Window frame assembly for use in an aircraft and associated method of manufacture
US6318035A · kind A · utility
4Cited by
10References
8Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jun 1, 1999 |
| Grant date | Nov 20, 2001 |
| Priority date | — |
| Expiry date | Jun 1, 2019 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C1/1492
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An IR window frame assembly for use within an aircraft is manufactured at a high temperature with both the window pane and the window frame of the window frame assembly having beveled surfaces. These beveled surfaces are placed in direct contact during manufacture. As a result, the window frame assembly maintains a low radar cross section (RCS) while allowing the window assembly to be small enough to conform with aerodynamic tolerances required in an aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.