# US 2019/0170088 A1 · System for actuating a panel of a turbojet engine nacelle > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2019/0170088 A1 - Document ID: US20190170088A1 - Status: Published application - Kind: A1 - Application number: 16/257,765 - Filed: 2019-01-25 - Published: 2019-06-06 - Earliest claimed: 2016-07-25 - Assignees: Safran Nacelles - Applicants: Safran Nacelles - Inventors: Patrick GONIDEC; Loïc CHAPELAIN; Faycel BOUABDALLAH - Web page: https://patentgrep.com/patent/US20190170088A1 ## CPC - F02K 1/763: {with actuating systems or actuating devices; Arrangement of actuators for thrust reversers} - B64D 29/06: Attaching of nacelles, fairings or cowlings - F02K 1/06: Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) - F02K 1/11: by means of pivoted eyelids - F02K 1/12: by means of pivoted flaps - F02K 1/1207: {of one series of flaps hinged at their upstream ends on a fixed structure (F02K1/1215 - F02K1/1292 take precedence)} - F02K 1/70: using thrust reverser flaps or doors mounted on the fan housing - F05D 2250/42: with two degrees of freedom - F05D 2260/57: using servos, independent actuators, etc. - F05D 2270/62: Electrical actuators - F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00) - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A pod for a turbojet engine includes an outer cowl having a structure with at least one opening and a panel pivotably mounted about an axis between a closed position and an open position, and a system for actuating the panel designed to lock the panel in closed position and to move same between the closed position and the open position thereof. The actuation system includes a lateral connecting rod connected to the panel and to the structure, pivoting relative to the structure about a first pivoting axis and about a second pivoting axis, and a linear actuator attached to the lateral connecting rod. The actuator system is designed to move the lateral connecting rod during the extension of the actuator, and the lateral connecting rod exerts a force on the panel during the movement thereof, pivoting the panel about the axis thereof. ## Claims ### Claim 1 A nacelle for an aircraft turbojet engine, the nacelle comprising: an outer cowling comprising: a structure comprising at least one aperture; and at least one panel pivotally mounted about an axis between a closed position that obstructs said at least one aperture and an open position in which part of a secondary air flow, flowing through an annular channel defined between said outer cowling and an inner fixed structure of the nacelle defining a fairing of the turbojet engine passes through the at least one aperture; and an actuation system that locks the panel in said closed position and displaces said at least one panel between said closed position and said open position, the actuation system comprising: at least one lateral tie rod connected on one side to the at least one panel and connected to the structure of the outer cowling on another side, said at least one lateral tie rod being pivotally mounted relative to the structure on one side about a first pivot axis substantially parallel to a longitudinal axis of the nacelle and about a second pivot axis substantially perpendicular to the first pivot axis on another side; and a linear actuator attached to said at least one lateral tie rod, the linear actuator extendable between a retracted position and an extended position, wherein the actuation system displaces the at least one lateral tie rod during extension of said linear actuator, causing the at least one lateral tie rod to pivot about said first and second pivot axes, and so that the at least one lateral tie rod, bearing on the structure, exerts, during its displacement, a force on the panel, causing a pivoting of said panel about its axis. ### Claim 2 (depends on 1) The nacelle according to claim 1, wherein the linear actuator is attached to the at least one lateral tie rod by a movement transmission device comprising: a yoke attached to the at least one panel and pivotally mounted about a vertical axis, a movable rod of the linear actuator being attached to said yoke; and a spider mounted to a second end of the lateral tie rod via a ball joint connection. ### Claim 3 (depends on 2) The nacelle according to claim 2, wherein the actuator and the movement transmission device are located in an inner space of the at least one panel. ### Claim 4 (depends on 1) The nacelle according to claim 1, wherein the at least one panel is further mounted free in translation along an axis parallel to a longitudinal axis of the nacelle, wherein the actuation system drives the at least one panel from a downstream position to an upstream position of the nacelle when the at least one panel passes from the closed position to the open position. ### Claim 5 (depends on 4) The nacelle according to claim 4, wherein at least one side wall of the at least one panel includes an oblong hole having a roller secured to the structure of the outer cowling such that the at least one panel is movable in translation along the axis parallel to the longitudinal axis of the nacelle, wherein the actuation system comprises a longitudinal tie rod having a first end connected to said structure and a second end connected to a yoke of a movement transmission device. ### Claim 6 (depends on 4) The nacelle according to claim 4, wherein at least one side wall of the at least one panel includes a rail receiving a ball joint or a slider secured to the structure of the outer cowling such that the at least one panel is movable in translation along the axis substantially parallel to the longitudinal axis of the nacelle, wherein the actuation system comprises a longitudinal tie rod having a first end connected to said structure and a second end connected to a yoke of a movement transmission device. ### Claim 7 (depends on 1) The nacelle according to claim 1, wherein a first end of the at least one lateral tie rod is connected to the structure of the outer cowling via a yoke pivotally mounted about the first pivot axis. ### Claim 8 (depends on 7) The nacelle according to claim 7, wherein the at least one lateral tie rod is further pivotally mounted relative to the yoke about the second pivot axis. ### Claim 9 (depends on 1) The nacelle according to claim 1, wherein the at least one panel includes an opening profiled on at least one side wall of the at least one panel, and the at least one lateral tie rod passes through said opening. ### Claim 10 (depends on 1) The nacelle according to claim 1, wherein the actuator is attached to an upstream wall of the at least one panel. ### Claim 11 (depends on 1) The nacelle according to claim 1, wherein the at least one panel includes two actuation systems that are symmetrical relative to an axis of symmetry of the at least one panel, each actuation system comprising a hydraulic, electrical, or aeraulic actuation motor. ### Claim 12 (depends on 1) The nacelle according to claim 1, wherein the at least one panel is further translated in a direction parallel to a longitudinal axis of the nacelle, and the actuation system alternately drives the at least one panel between a downstream position to an upstream position of the nacelle when the at least one panel passes from the closed position to the open position. ### Claim 13 (depends on 1) The nacelle according to claim 1, wherein the at least one panel is a panel of a secondary air flow ejection nozzle. ### Claim 14 (depends on 1) The nacelle according to claim 1, wherein the outer cowling forms a sliding cowl of a thrust reverser device.