim 1 wherein said dome shaped body comprises an elliptical shape. 7. The apparatus according to claim 1 further comprising a handle integrally formed or separately mounted proximate a center of said dome shaped body, said handle operable for external insertion and removal of said apparatus from the opening. 8. The apparatus according to claim 1 further comprising indexed surfaces defined across at least one of said dome shaped body, said rim and said flange to guide alignment of said apparatus with a fuel tank port and associated seal contact surfaces of the opening. 9. A door for sealing an opening in a vessel for pressure testing of the vessel, said door comprising: a body comprising a dome shaped profile, said body removably coupled to the vessel to provide selective access to an interior of the vessel;a contour lip extending about a perimeter of said body, said contour lip having a perimeter operable for engaging an opening of the vessel;a compression seal disposed on said contour lip and operable for compression sealing the opening; andan indicator coupled to said contour lip, said indicator separate from a compression seal and comprising at least one band oriented to provide a direct indication of a range of pressurization force within the vessel. 10. The door according to claim 9, wherein said at least one band comprises multiple color bands, visibility of a specific color band indicative of a respective degree of pressurization within the vessel and a respective degree of compression of said compression seal. 11. The door according to claim 9 wherein said indicator comprises an adhesive band extending about said contour lip. 12. The door according to claim 9 wherein at least one of said body and said contour lip comprises indexed surfaces to guide self alignment of said door within the opening of the vessel. 13. The door according to claim 9 wherein said body and said contour lip are integrally formed from composite materials. 14. The door according to claim 9 wherein said body and said contour lip are integrally formed from fiber-based composite materials. 15. The door according to claim 9 further comprising a handle integrally formed or separately mounted proximate a center of said body, said handle operable for external insertion and removal of said door from the opening. 16. A door for sealing an aircraft fuel tank for purposes of pressure testing of the fuel tank, the aircraft fuel tank including an opening to access an interior of the fuel tank, said door comprising: a body comprising a dome shaped profile and an outer sidewall, said body removably coupled to the fuel tank to provide selective access to an interior of the fuel tank;a lip extending from said outer sidewall, said lip defining a surface operable for engaging the fuel tank about the opening;a seal disposed on said lip, said seal operable for providing a compression sealing between the fuel tank and said door; andan indicator coupled to said outer sidewall, said indicator separate from said seal and comprising at least one band oriented to provide a direct indication of a range of pressurization force within the fuel tank.