GB676525A - Improvements in or relating to power gas generating assemblies - Google Patents

Improvements in or relating to power gas generating assemblies

Info

Publication number
GB676525A
GB676525A GB10162/49A GB1016249A GB676525A GB 676525 A GB676525 A GB 676525A GB 10162/49 A GB10162/49 A GB 10162/49A GB 1016249 A GB1016249 A GB 1016249A GB 676525 A GB676525 A GB 676525A
Authority
GB
United Kingdom
Prior art keywords
wall member
end wall
metal tube
end plate
grooves
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
GB10162/49A
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.)
Imperial Chemical Industries Ltd
Original Assignee
Imperial Chemical Industries 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
Priority to BE495121D priority Critical patent/BE495121A/xx
Application filed by Imperial Chemical Industries Ltd filed Critical Imperial Chemical Industries Ltd
Priority to GB10162/49A priority patent/GB676525A/en
Publication of GB676525A publication Critical patent/GB676525A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/38—Safety devices, e.g. to prevent accidental ignition
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

676,525. Rocket propulsion; gas generating cartridges. LIVINGSTON, R., HUTCHISON, A. C., and IMPERIAL CHEMICAL INDUSTRIES, Ltd. March 9, 1950. [April 14, 1949] No. 10162/49. Class 9 (i). [Also in Group XII] A power gas-generating assembly comprises a non-expendable framework portion and an expendible portion, the frame-work portion comprising a fore end wall member 2, an after end wall member 27 and an after end plate 1, and the expendable portion comprises an annular gas-generating charge 19 of solid composition contained in a metal tube 17 which extends:beyond the charge at both ends. The forward end wall member 2 and the after end wall member 27 have grooves 8 and 15 formed in their inner faces and are held at a variable distance apart so as to allow for minor variations in the lengths of the metal casings 17 of the expendable portions which are accommodated within the grooves 8 and 15. The after end wall member 27 may' be formed integrally with the after end plate 1, in which case the after end plate and the fore end wall member are held at variable distances apart by means of spacing rods which may be adjusted so as to clamp the metal tube 17 tightly in the grooves 8, 15. As shown in the Figures, the fore end wall member 2 and the after end plate 1 are held at a fixed distance apart by means of spacing rods 10, and the metal tube 17 is clamped by means of a locking nut 13 which screws into the after end plate 1 and bears against the after end wall member 27. The after end wall member 27 carries a propulsion nozzle 14 when the device is used for rocket propulsion, or a delivery pipe when the power gas is utilised in a turbine or reciprocating engine. The fore end wall member 2 has a safety bursting disc 6 and a hood 12 for deflecting the gases should the disc rupture. The ignition means 22 for the cartridge is situated at the forward end. A heat insulating layer 18 is disposed between the gas generating charge 19 and the metal tube 17, and the ends of the cartridge are closed by caps during storage.
GB10162/49A 1949-04-14 1949-04-14 Improvements in or relating to power gas generating assemblies Expired GB676525A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
BE495121D BE495121A (en) 1949-04-14
GB10162/49A GB676525A (en) 1949-04-14 1949-04-14 Improvements in or relating to power gas generating assemblies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10162/49A GB676525A (en) 1949-04-14 1949-04-14 Improvements in or relating to power gas generating assemblies

Publications (1)

Publication Number Publication Date
GB676525A true GB676525A (en) 1952-07-30

Family

ID=9962666

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10162/49A Expired GB676525A (en) 1949-04-14 1949-04-14 Improvements in or relating to power gas generating assemblies

Country Status (2)

Country Link
BE (1) BE495121A (en)
GB (1) GB676525A (en)

Also Published As

Publication number Publication date
BE495121A (en)

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