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https://drivepatents.com/patents/1399971 · 15 Apr 2026
A hook body (330) for a latch mechanism includes a plurality of longitudinal members (331, 333), each of the plurality of longitudinal members extending in a longitudinal direction with respect to the hook body (330); and a load slot (340) at a proximal en...
https://drivepatents.com/patents/1388140 · 11 Feb 2026
An aircraft engine cowling (102) comprises a first cowling portion (104) and a second cowling portion (106) moveable relative to each other. A cowling latch (114) secures the first cowling portion (104) and the second cowling portion (106) in a closed posi...
https://drivepatents.com/patents/1390597 · 31 Dec 2025
An engine nacelle inlet is provided. The inlet comprises an inner barrel having a leading edge and a trailing edge. A segmented attach flange is connected to an outer circumference of the trailing edge of the inner barrel, wherein the segmented attach flan...
https://drivepatents.com/patents/1394770 · 29 Oct 2025
An assembly for an aircraft propulsion system (10) includes an upstream cowl (66) and a downstream cowl (68). The upstream cowl (66) extends axially from a first upstream end (70) to a first downstream end (72). The upstream cowl (66) includes an inner bar...
https://drivepatents.com/patents/992589 · 27 Feb 2013
A turbine engine comprising an engine core bounded by a bypass duct, a first portion of the bypass duct defined by a fan casing having a radially inner wall and a radially outer wall, a second portion of the bypass duct defined by a radially inner wall and...
https://drivepatents.com/patents/1002810 · 2 May 2012
The aircraft nacelle (10) has limiting element (19) with at least one lock that is integral with the rest of nacelle or respectively the cowl (14). One part of lock occupies locked state in which lock interferes with the cowl and prevents deformation that ...
https://drivepatents.com/patents/1005835 · 25 Jan 2012
The nacelle has a variable section nozzle cowl (1) including a movable cowl part (3) with a thrust reverser arranged so that translational movement of the part allows the passage of the part from a stow position (5) of the reverser to a thrust reversal pos...
https://drivepatents.com/patents/1006687 · 28 Dec 2011
A guide system for translating components of an aircraft engine nacelle includes a track assembly and a slider assembly. The track assembly includes a track guide member (108) having a track channel (110). The slider assembly translatably engages the track...
https://drivepatents.com/patents/1007694 · 23 Nov 2011
A guide system for translating components of an aircraft engine nacelle includes a track assembly (106) and a slider assembly (150). The track assembly includes a track guide member (108) and a track liner (112) engaged therewith. The track guide member in...