GB642689A - Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like - Google Patents

Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like

Info

Publication number
GB642689A
GB642689A GB3002247A GB3002247A GB642689A GB 642689 A GB642689 A GB 642689A GB 3002247 A GB3002247 A GB 3002247A GB 3002247 A GB3002247 A GB 3002247A GB 642689 A GB642689 A GB 642689A
Authority
GB
United Kingdom
Prior art keywords
casing
boss
motor
charge
model aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB3002247A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JOSEPH NAIME MANSOUR
Wilmot Mansour & Co Ltd
Original Assignee
JOSEPH NAIME MANSOUR
Wilmot Mansour & Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JOSEPH NAIME MANSOUR, Wilmot Mansour & Co Ltd filed Critical JOSEPH NAIME MANSOUR
Priority to GB3002247A priority Critical patent/GB642689A/en
Publication of GB642689A publication Critical patent/GB642689A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/38Safety devices, e.g. to prevent accidental ignition

Abstract

642,689. Rocket motors. WILMOT, MANSOUR, & CO., Ltd., WILMOT, C. M., and MANSOUR, J. N. Nov. 11, 1947, No. 30022. [Class 9 (ii)] A reaction motor for propelling model aircraft comprises a casing for a gas-generating charge in which a spring-pressed member containing one or more jet orifices is movable relatively to the casing to allow the combustion gases to escape past it if abnormal pressure builds up in the casing. The motor 3 comprises a cylindrical casing 5 of aluminium closed at the front end 6 and enclosing a solid gas-generating charge 7 with an igniting wick 8 led through a wire gauze disc 9 and a jet member 11 in a removable end cap 10. The end cap comprises an outer plate 12 separated from a backing plate 13 by an annular asbestos washer 14 and held together by the jet member which is screwed into a boss 15 on the outer plate. Wire rods 16 bent into an annular groove 18 in the plate 12 hold the cap in position. These rods pass through holes in a front plate 20 fitting over a boss 21 projecting from the end 6. The rods carry anchorage members 22 against which abut springs 25. The boss 21 has a threaded bore to receive the end of a bolt in a model aircraft. To insert a charge the end cap 10 is removed by applying pressure to the anchorage members. When the charge is ignited combustion gases escape through the jet member. Should the pressure become excessive the end cap moves rearwardly against the action of the springs to allow the gases to escape between the cap and the casing. To prevent overheating of the surface of the charge the casing wall is thickened towards the rear or provided with fins. A model aircraft, vehicle or vessel may be provided with a metal clip in which the motor is placed so that two of the anchorage members 22 enter a channel in the clip and the boss 15 drops into a slot in an upturned lug. Alternatively a lug secured to the boss 21 may enter a slot in the body of the craft, or again the motor may be simply inserted in a socket. Air passages for cooling purposes are left between the wall of the socket and the motor. In a modification, the nozzle or jet member has a cup-like extension and is held in position within an extension of the casing by a spring which yields to allow the nozzle to move outwardly under excess pressure.
GB3002247A 1947-11-11 1947-11-11 Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like Expired GB642689A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3002247A GB642689A (en) 1947-11-11 1947-11-11 Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3002247A GB642689A (en) 1947-11-11 1947-11-11 Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like

Publications (1)

Publication Number Publication Date
GB642689A true GB642689A (en) 1950-09-06

Family

ID=10300996

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3002247A Expired GB642689A (en) 1947-11-11 1947-11-11 Improvements relating to reaction motors suitable for the jet propulsion of model aircraft or the like

Country Status (1)

Country Link
GB (1) GB642689A (en)

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