LTIP134A - Jet rotary engine - Google Patents
Jet rotary engineInfo
- Publication number
- LTIP134A LTIP134A LTIP134A LTIP134A LTIP134A LT IP134 A LTIP134 A LT IP134A LT IP134 A LTIP134 A LT IP134A LT IP134 A LTIP134 A LT IP134A LT IP134 A LTIP134 A LT IP134A
- Authority
- LT
- Lithuania
- Prior art keywords
- combustion chamber
- air
- windows
- jet
- air channel
- Prior art date
Links
Landscapes
- Jet Pumps And Other Pumps (AREA)
- Supercharger (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
Išradimas susijęs su reaktyviniais vidaus degimo varikliais ir gali būti panaudotas įvairiuose techniniuose objektuose: transporto ir žemės ūkio mašinose, stacionarinuose įrenginiuose ir kitiems tikslams.@Išradimo tikslas - padidinti variklio naudingumo koeficentą.@Variklio statorius turi koncentrišką kolektorių (1) su langais (2) atidirbusioms dujoms išeiti, atidirbusių dujų utilizacijos sistema, atidirbusių dujų ištekėjimo iš kolektoriaus pagreitinimo sistema su mentėmis (4), nejudomai išdėstytomis kolektoriuje. Rotoriaus velenas (7) turi kanalus (8 ir 9) dujomis ir orui paduoti per langus (10) į degimo kamerą (11). Degimo kamera apgaubta papildomu kontūru (14), sudarančiu oro kanalą. Išorinėje degimo kameros dalyje yra reaktyvinės tūtos (15). Pertvarėlė (16) skirta įeinančiam orui nukreipti oro kanalu į degimo kamerą (11).The invention relates to jet combustion engines and can be used in a variety of technical facilities: transport and agricultural machinery, stationary equipment and other purposes. @ The object of the invention is to increase the efficiency of the motor. @ The motor stator has a concentric collector (1) with windows (2) Exhaust Gas Exhaust System, Exhaust Gas Exhaust System Accelerator System with blades (4), stationary in the manifold. The rotor shaft (7) has channels (8 and 9) for gas and air to pass through windows (10) into the combustion chamber (11). The combustion chamber is surrounded by an additional contour (14) forming the air channel. There are jet nozzles (15) in the outer part of the combustion chamber. The partition (16) is designed to direct the incoming air through the air channel to the combustion chamber (11).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LTIP134A LT3025B (en) | 1992-10-01 | 1992-10-01 | Jet rotary engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LTIP134A LT3025B (en) | 1992-10-01 | 1992-10-01 | Jet rotary engine |
Publications (2)
Publication Number | Publication Date |
---|---|
LTIP134A true LTIP134A (en) | 1994-04-25 |
LT3025B LT3025B (en) | 1994-08-25 |
Family
ID=19721053
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
LTIP134A LT3025B (en) | 1992-10-01 | 1992-10-01 | Jet rotary engine |
Country Status (1)
Country | Link |
---|---|
LT (1) | LT3025B (en) |
-
1992
- 1992-10-01 LT LTIP134A patent/LT3025B/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
LT3025B (en) | 1994-08-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM9A | Lapsed patents |
Effective date: 20011001 |