Counterrotating aircraft propulsor blades

Details Counterrotating aircraft propulsor blades Counterrotating aircraft propulsor blades

B - Operations, Transporting

64

C

244/120

B64C 11/20 (2006.01) B64C 11/18 (2006.01) B64C 11/48 (2006.01)

Patent

CA 1319357

13DV 8687 COUNTERROTATING AIRCRAFT PROPULSOR BLADES ABSTRACT OF THE DISCLOSURE A propulsor blade for an aircraft engine includes an airfoil section formed in the shape of a scimitar. A metallic blade spar is interposed between opposed surfaces of the blade and is bonded to the surfaces to establish structural integrity of the blade. The metallic blade spar includes a root end allowing attachment of the blade to the engine.

556028

Affiliated with

Also associated with

Rating

Counterrotating aircraft propulsor blades does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Counterrotating aircraft propulsor blades, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Counterrotating aircraft propulsor blades will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1302038