Air intake for commercial aircraft jet engine nacelle

B - Operations – Transporting – 64 – D

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64D 33/02 (2006.01) F02C 7/04 (2006.01) F02C 7/045 (2006.01)

Patent

CA 2398653

The air inlet is of scarf type and the internal profile ¬5S( )| of the upper sections ¬S( )| of its lip 1 comprises, with respect to the identical and symmetrical horizontal sections (Sb) of the said lip, an internal bulge (10) which is all the bigger the larger the scarf angle and which is a maximum at the upper vertical section ¬S(0)|.

- L'entrée d'air est de type scarf et le profil interne [5S(.theta.)] des sections supérieures [S(.theta.)] de sa lèvre 1 comporte, par rapport aux sections horizontales, identiques et symétriques, (Sb) de ladite lèvre, un renflement interne (10) qui est d'autant plus important que l'angle de scarf est plus grand et qui est maximal à la section verticale supérieure [S(0)].

LandOfFree

Say what you really think

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

Rating

Air intake for commercial aircraft jet engine nacelle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Air intake for commercial aircraft jet engine nacelle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Air intake for commercial aircraft jet engine nacelle will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1429072

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