Aircraft tail cone

B - Operations – Transporting – 64 – C

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64C 1/00 (2006.01) B64C 1/26 (2006.01) B64D 11/00 (2006.01) B64D 11/04 (2006.01)

Patent

CA 2657218

The subject of the invention is a special layout of the tail cone (4) of the fuselage (1) of an aeroplane. This aeroplane has a fuselage (1) with a nose cone, a main section and a tail cone (4) bearing a vertical stabilizer (14) and an empennage (15). The fuselage (1) is divided into two superimposed regions by a floor (10) forming a main deck, these being respectively a pressurized and air-conditioned upper region (11) in which a passenger cabin (2) is formed, and a pressurized lower region (12) that forms a cargo hold (3). The pressurized upper region (11) is extended into the tail cone (4) by a pressurized space (40) which extends as far as a leaktight and strong transverse bulkhead (41) positioned in the rear part of that portion (13) of the fuselage that is covered by the vertical stabilizer (14), said pressurized space (40) constituting an area accessible to individuals and extending over the majority of that portion (13) of the fuselage that is covered by the vertical stabilizer (14).

L'invention a pour objet une disposition particulière du cône arrière (4) du fuselage (1) d'un avion. Cet avion a un fuselage (1 ) avec une pointe avant, une partie principale et un cône arrière (4) portant une dérive (14) et un empennage (15). Le fuselage (1) est séparé en deux zones superposées par un plancher (10) formant pont principal, respectivement une zone supérieure (11) pressurisée et climatisée dans laquelle est ménagée une cabine de passagers (2), et une zone inférieure (12) pressurisée formant une soute (3). La zone supérieure (11) pressurisée est prolongée dans le cône arrière (4) par un espace pressurisé (40) qui s'étend jusqu'à une paroi transversale (41) étanche et résistante, placée dans la partie arrière de la portion (13) du fuselage couverte par la dérive (14), ledit espace pressurisé (40) constituant un local accessible aux personnes, et s'étendant sur la plus grande partie de la portion (13) du fuselage couverte par la dérive (14).

LandOfFree

Say what you really think

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

Rating

Aircraft tail cone does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFCA-PAI-O-1636036

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