Turbojet having a large bypass ratio

Power plants – Reaction motor – Interrelated reaction motors

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C239S265390, C060S770000

Reexamination Certificate

active

07430852

ABSTRACT:
A turbojet comprises at least a fan, a compressor, a combustion chamber, a turbine, and a rigid substantially-cylindrical jacket fastened at its upstream end to an intermediate casing and at its downstream end to an exhaust casing, the jacket serving to transmit forces between the intermediate casing and the exhaust casing.

REFERENCES:
patent: 4471609 (1984-09-01), McLaren
patent: 4683717 (1987-08-01), Naud
patent: 4785625 (1988-11-01), Steel et al.
patent: 5056307 (1991-10-01), Liang
patent: 5275357 (1994-01-01), Seelen et al.
patent: 5592813 (1997-01-01), Webb
patent: 5791138 (1998-08-01), Lillibridge et al.
patent: 5943856 (1999-08-01), Lillibridge et al.
patent: 6223524 (2001-05-01), Durcan
patent: 6666018 (2003-12-01), Butler et al.
patent: 6990797 (2006-01-01), Venkataramani et al.
patent: 7047725 (2006-05-01), Moe et al.
patent: 7100869 (2006-09-01), Picard et al.
patent: 7140174 (2006-11-01), Johnson
patent: 7188467 (2007-03-01), Johnson
patent: 7216475 (2007-05-01), Johnson
patent: 7246481 (2007-07-01), Gutmark et al.
patent: 2005/0081509 (2005-04-01), Johnson
patent: 2007/0144141 (2007-06-01), Roberge et al.
patent: 2007/0186535 (2007-08-01), Powell et al.
patent: 2625261 (1989-06-01), None

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Turbojet having a large bypass ratio does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbojet having a large bypass ratio, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbojet having a large bypass ratio will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4019410

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.