GB1338281A - Internal combustion turbine engine - Google Patents
Internal combustion turbine engineInfo
- Publication number
- GB1338281A GB1338281A GB837071A GB837071A GB1338281A GB 1338281 A GB1338281 A GB 1338281A GB 837071 A GB837071 A GB 837071A GB 837071 A GB837071 A GB 837071A GB 1338281 A GB1338281 A GB 1338281A
- Authority
- GB
- United Kingdom
- Prior art keywords
- internal combustion
- power impulse
- cylinder
- exhaust
- reciprocated
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
Abstract
1338281 Power plant; rotary cylinder engines, valves, driving gear W L TODD 29 Feb 1972 [1 April 1971] 8370/71 Heading F1B, F1G, F1Q In a method of operating an I.C. engine a rotor 16, Fig. 1, which includes a cylinder 16, is mounted between bearings 12, 13, Fig. 2 and activated by internal combustion within the cylinder to rotate within a stator 4 having an induction passage 5 and a exhaust duct 6 in which vanes are fixed to co-operate with the exhaust gases to provide a secondary power impulse, the operating cycle being induction, compression, primary power impulse, secondary power impulse and exhaust. The piston 21 is reciprocated via a rod 23, shaft 17 and rollers 18, Fig. 2, which run in cam tracks 3. A slide valve 28 is reciprocated by cam 2 and the sparking plug 36 fires when terminal 37 contacts blade 35. (For Figures see next page)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB837071A GB1338281A (en) | 1972-02-29 | 1972-02-29 | Internal combustion turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB837071A GB1338281A (en) | 1972-02-29 | 1972-02-29 | Internal combustion turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1338281A true GB1338281A (en) | 1973-11-21 |
Family
ID=9851236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB837071A Expired GB1338281A (en) | 1972-02-29 | 1972-02-29 | Internal combustion turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1338281A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4078529A (en) * | 1976-04-15 | 1978-03-14 | Douglas Warwick | Rotary engine |
| GB2305471A (en) * | 1995-09-23 | 1997-04-09 | James Linton | Intermittant-combustion turbine engine |
-
1972
- 1972-02-29 GB GB837071A patent/GB1338281A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4078529A (en) * | 1976-04-15 | 1978-03-14 | Douglas Warwick | Rotary engine |
| GB2305471A (en) * | 1995-09-23 | 1997-04-09 | James Linton | Intermittant-combustion turbine engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |