DE3627322A1 - Turbojet - Google Patents
TurbojetInfo
- Publication number
- DE3627322A1 DE3627322A1 DE19863627322 DE3627322A DE3627322A1 DE 3627322 A1 DE3627322 A1 DE 3627322A1 DE 19863627322 DE19863627322 DE 19863627322 DE 3627322 A DE3627322 A DE 3627322A DE 3627322 A1 DE3627322 A1 DE 3627322A1
- Authority
- DE
- Germany
- Prior art keywords
- nozzle
- cow horn
- cow
- balanced
- thrust
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
- F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Description
Bei einer herkömmlichen Rakete und einem Strahltriebwerk bewir ken Rückstoß und Durchfluß den Vortrieb.With a conventional rocket and a jet engine recoil and flow the propulsion.
Mit meiner Neuerung leite ich den Gasstrahl durch ein konisches und gebogenes Rohr und mehrere Verbrennungskammern. In dem spi ralförmigen Rohr wandel ich den Gasstrahldruck in Druck- und Unterdruckzonen um, die auf die Rohrwandung wirken und die sy metrisch gelagerte Düse in Drehung bringt. Die Länge meines spiralförmigen, konischen Schlangenrohres und die Anzahl der Verbrennungskammern, die im Verhältnis zur ersten Verbrennungs kammer stehen, bestimmen Verbrennungsgrad, Lärmstärke, Wir kungsgrad und Gasmenge.With my innovation, I direct the gas jet through a conical one and bent tube and several combustion chambers. In the spi raliform tube I convert the gas jet pressure into pressure and Vacuum zones around, which act on the pipe wall and the sy metric nozzle rotates. The length of mine spiral, conical snake tube and the number of Combustion chambers that are in proportion to the first combustion standing chamber, determine degree of combustion, noise level, we efficiency and amount of gas.
Bei optimalem Verhältnis erreiche ich restlose Verbrennung, Ge räuschlosigkeit bei hohem Wirkungsgrad.With an optimal ratio I achieve complete combustion, Ge noiselessness with high efficiency.
Auf meiner Zeichnung "2" habe ich ein Pulso-Strahl triebwerk mit meinem düsenförmigen Abströmrohr, drehbar gela gert, als Luftblatttrieb gezeichnet, bei "1" ein Strahltrieb werk und auf Blatt "3" das System.On my drawing "2" I have a pulsed jet engine with my nozzle-shaped outflow pipe, rotatably mounted, drawn as an air bladed drive, at "1" a jet engine and on sheet "3" the system.
Vorteil der Neuerung:
Da eine Reihe von Energieumsetzungsprozesse und deren Verluste
vermieden werden, niedrige Fertigungskosten, geräuscharme,
vollkommene Verbrennung, geringe Wartungskosten, leichte Bau
weise.Advantage of the innovation:
Because a number of energy conversion processes and their losses are avoided, low manufacturing costs, low-noise, perfect combustion, low maintenance costs, lightweight construction.
Claims (8)
StrahltriebturbineGeneric term:
Jet engine turbine
Kuhhorn- oder schlangenförmige Gasab strömdüse.Characteristic part:
Cow horn or serpentine gas outlet nozzle.
Abströmrohr sieht wie ein Kuhhorn oder eine Schlange aus.General term / characteristics:
Drain pipe looks like a cow horn or a snake.
Eine herkömmliche Impulsorakete oder Ex plosionsraum mit der kuhhornförmigen Abströmdüse setzt die ge samte Energie, in dem Kuhhorn aus Blech, in Schub um. Atmosphä rischer Rückstoß erfolgt nicht, so daß diese Technik im Welt raum ihre Höchstleistung erreicht und dort unendlich zu be schleunigen ist.Inventive features:
A conventional impulse rocket or explosion room with the cowhorn-shaped outflow nozzle converts the entire energy, in the cow horn made of sheet metal, into thrust. Atmospheric recoil does not occur, so that this technology achieves its maximum performance in space and can be accelerated there infinitely.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19863627322 DE3627322A1 (en) | 1986-08-12 | 1986-08-12 | Turbojet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19863627322 DE3627322A1 (en) | 1986-08-12 | 1986-08-12 | Turbojet |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3627322A1 true DE3627322A1 (en) | 1988-06-01 |
Family
ID=6307219
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19863627322 Ceased DE3627322A1 (en) | 1986-08-12 | 1986-08-12 | Turbojet |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3627322A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10118373B4 (en) * | 2001-04-12 | 2009-04-09 | Josef Geimer | Rotary ramjet engine as drive unit in stationary and mobile applications |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DD15849A (en) * | ||||
GB314722A (en) * | 1928-09-11 | 1929-07-04 | Hans Strauscheid | A reaction gas turbine |
DE557859C (en) * | 1928-11-28 | 1932-08-29 | Explorotor A G | Rotary engine whose impeller is provided with channels for the passage of the propellant |
US2644301A (en) * | 1949-02-08 | 1953-07-07 | Karlby Henning | Ram jet turbine |
US2978205A (en) * | 1958-09-29 | 1961-04-04 | Ryan Aeronautical Co | Tip-jet driven ducted fan for aircraft |
US3008293A (en) * | 1957-05-18 | 1961-11-14 | Snecma | Intermittently-operating thermo-propulsive duct designed for driving a shaft and applicable to rotary wing aircraft |
US3677503A (en) * | 1968-07-31 | 1972-07-18 | Carlos A Freeman Jr | Reaction--impulse--counterrotating--airfoil |
-
1986
- 1986-08-12 DE DE19863627322 patent/DE3627322A1/en not_active Ceased
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DD15849A (en) * | ||||
GB314722A (en) * | 1928-09-11 | 1929-07-04 | Hans Strauscheid | A reaction gas turbine |
DE557859C (en) * | 1928-11-28 | 1932-08-29 | Explorotor A G | Rotary engine whose impeller is provided with channels for the passage of the propellant |
US2644301A (en) * | 1949-02-08 | 1953-07-07 | Karlby Henning | Ram jet turbine |
US3008293A (en) * | 1957-05-18 | 1961-11-14 | Snecma | Intermittently-operating thermo-propulsive duct designed for driving a shaft and applicable to rotary wing aircraft |
US2978205A (en) * | 1958-09-29 | 1961-04-04 | Ryan Aeronautical Co | Tip-jet driven ducted fan for aircraft |
US3677503A (en) * | 1968-07-31 | 1972-07-18 | Carlos A Freeman Jr | Reaction--impulse--counterrotating--airfoil |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10118373B4 (en) * | 2001-04-12 | 2009-04-09 | Josef Geimer | Rotary ramjet engine as drive unit in stationary and mobile applications |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8127 | New person/name/address of the applicant |
Owner name: WERDING, HANS, 2800 BREMEN, DE |
|
8127 | New person/name/address of the applicant |
Owner name: WERDING, HANS, 4520 MELLE, DE |
|
8181 | Inventor (new situation) |
Free format text: ERFINDER IST ANMELDER |
|
8110 | Request for examination paragraph 44 | ||
8131 | Rejection |