NL7613617A - Ignition system for engines - which is esp. for use when ignition has to be at rear of engine - Google Patents
Ignition system for engines - which is esp. for use when ignition has to be at rear of engineInfo
- Publication number
- NL7613617A NL7613617A NL7613617A NL7613617A NL7613617A NL 7613617 A NL7613617 A NL 7613617A NL 7613617 A NL7613617 A NL 7613617A NL 7613617 A NL7613617 A NL 7613617A NL 7613617 A NL7613617 A NL 7613617A
- Authority
- NL
- Netherlands
- Prior art keywords
- ignition
- engine
- dia
- igniter
- tube
- Prior art date
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
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
Abstract
An ignition system for an engine incorporates a cylindrical tube open at one end and closed at the other, with a section reduced in dia. at the closed end. There are several segments projecting outwards near the closed end, an igniter in the section of reduced dia. and a charge in the tube. In the open end is a polyurethane foam wad and around the igniter a shock-absorbing ring of the same material. The tube itself is made of material e.g. 30% glass fibre and 70% Nylon (RTM). The charge consists of e.g. granules of nitrate of potassium and of boron, 3.175 mm dia., 4.775 mm long. The system is partic. intended for an engine with a jet-pipe having a single orifice, in which the ignition has to be at the rear, because of the isolated configuration of the head.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL7613617A NL168297C (en) | 1976-12-08 | 1976-12-08 | IGNITION FOR A ROCKET ENGINE. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL7613617A NL168297C (en) | 1976-12-08 | 1976-12-08 | IGNITION FOR A ROCKET ENGINE. |
Publications (3)
Publication Number | Publication Date |
---|---|
NL7613617A true NL7613617A (en) | 1978-06-12 |
NL168297B NL168297B (en) | 1981-10-16 |
NL168297C NL168297C (en) | 1982-03-16 |
Family
ID=19827346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL7613617A NL168297C (en) | 1976-12-08 | 1976-12-08 | IGNITION FOR A ROCKET ENGINE. |
Country Status (1)
Country | Link |
---|---|
NL (1) | NL168297C (en) |
-
1976
- 1976-12-08 NL NL7613617A patent/NL168297C/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
NL168297B (en) | 1981-10-16 |
NL168297C (en) | 1982-03-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
V1 | Lapsed because of non-payment of the annual fee |