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US 9,849,995 B2Granted
Aircraft nacelle comprising a spacing system which is intended to maintain the two cowls spaced apart
AssigneeAirbus Operations GmbH
InventorsFlorent Bonneau, Julien Lezerac
Life of this patent
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Abstract
An aircraft nacelle with a system to provide spacing between two halves of a cowl. The cowls open and close by rotating about an axis in the upper regions of the cowls, and the cowls have indexing features in a region of the lower edges. The indexers are in sliding contact the spacing system, which is rigidly mounted to the nacelle. The spacing system comprises a housing for receiving the indexers and two levers with features for prescribing the movement of the cowls. The spacing system further comprises an actuator and a plurality returns to assist the movement of the cowls.
Claims3
A nacelle comprising:
- two cowls arranged symmetrically about an opening axis, each cowl comprising:
- an upper region and a lower region, and
- an indexer disposed in the lower region,
- wherein the opening axis is disposed in the upper region of each cowl, and the cowls are configured to be rotatable about the opening axis such that the lower regions contact with each other in a closed position and are spaced apart from each other in an open position, and
- a spacing system comprising:
- a base which is attached to the nacelle,
- a lever for each cowl, wherein each lever is rotatable about the base between an engagement position, in which the indexer is in the housing or against a stop, and a disengagement position, in which the lever is retracted in order to allow the movement of the indexer,
- a housing in which the indexers are received when the corresponding cowl is in the closed position,
- the stop disposed on each lever and against which each indexer is positioned when the corresponding cowl is in the open position,
- a return for each lever and which is configured to urge each lever into the engagement position,
- an actuator which is common to the two levers and whose actuation allows movement of each lever from the engagement position to the disengagement position,
- wherein the levers can be positioned independently from one another, and
- wherein each lever has an extension on which the indexer slides when the indexer is beyond the stop in relation to the housing.
10 more elements
An aircraft comprising:
- a strut, and
- a nacelle fixed under the strut, wherein the nacelle comprises:
- two cowls arranged symmetrically about an opening axis, each cowl comprising:
- an upper region and a lower region, and
- an indexer disposed in the lower region,
- wherein the opening axis is disposed in the upper region of each cowl, and the cowls are configured to be rotatable about the opening axis such that the lower regions contact with each other in a closed position and are spaced apart from each other in an open position, and
- a spacing system comprising:
- a base which is attached to the nacelle,
- a lever for each cowl, wherein each lever is rotatable about the base between an engagement position, in which the indexer is in the housing or against a stop, and a disengagement position, in which the lever is retracted in order to allow the movement of the indexer,
- a housing in which the indexers are received when the corresponding cowl is in the closed position,
- the stop disposed on each lever and against which each indexer is positioned when the corresponding cowl is in the open position,
- a return for each lever which is configured to urge each lever into the engagement position,
- an actuator which is common to the two levers and whose actuation allows movement of each lever from the engagement position to the disengagement position,
- wherein the levers can be positioned independently from one another, and wherein each lever has an extension on which the indexer slides when the indexer is beyond the stop in relation to the housing.
11 more elements
Dependencies are inferred from the claim text.