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Cargo compartment door for an aircraft

  • US 5,335,880 A
  • Filed: 10/16/1992
  • Issued: 08/09/1994
  • Est. Priority Date: 10/18/1991
  • Status: Expired due to Term
First Claim
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1. A combination comprising a medium sized aircraft fuselage and a cargo compartment door structure for said aircraft fuselage, a floor connected to said fuselage at lateral connecting areas, said floor dividing said fuselage into a passenger cabin above said floor and into a cargo compartment below said floor, said fuselage having a vertical central plane passing longitudinally through said fuselage perpendicularly to said floor, a curved door opening in said fuselage, said curved door opening extending through an angular range beginning at one of said connecting areas and reaching circumferentially and downwardly at least beyond said vertical central plane to form an opening sector having a center where said vertical central plane and said floor intersect to form an opening angle of more than 90°

  • , a curved door for covering said curved door opening in a sealed manner, a first hinge securing said curved door to said fuselage, and a conveyor belt (5A) in said cargo compartment, said conveyor belt extending toward said door opening for loading baggage onto said conveyor belt through said curved door opening, wherein said curved door comprises at least two foldable door sections, and a second hinge foldably interconnecting said door sections, and wherein a lower door section of said at least two foldable door sections (17) forms an inwardly facing surface constructed as a stepping platform (20) extending substantially horizontally when said door is open, and a brace for holding said lower door section in a fixed substantially horizontal position when said door is open, so that said inwardly facing surface of said lower door section can be used as a stepping platform when said door is open.

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