Mechanically fastened large pressurized vehicle structure
A first part, a second part, and a seal ring are fastened together to form a pressure structure configured for a spacecraft structure of a spacecraft, wherein the first part and the second part are each formed from a single workpiece.
1. A method comprising:
joining a first part and a second part to form an enclosed volume for a vehicle structure by pressing a first flange extending beyond a first rim of the first part and a second flange extending beyond a second rim of the second part together with a seal ring and a number of sealing elements sandwiched between the first flange and the second flange by a plurality of fasteners passing through a plurality of through holes in the seal ring, and a plurality of openings in the first flange and in the second flange;
passing each of a number of the fasteners through a first number of the through holes in the first flange and through a second number of openings in the second flange;
tightening the plurality of fasteners to form a seal between the first part and the second part;
affixing first members in first channels in an outside surface of the first part and affixing second members in second channels in the outside surface of the first part;
ngaging a tunnel to one of the first part and the second part;
affixing a hatch outer assembly to the tunnel; and
affixing a hatch inner assembly to the tunnel.
2. The method of claim 1 , wherein the seal is configured to hold a pressure in a volume outside an atmosphere of a planet.
3. The method of claim 1 further comprising:
prior to joining, indentifying a configuration for a plurality of parts to form the vehicle structure, the plurality of parts including at least the first part and the second part.
4. The method of claim 3 further comprising:
after identifying, manufacturing the plurality of parts.
5. The method of claim 1 further comprising:
forming a first workpiece into the first part by spinning the first workpiece about an axis while a roller presses the first workpiece into a first shape; and
forming a second workpiece into the second part by spinning the second workpiece about the axis while the roller presses the second workpiece into a second shape.
6. The method of claim 5 further comprising:
manufacturing the seal ring and the number of sealing elements.
7. The method of claim 5 further comprising:
machining the first shape to the first flange and machining the second shape to form the second flange by removing a first amount of a material from the first shape and the second shape.
8. The method of claim 5 further comprising:
machining the first shape to form first features and the first channels on the outside surface of the first part; and
machining the second shape to form second features and the second channels on the outside surface.
9. The method of claim 1 further comprising:
machining the first flange, the seal ring, and the second flange for joining by the plurality of fasteners to form the enclosed volume.
10. The method of claim 8 , wherein the plurality of parts further comprise a plurality of features, which include at least the first features and the second features.
11. The method of claim 10 , wherein the plurality of features comprise a plurality of patterns and a plurality of channels which include the first channels and the second channels.
12. The method of claim 11 , wherein the plurality of patterns comprise a plurality of inner walls, a plurality of blind holes, and a plurality of nodes.
13. The method of claim 12 , wherein the plurality of inner walls intersect at a plurality of nodes.
14. The method of claim 11 , wherein the plurality of channels comprise a plurality of outer walls that form a plurality of boundaries between the plurality of patterns and the plurality of channels.
15. The method of claim 14 wherein the plurality of outer walls comprise a second plurality of openings configured to receive fasteners to affix an additional structure to the outside surface.