Turbojet Engine Nacelle with Lateral Opening of Covers
First Claim
1. A nacelle of a turbojet designed to be attached to a structure of an aircraft by a connecting pylon and comprising at least one movable portion capable of being opened so as to allow access to the inside of the nacelle, characterized in that said movable portion is mounted so as to pivot about a pivot shaft oriented along a shaft that is substantially perpendicular to the plane of the structure of the aircraft to which the nacelle is attached.
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Accused Products
Abstract
The present invention relates to a nacelle (1) of a turbojet engine (4), which nacelle is intended to be attached to a structure (2) of an aeroplane by a connecting pylori (3) and comprises at least one moving part (9′, 9′) above to be opened in order to provide access to the interior of the nacelle, characterized in that the said moving part is mounted to pivot about a pivot axis (25) directed along a line more or less perpendicular to the plane of the structure of the aeroplane to which the nacelle is attached.
20 Citations
12 Claims
- 1. A nacelle of a turbojet designed to be attached to a structure of an aircraft by a connecting pylon and comprising at least one movable portion capable of being opened so as to allow access to the inside of the nacelle, characterized in that said movable portion is mounted so as to pivot about a pivot shaft oriented along a shaft that is substantially perpendicular to the plane of the structure of the aircraft to which the nacelle is attached.
Specification