The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 23, 2010

Filed:

Apr. 19, 2005
Applicants:

Alain Fournier, Le Plessis Robinson, FR;

Bernard Laboure, Velizy, FR;

Robert Standish, Saint-Cloud, FR;

Inventors:

Alain Fournier, Le Plessis Robinson, FR;

Bernard Laboure, Velizy, FR;

Robert Standish, Saint-Cloud, FR;

Assignee:

Aircelle, Harfleur, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turboprop engine includes a power jet mounted coaxially to the engine axis (X-X'), and has a fan case and a gas ejecting system provided with two afterbody half-cowlings () each of which is pivotable around an axis (A) between open and closed positions, wherein the half-cowlings are connected to the downstream of the fan case through a 'V-blade/V-groove' system. In a first embodiment, the pivot axes (A) make an angle α>3° to the engine axis (X, X′) and a joint plane (Z-Z) between the afterbody half-cowlings and the downstream of the fan case makes to the plane (Y, Y′) perpendicular to the engine axis (X, X′) an angle β in such a way that the difference between the angle α and the angle β is less than or equal to 3°. In the other embodiment, the axes are converged to each other in a downstream direction.


Find Patent Forward Citations

Loading…