SUSPENSION DEVICE OF GAS-TURBINE ENGINE, AND GAS-TURBINE ENGINE CONTAINING SUCH SUSPENSION DEVICE Russian patent published in 2013 - IPC F02C7/20 

FIELD: engines and pumps.

SUBSTANCE: suspension device of gas-turbine engine on load-carrying structure of airborne vehicle includes a beam. The latter includes the first element, such as upper platform, in which there can be arranged attachment devices to the above load-carrying structure, and the second element, in which there can be arranged attachment devices to gas-turbine engine. Also, beam includes one set of the first plates and at least one set of the second plates, which are intended to be arranged in transverse direction in relation to engine axis. Plates are connected to each other by means of adhesiveness of elastomeric material layers. The first plates are rigidly connected to the first element, and the above second plates are rigidly connected to the second element. Attachment device to gas-turbine engine includes at least one lever hinged by means of a tie to ball hinge on the second element of the beam. The other subject of the present invention is gas-turbine engine containing the above suspension device.

EFFECT: invention allows reducing the size of suspension device of gas-turbine engine.

6 cl, 5 dwg