Patent GB-951130-A (GB)
Title: Improvements relating to jet engines
Inventor: MAGUIRE ADDISON CHARLES
IPC: F02K1/12
Filed: 1961-07-28
Abstract: 951,130. Jet propulsion nozzles. ROLLS-ROYCE Ltd. July 20, 1962 [July 28, 1961; Feb. 12, 1962], Nos. 27553/61 and 5379/62. Heading F1J. A jet propulsion engine is provided with a convergent-diverent nozzle, the nozzle comprising first and second sets of nozzle members which respectively form the convergent and divergent parts of the nozzle, radial movement of the nozzle members varying the size of the throat of the nozzle, an assembly of casing members within which the nozzle members are mounted, radial movement of the sets of nozzle members together with radial movement in the same sense of the assembly of casing members, being effected solely by axial movement of the assembly of casing members. The downstream end of the jet pipe 15 of a gas turbine jet engine is shown in Fig. 3, the engine being mounted within a nacelle 11, the nacelle having an axially-movable portion 23 mounted thereon at its downstream end. At the downstream end of the portion 23 an annular assembly of casing members 25, 26 (see also Figs. 4, 5) is pivotally mounted. by means of pivots 24. The nacelle portion 23 is movable by means of a series of rams 45, the rods 46 of which are connected to brackets 47 secured to the portion 23. The jet pipe 15 terminates in a convergent frusto-conical portion 16, at the downstream end of which is an annular support member 17 on which are pivotally mounted on pivots 18 an annular assembly of nozzle members 20. To the downstream end of each nozzle member 20 is pivotally mounted on a pivot 21 a further nozzle member 22. Each nozzle member 20 is connected to an associated casing member 25 or 26 by means of a roller 28 on a bracket 27 secured to the casing member, the roller engaging in a cam groove 29 formed in a bracket secured to the nozzle member 20. Each nozzle member 22 is connected to an associated casing member 25 or 26 by means of a bracket 30 secured to the nozzle member, the bracket carrying rollers 31 which engage in a groove 32 in the member 25 or 26. Each of the casing members 25 is provided on its inner surface with a track 34, a pair of rollers 35 carried by a radial arm 36 being slidably mounted in each track. The arm 36 is secured to an axiallyextending rod 37 which is pivotally mounted at 38 to a bracket 39 secured to the jet pipe 15. Each of the casing members 26 is provided internally with a plate member 40 formed with a cam groove 41 at each side thereof, each groove receiving a roller 42 mounted on an arm 43 connected to the rod 37, see Fig. 5. When it is desired to decrease the size of the throat of the convergent-divergent nozzle, the nacelle portion 23 is cuased to be moved to the left, whereupon the casing members 25, 26 are caused to be swung radially inwardly about the pivots 24 because of the engagement of the rollers 42 in the cam grooves 41. The inward movement of the casing members is transmitted to the nozzle members 20 and 22 by means of the links 27 and 30, the nozzle members moving to the positions indicated by broken lines. In a second embodiment, Fig. 7, nozzle members 58 are pivotally mounted at the downstream end of the jet pipe and further nozzle members 59 are pivotally mounted at the downstream end of a frusto-conical member 57 which is secured to a cylindrical casing 55 which may be moved axially with respect to the jet pipe. The nozzle members 58 carry rollers 62 which engage the frusto-conical member 57 whereby upon axial movement of the casing 55 and member 57 to the left from the position shown in Fig. 7, the nozzle members 58 are swung inwardly about their pivot points. Casing members 63 are pivotally connected at their upstream ends to the casing 55 and are connected to the nozzle members 58 by means of links 64 so that as the nozzle members 58 swing radially inwardly, the casing members 63 are also sung inwardly. The nozzle members 59 are connected to the casing members 63 by a link arrangement 66, 67, 68 so that as the casing members 63 are moved inwardly, so the nozzle members 59 are also moved inwardly.