Title:
LOW-NOISE AIRCRAFT, PARTICULARLY AT TAKE-OFF AND LANDING
Document Type and Number:
WIPO Patent Application WO2006108957
Kind Code:
A3
Abstract:
The invention concerns an aircraft comprising: a rear vertical tail unit consisting of at least two tail fins (5, 6) forming, with the rear part (7) of said fuselage (4), a channel (8) arranged on the back thereof; and at least one turbine engine (9, 10) arranged on the back of said fuselage (4) so that the gas streams generated by said turbine engine (9, 10) penetrate into said channel (8); and moreover, the main landing gear of said aircraft is arranged integrally beneath the fuselage (in 11); said wings (2, 3) have a slight sweep angle(f); and said wings have a large fineness ratio.
Inventors:
CROS CHRISTOPHE (FR)
Application Number:
PCT/FR2006/000794
Publication Date:
December 14, 2006
Filing Date:
April 11, 2006
Export Citation:
Assignee:
AIRBUS FRANCE (FR)
CROS CHRISTOPHE (FR)
CROS CHRISTOPHE (FR)
International Classes:
B64D27/20
Foreign References:
| EP0273466A2 | 1988-07-06 | |||
| EP1041000A2 | 2000-10-04 | |||
| US4674712A | 1987-06-23 | |||
| US3936017A | 1976-02-03 |
Other References:
STEINKE S: "AUS DER TRICKKISTE DER FLUGZEUGENTWICKLER AIRBUS-KONZEPTE FUER UEBERMORGEN", FLUG REVUE, STUTTGART, DE, vol. 1/2001, January 2001 (2001-01-01), pages 22 - 25, XP009053625
Download PDF:
Previous Patent: SELF-CONTAINED DEVICE FOR BIOLOGICAL TREATMENT OF EFFLUENTS
Next Patent: APPARATUS FOR HANDLING LOADS SUCH AS LUGGAGE ITEMS
Next Patent: APPARATUS FOR HANDLING LOADS SUCH AS LUGGAGE ITEMS