GB959360A - Articles having resin-impregnated walls - Google Patents

Articles having resin-impregnated walls

Info

Publication number
GB959360A
GB959360A GB4822562A GB4822562A GB959360A GB 959360 A GB959360 A GB 959360A GB 4822562 A GB4822562 A GB 4822562A GB 4822562 A GB4822562 A GB 4822562A GB 959360 A GB959360 A GB 959360A
Authority
GB
United Kingdom
Prior art keywords
face
resin
laminations
nozzle
impregnated
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
GB4822562A
Inventor
Elmer Pershing Warnken
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.)
Studebaker Corp
Original Assignee
Studebaker Corp
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 Studebaker Corp filed Critical Studebaker Corp
Priority to GB4822562A priority Critical patent/GB959360A/en
Publication of GB959360A publication Critical patent/GB959360A/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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

959,360. Non-metallic pipes. STUDEBAKER CORPORATION. Dec. 20, 1962, No. 48225/62. Heading F2P. [Also in Divisions B5, F1 and F3] An annular wall having a face for engagement by fluid flow and formed of resin-impregnated annular flat fabric laminations arranged in face-to-face, aligned, substantially parallel overlapping relation, has each lamination extending towards the fluid with a minor portion of one of its faces along one edge exposed to trailing contact with the fluid flow and a major portion of the face overlapped by an adjacent upstream lamination. A rocket exhaust nozzle, Fig. 9, is formed of a strip of resin-impregnated glass or asbestos fibre 37 wound in overlapping relationship. The laminations 43 are at a substantially constant angle to the inner face of the nozzle from the inlet to the throat 44 and from the throat 44 onwards they are parallel to the axis of the nozzle. The moulding of the laminations 37 on a two piece mandrel 35, 36 is described. The construction is applicable generally to bodies subject to high fluid velocities.
GB4822562A 1962-12-20 1962-12-20 Articles having resin-impregnated walls Expired GB959360A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4822562A GB959360A (en) 1962-12-20 1962-12-20 Articles having resin-impregnated walls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4822562A GB959360A (en) 1962-12-20 1962-12-20 Articles having resin-impregnated walls

Publications (1)

Publication Number Publication Date
GB959360A true GB959360A (en) 1964-06-03

Family

ID=10447827

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4822562A Expired GB959360A (en) 1962-12-20 1962-12-20 Articles having resin-impregnated walls

Country Status (1)

Country Link
GB (1) GB959360A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2243104A (en) * 1990-04-20 1991-10-23 Gen Electric Mold tool for consolidating composite materials
GB2300138A (en) * 1995-04-21 1996-10-30 Fluorovac Ltd Seal arrangement in vacuum bagging moulding
FR2850369A1 (en) * 2003-01-23 2004-07-30 Eads Space Transportation Sa Application of heat-resistant coating to rocket nozzle or space vehicle re-entry shield consists of applying layers at constant angle and adjusting thickness
CN101733614B (en) * 2008-11-20 2011-12-07 中国兵器工业第五九研究所 Method for preparing rocket engine jet pipe and special equipment thereof

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2243104A (en) * 1990-04-20 1991-10-23 Gen Electric Mold tool for consolidating composite materials
US5145621A (en) * 1990-04-20 1992-09-08 General Electric Company Crossover mold tool for consolidating composite material
GB2243104B (en) * 1990-04-20 1993-11-17 Gen Electric Mold tool for consolidating composite materials
GB2300138A (en) * 1995-04-21 1996-10-30 Fluorovac Ltd Seal arrangement in vacuum bagging moulding
FR2850369A1 (en) * 2003-01-23 2004-07-30 Eads Space Transportation Sa Application of heat-resistant coating to rocket nozzle or space vehicle re-entry shield consists of applying layers at constant angle and adjusting thickness
WO2004067943A1 (en) * 2003-01-23 2004-08-12 Eads Space Transportation Sa. Method of producing a thermal barrier coating comprising inclined layers and structures thus obtained
CN101733614B (en) * 2008-11-20 2011-12-07 中国兵器工业第五九研究所 Method for preparing rocket engine jet pipe and special equipment thereof

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