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    • 1. 发明专利
    • Improvements in means for suppression of noise in turbo-jet engines
    • GB878191A
    • 1961-09-27
    • GB2646258
    • 1958-08-18
    • VICKERS AIRCRAFT HOLDINGS LTDELFYN JOHN RICHARDS
    • HAY JOHN ANTHONYRICHARDS ELFYN JOHN
    • F02K1/36
    • 878,191. Jet-propulsion nozzles. VICKERS AIRCRAFT HOLDINGS Ltd., and RICHARDS, E. J. Oct. 14, 1959 [Aug. 18, 1958], No. 26462/58. Class 110 (3). In a gas-turbine jet-propulsion engine, the jet nozzle outlet has a large width to depth ratio, and the nozzle is combined with an air-induction casing arranged to surround the nozzle and of such a length as to cause ambient air to be drawn in and entrained with the gas discharge. The propulsion nozzle 10 is of circular section at its upstream end 101 and of rectangular section at its outlet 102. The nozzle is enclosed within a nacelle 11, the upper and lower walls of which terminate at 111, while the side walls thereof terminate level with the nozzle outlet 102. The air induction casing associated with the nozzle is shown in its retracted or inoperative position in Fig. 1 in full lines and in its projected or effective position in chain-dotted lines, and comprises upper and lower fairing members 15 and side plates 14 connected together to form an open-ended casing which is disposed around the nozzle 10. The upper and lower members 15 are of aerofoil or tapered cross-section and when in the projected position afford, together with upper and lower edges of the nozzle 10, openings C through which air is drawn to be entrained with the discharging gases thereby producing a noise suppression effect. The side plates 14 of the induction casing are disposed in the spaces between the side walls 112 of the nacelle and the side walls of the nozzle and are supported by means of rollers 13 which are movable in channel-section members 12 secured one to each of the side walls 112. A cable 17 is secured to the rollers 13 and threaded around pulleys 16, the movable element 181 of a fluid-pressure pressure ram 18 being connected to the cable, so that movement of the ram in the direction B causes the induction casing to be moved from the retracted to the projected position. The jet nozzle may be of elliptical instead of rectangular section; also a series of nozzles may be disposed side-by-side, a single induction casing being associated with the nozzles.
    • 2. 发明专利
    • Improvements in or relating to helicopter rotor propulsion means
    • GB774396A
    • 1957-05-08
    • GB1178954
    • 1954-04-23
    • ELFYN JOHN RICHARDS
    • B64C27/18B64D39/00
    • 774,396. Jet propelled helicopter rotors. RICHARDS, E. J. April 1, 1955 [April 23, 1954], No. 11789/54. Class 4. [Also in Groups XXVI and XXVII] A helicopter rotor blade is provided at or adjacent the trailing edge of the tip portion of the blade with an elongated narrow nozzle of fixed configuration in the form of a generally linear slot or other closed figure and means for emitting a propulsive jet from that nozzle. A rotor blade is formed with a spanwise duct 10 formed with chord wise branches 11 which terminate in nozzles 12 collectively arranged to emit a long narrow propulsive jet generated by the combustion of air from the duct 10 and fuel supplied to pipes 14 which inter-connect the nozzles. The nozzle outlets may be deflected downwardly to provide a lift component and the outlet edges of the nozzles may be corrugated to reduce noise. It is stated in the Provisional Specification that rods placed across the outlet of the nozzle assist in reducing noise. In other embodiments the nozzles have the form of circular or elliptical annular outlets from combustion chambers mounted at the tips of the rotor blades.
    • 9. 发明专利
    • Improvements in mufflers for the exhaust of jet engines
    • GB890106A
    • 1962-02-28
    • GB2458659
    • 1959-07-17
    • HALL ENGINEERING LTDELFYN JOHN RICHARDS
    • B64F1/26
    • 890,106. Exhaust silencers. HALL ENGINEERING Ltd., and RICHARDS, E. J. Aug. 29, 1960 [July 17, 1959], No. 24586/59. Class 7(2). A silencer for the exhaust of jet engines comprises a curved rectangular section diverging expansion duct c, Fig. 1, in which the jet is expanded and turned upwards. The tube c at its entry end has an approximately square cross-section which becomes wider and of smaller depth so that at the cross-section 11- 11 it is a wide slot which discharges through a perforated member d into a diffusion outlet c. The inlet end of duct c is provided with an adapter a carried by pivoted, counterweighted arms f so that it can be adjusted to the height of the jet engine. The adapter a is provided with a baffle b Fig. 8 through which air is drawn to enter the jet stream, the parts a, b, being covered with sound absorbing material. Water jets may also be sprayed on to the stream in the conduit c which is pivotally supported on a platform p by a pillar n and struts q. In a modification, Fig. 15, the tube c is carried on a wheeled platform p, which can be raised off its wheels by jacks t, and the height and inclination of the conduit can be varied by adjustable struts x, y.