GB1525467A - Forming a composite article by moulding - Google Patents
Forming a composite article by mouldingInfo
- Publication number
- GB1525467A GB1525467A GB2463575A GB2463575A GB1525467A GB 1525467 A GB1525467 A GB 1525467A GB 2463575 A GB2463575 A GB 2463575A GB 2463575 A GB2463575 A GB 2463575A GB 1525467 A GB1525467 A GB 1525467A
- Authority
- GB
- United Kingdom
- Prior art keywords
- adhesive
- moulding
- forming
- lining
- phenol
- 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
Links
- 238000000465 moulding Methods 0.000 title abstract 5
- 239000002131 composite material Substances 0.000 title abstract 2
- 239000000853 adhesive Substances 0.000 abstract 5
- 230000001070 adhesive effect Effects 0.000 abstract 5
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 229910000831 Steel Inorganic materials 0.000 abstract 1
- 239000004411 aluminium Substances 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract 1
- 239000010425 asbestos Substances 0.000 abstract 1
- 230000001680 brushing effect Effects 0.000 abstract 1
- 239000003795 chemical substances by application Substances 0.000 abstract 1
- 239000011248 coating agent Substances 0.000 abstract 1
- 238000000576 coating method Methods 0.000 abstract 1
- 238000007598 dipping method Methods 0.000 abstract 1
- 229910052751 metal Inorganic materials 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 229910052895 riebeckite Inorganic materials 0.000 abstract 1
- 239000002904 solvent Substances 0.000 abstract 1
- 235000015096 spirit Nutrition 0.000 abstract 1
- 238000005507 spraying Methods 0.000 abstract 1
- 239000010959 steel Substances 0.000 abstract 1
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
- F02K9/34—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)
- Manufacture Of Macromolecular Shaped Articles (AREA)
Abstract
1525467 Attaching by moulding IMPERIAL METAL INDUSTRIES (KYNOCH) Ltd 21 May 1976 [9 June 1975] 24635/75 Heading B5A A method of forming a composite article, e.g. a gas transfer tube or a planar article for a rocket motor as shown in Fig. 1 comprises coating a pre-formed part by an aluminium or steel support 10 with an adhesive and then moulding a part, e.g. lining 14 against the adhesive to thereby bond with the preformed part, the moulded part being formed from material having self-release properties, e.g. it contains a mould release agent. The adhesive may be a phenol and the lining 14 may be formed from a phenol/asbestos moulding material. The adhesive may be applied in a solvent, e.g. methylated spirits by spraying, brushing, dipping or by filling and emptying the part 10. The latter may be degreased and shot-blasted to improve bonding. The adhesive may be partially cured so that it remains in place during moulding.
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EG47574A EG12325A (en) | 1973-11-12 | 1974-10-29 | Bis substituted succinamides and their utility as moulding techniques herbicides |
| GB2463575A GB1525467A (en) | 1975-06-09 | 1975-06-09 | Forming a composite article by moulding |
| AU14126/76A AU512442B2 (en) | 1975-06-09 | 1976-05-20 | Heat-insulative lining for rocket motor gas tube |
| IT23568/76A IT1070033B (en) | 1975-06-09 | 1976-05-24 | METHOD TO FORM A COMPOSITE ITEM INCLUDING THE PHASE OF PRINTING ONE OF ITS PARTS AND THE OTHER PART, PREFORMED |
| SE7606439A SE7606439L (en) | 1975-06-09 | 1976-06-08 | FORMING PROCEDURE |
| FR7617294A FR2316057A1 (en) | 1975-06-09 | 1976-06-08 | Gas pipe for rocket motor - produced from parts and simultaneously given plastic protective lining |
| DE19762625837 DE2625837A1 (en) | 1975-06-09 | 1976-06-09 | PROCESS FOR PRODUCING A COMPOSITE BODY |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2463575A GB1525467A (en) | 1975-06-09 | 1975-06-09 | Forming a composite article by moulding |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1525467A true GB1525467A (en) | 1978-09-20 |
Family
ID=10214836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2463575A Expired GB1525467A (en) | 1973-11-12 | 1975-06-09 | Forming a composite article by moulding |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1525467A (en) |
-
1975
- 1975-06-09 GB GB2463575A patent/GB1525467A/en not_active Expired
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |