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ARCHIVE > Patents > Patent 688,838

PATENT SPECIFICATION 688,838
Inventors: CHARLES MANDEVILLE WILMOT and JOSEPH NAIME MANSOUR.

 
Date of filing Complete Specification: Feb. 23, 1951. No. 4860/50.
Application Date: Feb. 24, 1950.
Complete Specification Published: March 18, 1953.


COMPLETE SPECIFICATION

Improvements relating to Reaction Motors.

      We, WILMOT MANSOUR & COMPANY LIMITED, a British Company, of Salisbury Road, Totton, Hampshire, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement;—
 
Seal - UK Patent Office
      Various experiments have been made in recent years with model aircraft driven by reaction motors in which the forward thrust is produced by the reaction of the rearward discharge of gases of combustion. The advantages of using such a motor in a model aircraft, vehicle or vessel are obvious, the principal ones being the absence of any torque reaction in flight and the elimination of the need for winding any rubber-band motor. The present invention relates to small reaction motors of the rocket type suitable for use in a model aircraft or vehicle or for other purposes.
      In such a small motor the gases may be generated by igniting a composition inserted in pellet form into a casing, the ignition being effected by producing a temperature of about 200°C. by means either of a fuze or a hot point. In constructing such a motor lightness of weight is essential and in consequence the strength of the parts is necessarily comparatively low. In particular the casing in which the gas-generating charge is placed and in which it burns must be made as thin-walled as possible. To produce the necessary forward thrust the combustion gases must pass rearwardly through one or more small jet orifices. There is a risk of these becoming clogged and in such a case the gases will be unable to escape and a high pressure will rapidly be developed. This may well lead to bursting of the casing.
 
The advantages […] are obvious, the principal ones being the absence of any torque reaction in flight and the elimination of the need for winding any rubber-band motor.
      According to this invention a safety device controlling one or more openings separate from the jet orifice or orifices is provided to allow any abnormal pressure to be relieved from a casing in which a gas-generating charge is burnt and from which the gases escape through one or more jet orifices. The safety device consists either of a springloaded valve, or of a frangible disc or the like, e.g. a wad blown wholly out of the opening to relieve the abnormal pressure. As a rule there is only one jet orifice and it may advantageously, be made in a plug screw-threaded into an opening in the rear end wall of the casing.
      The opening to receive the orifice member may be eccentric to the axis of a cylindrical casing and another eccentric opening may then be provided in the same end wall and be closed by a spring-loaded valve or a thin disc which will withstand the normal working pressure but break if any abnormal and dangerous pressure is produced.
 
According to this invention a safety device […] is provided to allow any abnormal pressure to be relieved from a casing in which a gas-generating charge is burnt
      The invention will be more clearly understood by reference to the accompanying drawings in which:
      Figure 1 is a longitudinal section through one motor according to the invention on the line X-X in Figure 2;
      Figure 2 is an end view of the motor shown in Figure 1; and
      Figure 3 is a central longitudinal section through another motor according to the invention.
      In the construction shown in Figures 1 and 2, there is a cylindrical casing 1 closed at the forward end and provided with a screw-threaded cap 2 at the rearward end, a washer 3 being interposed between the cap and the casing. A single jet orifice 4 is formed eccentrically in the cap and so are two openings 11 which are tapped to receive tubular valve fittings 5. The outer ends of these are formed with reamered orifices having sharp edges against which steel balls 6 are pressed by cups 7 carried by a leaf spring 8 which is held in a mounting 9 carried by the cap 2. This mounting is a stud in line with and midway between the valve fittings, and the leaf spring extends from it over each fitting and receives a pin 10 extending up from each cup 7. The mounting 9 is made of heat-insulating material and the cups 7 are lined with asbestos so as to minimise the transmission of heat to the spring. It is found to be important to harden the steel balls and to reamer the valve seats in the fittings because in this way a knife edge seat is formed and is still gas-tight on closing after the balls have moved to relieve abnormal pressure. The knife edge helps to cut through any dirt that may lodge on the valve seat.
      In the motor shown in Figure 3, a casing 2 of the same type is used and receives a screw-threaded end cap 12 into the middle of which an orifice member 13 is screwed. A thin frangible disc 14 is held against the inner face of the cap by a backing plate 15, which is itself held in position by a flange 16 on the orifice member 13. When a frangible disc is used, difficulty arises in making the disc both weak enough to yield directly the pressure rises and yet sufficiently resistant to heat to withstand the normal conditions. It is found that the requirements are satisfied if the frangible disc 14 is made of thin asbestos paper, say 0.02 inches thick, and registering holes 17 and 18 are made in the cap and backing plate respectively, these holes being individually small.Thus, there may be four holes in the cap and four corresponding holes in the backing plate and each hole may be, say, 1/16th of an inch in diameter. It is found that the unsupported parts of the disc in register with the holes in the cap and backing plate will then collapse under a pressure of about 175 lbs. per square inch. Naturally the frangible disc may be made of any other appropriate heat-resisting material, and its thickness and the size of the two sets of holes depend upon the exact strength of the material used.
      What we claim is: -
      1. A reaction motor of the type set forth comprising a casing for the reception of a gas-generating charge with one or more jet orifices for the discharge of the combustion gases in which a safety device controlling one or more openings separate from the jet orifice or orifices and consisting either of a spring-loaded valve, or of a frangible disc or the like, is provided to allow any abnormal pressure to be relieved.
      2. A reaction motor of the type set forth comprising a casing for the reception of a gas-generating charge with one or more jet orifices for the discharge of the combustion gases in which a spring-loaded valve separate from the jet orifice or orifices is provided to relieve the pressure within the casing should this rise above a predetermined value, the spring or springs being disposed outside the path of the gases.
      3. A motor according to claim 2 in which the valve comprises hardened steel balls engaging seats with knife edges.
      4. A motor according to claim 1 in which the safety device is a frangible disc made of asbestos paper or the like held in position between the inner wall of the rearward end of the casing and a backing plate formed with holes which register with holes made in the rearward end of the casing.
      5. A rocket motor according to any of the preceding claims in which there is a single jet orifice made eccentrically in a plug or the like screw-threaded into an opening in the rear end wall of the casing and another eccentric opening is provided in the same end wall and is closed by the spring-loaded valve or thin disc.
      6. A rocket motor of the type set forth constructed substantially as described with reference to Figures 1 and 2 or Figure 3 of the accompanying drawings.
For the Applicants:
GILL, JENNINGS & EVERY.
Chartered Patent Agents,
51/52 Chancery Lane, London, W.C.2.

Printed for Her Majesty's Stationery Office, by Wickes & Andrews Ltd., E.C.4.   89/244 — 1953
Published at The Patent Office, 25, Southampton Buildings. London, W.C.2, from which copies may be obtained.
  Fig. 1 Fig. 1

Fig. 2 Fig. 2

Fig. 3 Fig. 3
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Acknowledgements

- Original patents located, copied and compiled by Gerhard Everwyn; contributed by Terry Kidd

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