- Gainesville TX, US Aamir Jafri - Little Elm TX, US Robert W. Trimble - Gainesville TX, US
International Classification:
B64D 11/06
Abstract:
A safety belt () is secured to a seat structure () using movable anchor points (). In an embodiment, a y-belt () is attached to left and right pivotable anchor plates (). The anchor plates () pivot when a load is applied to the safety belt (), thus allowing the anchor points to self-align to maintain an equal amount of tension across the lower and higher portion of the seat belt. In a different embodiment, a 2-point safety belt () is attached to slidable anchors () that move within channels () in response to load applied to the safety belt, allowing the anchor points to self-align to maintain proper tension and positioning of the safety belt ().
- Gainesville TX, US Michael Romano - Denton TX, US Aamir Jafri - Little Elm TX, US Dianna Sabo - The Colony TX, US Rik Westerink - The Hague, NL Armando Valdes - Krum TX, US
Assignee:
ZODIAC SEATS US LLC - Gainesville TX
International Classification:
B60N 2/26 B64D 11/06 B60R 22/00
US Classification:
297257, 297464
Abstract:
The present invention generally relates to passenger aircraft seats. Some examples provide systems for integrating a child seat into a certified aircraft seat. Some examples include a passenger seat backrest having an integrated child seat. An integrated child seat base may be moved between a stowed position and a deployed position. When in the stowed position, the integrated child seat base may fit within a recessed surface of the seat backrest and the seat may then accommodate an adult passenger. When in a deployed position, the integrated child seat may then accommodate a child passenger. The integrated seat may include a harness system that extends through the seat backrest and couples with an internal support structure of seat backrest. In some embodiments the mounting points of the harness system may be reinforced with stiff brackets attached to the internal support structure.
Naval Air Warfare Center Aircraft Division (Nawcad)
Scientific and Research Engineer
Friedman Research Corporation
Director
Friedman Research Corporation Apr 2009 - Apr 2010
Fea Engineer
Zodiac Aerospace Apr 2009 - Apr 2010
Group Technical Expert, Design Validation and Simulation at Zodiac Aerospace
Trw Jan 2004 - Dec 2008
Senior Product Engineer
Education:
Wayne State University 1998 - 1999
Masters, Master of Engineering, Engineering, Mechanical Engineering
N.e.d University and Technology, Karachi 1989 - 1995
Ned University of Engineering and Technology 1990 - 1995
Bachelors, Mechanical Engineering
Ned University of Engineering and Technology
Skills:
Aerospace As9100 Aircraft Aeronautics Avionics Do 178B Lean Manufacturing Catia Continuous Improvement Nadcap Airworthiness Six Sigma Simulations Engineering Modeling Solidworks Ls Dyna Manufacturing Project Management Product Development Cad Microsoft Office Strategic Planning Autocad Microsoft Word Matlab Microsoft Excel
Zodiac Aerospace since Apr 2010
Design validation engineer
Friedman Research Corporation Apr 2009 - Apr 2010
FEA Engineer
TRW Jan 2004 - Dec 2008
Senior Product Engineer
Education:
Wayne State University 1998 - 1999
Master's degree, Mechanical Engineering
N.E.D University of Engineering and Technology 1990 - 1995
Bachelor's degree, Mechanical Engineering