초록

Some but not all engines of an aircraft are provided with thrust reversers. A safety device disables, at least from the position corresponding to idling, the action of the throttles corresponding to the engines devoid of thrust reversers when the thrust reversers are controlled to deployment.

대표청구항 ▼

The invention claimed is: 1. An aircraft provided with a plurality of engines whose speeds are controlled individually, between idling and full speed, by throttles respectively associated with said engines, wherein: certain of said engines of said plurality are equipped with thrust reversers that a

The invention claimed is: 1. An aircraft provided with a plurality of engines whose speeds are controlled individually, between idling and full speed, by throttles respectively associated with said engines, wherein: certain of said engines of said plurality are equipped with thrust reversers that are operable to be controlled so as to be able to go from an inactive retracted position to an active deployed position and, conversely, from said active deployed position to said inactive retracted position; other engines of said plurality are devoid of thrust reversers, and a safety device is provided so as to disable, at least from the position corresponding to idling, the action of the throttles corresponding to said engines devoid of thrust reversers, when said thrust reversers are controlled so as to go from their inactive retracted position to their active deployed position. 2. The aircraft as claimed in claim 1, wherein said engines comprise four engines carried by the wings of said aircraft and pairwise symmetric with respect to the fuselage of the latter, so that each wing carries an inboard engine and an outboard engine wherein said inboard engines are provided with thrust reversers whereas said outboard engines are devoid thereof. 3. The aircraft as claimed in claim 1, wherein said safety device comprises a detector of the control of said thrust reversers to deployment and latching components controlled by said detector and latching, when idling, said engines devoid of thrust reversers, these latter engines having previously been brought to idling through an intentional action. 4. The aircraft as claimed in claim 3, wherein said latching components lock, in the position corresponding to idling, the throttles of said engines devoid of thrust reversers, the latter throttles having previously been brought to said position corresponding to idling through an intentional action. 5. The aircraft as claimed in claim 1, wherein said safety device comprises a detector of the control of said thrust reversers to deployment and idling units imposing idling on said engines devoid of thrust reversers, irrespective of the speed of the latter engines. 6. The aircraft as claimed in claim 5, wherein said idling units imposing idling on said engines devoid of thrust reversers act on the fuel supply rate to the latter engines. 7. The aircraft as claimed in claim 1, wherein said safety device disables the action of said throttles, corresponding to said engines devoid of thrust reversers as soon as at least one of the thrust reversers is controlled to deployment. 8. The aircraft as claimed in claim 1, wherein said safety device is sensitive to a cue indicating that said aircraft is in contact with the ground and does not disable the action of said throttles corresponding to said engines devoid of thrust reversers unless said aircraft is on the ground. 9. The aircraft as claimed in claim 1, wherein said safety device is sensitive to a cue representative of a velocity threshold with respect to the ground of said aircraft and does not disable the action of said throttles corresponding to said engines devoid of thrust reversers unless the velocity with respect to the ground of said aircraft is greater than said threshold. 10. The aircraft as claimed in claim 1, wherein said safety device is sensitive to cues representative of the respective positions of said throttles and does not disable the action of said throttles corresponding to said engines devoid of thrust reversers unless said throttles are in a position corresponding to idling, except possibly one or more of the throttles corresponding to said engines devoid of thrust reversers. 11. The aircraft as claimed in claim 10, which comprises an alarm device activated by said safety device when at least one of the throttles corresponding to one of said engines devoid of thrust reversers is not in the position corresponding to idling. 12. The aircraft as claimed in claim 1, wherein said safety device maintains idling on said engines devoid of thrust reversers for a predetermined duration after the end of control to deployment of the thrust reversers and the return of the latter from the active deployment position to the inactive retracted position.