Rocket motor extendible nozzle exit cone
US4872612A · kind A · utility
Assignee
Inventor
Key dates
| Filing date | Jul 23, 1987 |
| Grant date | Oct 10, 1989 |
| Priority date | — |
| Expiry date | Jul 23, 2007 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64G1/403
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A membrane of refractory material having opposed arcuate edges one of which is longer than the other, having opposed straight edges which when welded together in edge-to-edge relationship form the frustum of cone, is deformed by brake or die press means over a portion adjacent the longer arcuate edge to provide thereon a pattern comprising two sets of creases in each of five equal sectors, a first set of which creases points at the viewer from the exterior of the membrane (as it subsequently is formed into the frustum of a cone) and a second set which points away from the viewer. The creases of the first set run both circumferentially and longitudinally with respect to the surface of the cone while the creases of the second set run longitudinally only. This crease pattern enables a membrane portion forward of the larger diameter of the cone to be folded inwardly in multiple layers and permits an amount of membrane material sufficient to produce a very large area ratio at the exit plane to be stowed in a much reduced envelope, with the cone in folded form being quite rigid. In other embodiments the membrane is formed into an integral seamless free standing shape by spinning a sheet …
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.