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ARCHIVE: Patent 922,560
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ARCHIVE > Patents > Patent 922,560

PATENT SPECIFICATION 922,560
Inventors: CECIL ARTHUR RASSIER and JOSEPH NAIME MANSOUR.

 
Date of filing Complete Specification: Aug. 24, 1959.
Application Date: Aug. 25, 1958. No. 27258/58.
Complete Specification Published: April 3, 1963.


COMPLETE SPECIFICATION

Improvements in or relating to Rocket Motors

      We, D. SEBEL & COMPANY LIMITED, of 177, West Street, Erith, Kent, a British Company, 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
      The present invention relates to small rocket motors suitable for use in a model aircraft or other vehicle or for other purposes.
      In such a small motor gases are usually generated by igniting a combustible composition in the casing, ignition being effected by producing a temperature sufficient to ignite the combustible composition by means either of a fuse or hot point. In such motors where lightness of weight is essential the strength of the parts is necessarily comparably low and in particular the casing in which the gas generating composition is placed and in which it burns must be made as thin walled as possible. The propelling thrust is created by the combustion gases passing rearwardly through one or more small jet orifices in the casing. In the event of the jet orifice or orifices becoming clogged a high pressure rapidly builds up in the casing which may well lead to the bursting of the casing. A construction of casing is already known in which provision is made for relieving excess pressure and which comprises a cap on the casing which lifts on excess pressure being built up in the casing.
      An object of the present invention is to provide a construction of small reaction motor of the rocket type which is provided with a safety device to allow any abnormal pressure to be relieved and to permit the device to be reset and in which the cap is held in fixed relation to the casing.
      According to the present invention there is provided a rocket motor having a device for relieving any abnormal pressure in the combustion chamber thereof, which device comprises a frangible diaphragm, held in position between the inner wall of the rearward end of the casing of the motor and a backing plate, formed with holes which register with holes in the rearward end of the casing said plate being held positively against the said inner wall around its periphery.
 
In the event of the jet orifice or orifices becoming clogged a high pressure rapidly builds up in the casing which may well lead to the bursting of the casing.
      For a better understanding of the invention and to show how the same may be carried into effect reference will now be made to the accompanying drawings in which:
      Figure 1 is a fragmentary part sectional elevation of a small reaction motor of the rocket type incorporating the present invention; and
      Figure 2 is a fragmentary perspective view to an enlarged scale of a modified detail of a small reaction motor incorporating the present invention.
      The reaction motor shown in Figure 1 comprises a combustion chamber having a casing 1 of substantially cylindrical configuration closed at one end 2 and provided at the rear end 3 with a cap 4 secured to the casing 1 by means of a screw thread 5.
      Projecting from the middle of the cap 4 is the jet orifice 6 which is located at the end of a rearwardly directed nozzle 7. Around the base of the nozzle 7 and in the wall 8 of the cap are three apertures 9 of about 1/16th of an inch in diameter. On the inside of the cap 4 is a back plate 10 having three apertures 11 similarly spaced and having also a fourth aperture 12 which engages a short locating pin 13 mounted on the inside face of the wall 8 of the cap 4. This locating pin 13 ensures that the apertures in the back plate 10 coincide with the apertures 9 in the cap 4.
      The centre of the back plate apertured as at 14 to give access so that the jet orifice 6 is open to the interior of the combustion chamber casing 1.
      The back plate 10 fits snugly into the cap 4 so that when the cap 4 is screwed home onto the cylindrical casing 1 of the motor it is gripped firmly between the cap 4 and the annular end face 15 of the motor casing and is pressed firmly towards the inside face of the wall 8 of the cap.
  Fig. 1 Fig. 1
      Between the back plate 10 and the inside face of the cap there is fitted an annulus 17 of asbestos paper which may be of any suitable thickness for example 0.012 of an inch thick or 0.02 of an inch thick, depending upon the pressure at which relief is desired. For example, the thickness of the annulus can be such that it will fracture at a pressure of about 50 pounds per square inch or more depending upon the design of the motor and the pressure of the operating thrust.
      The screw threading 3 may if desired take the form of three or more lugs 19 mounted or formed on the outer surface of the motor casing 1 engaging with lugs 20 on the inside of the cap 4 the lugs on one or the other or both having inclined faces up which the ether lugs ride. This is shown in figure 2.
 
[T]he thickness of the annulus can be such that it will fracture at a pressure of about 50 pounds per square inch or more
      For convenience it is preferred for threads on the cap 4 and the casing 1 to be rolled into the material.
      Conveniently, the screw threading or other means for securing the cap to the casing is such that in the event of any one [sic] attempting to insert a diaphragm of thicker material, for example a metal annulus, the screw threading or other securing means will not engage.
      When the motor is in use and the jet becomes clogged pressure builds up in the casing 1 until the asbestos paper annulus 17 spanning the holes in the cap and the apertures 11 in the back plate 10 bursts giving an immediate relief of pressure in the casing 1.
      In order to put the motor into working operation again it is only necessary to remove the back plate 10, insert a new annulus 17 of asbestos paper or other frangible material, and reinsert the back plate 10 and screw the cap 4 home upon the casing 1.
      WHAT WE CLAIM IS:
      1. A rocket motor provided with a device for relieving any abnormal pressure in the combustion chamber thereof, comprising a frangible element held in position between the inner wail of the rearward end of the casing of the combustion chamber and a backing plate formed with holes which register with holes in the rearward end of the casing, the backing plate being held positively around its periphery against the inner wall.
      2. A motor as claimed in Claim 1, wherein the. frangible element and the backing plate are held in position by a cap which is secured to the casing, and wherein the jet orifice of the motor is located in the cap.
      3. A motor as claimed in Claim 2, wherein the cap is screwed, or otherwise releasably secured to the casing so that the frangible element is readily replaceable in the event of the element being fractured.
      4. A motor as claimed in Claim 1, 2 or 3 wherein the frangible element is constituted by an annular disc having a through bore for the propelling gases to be fed to the jet orifice of the motor, the disc being formed from asbestos paper or other material which may be made to fracture at or above a predetermined pressure.
      5. A motor as claimed in Claim 2, 3 or 4, wherein the means provided on the cap for releasably securing same to the casing is such that if the thickness of the frangible element exceeds a predetermined value the cap can not be secured to the casing.
      6. A motor for having a device for relieving pressure in the combustion chamber, substantially as hereinbefore described with reference to Figure 1 or 2 of the accompanying drawing.

For the Applicant:
ARNOLD TICKNER,
Chartered Patent Agent,
Alexander House,
239/241, Shaftesbury Avenue,
London, W.C.2.

Leamington Spa: Printed for His Majesty's Stationery Office, by the Courier Press.—1963.
Published by The Patent Office, 25, Southampton Buildings, London, W.C.2, from which copies may be obtained.
  Fig. 2 Fig. 2
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Acknowledgements

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

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