CN102383969A - Kinetic energy pressure type jet engine - Google Patents
Kinetic energy pressure type jet engine Download PDFInfo
- Publication number
- CN102383969A CN102383969A CN2010102664193A CN201010266419A CN102383969A CN 102383969 A CN102383969 A CN 102383969A CN 2010102664193 A CN2010102664193 A CN 2010102664193A CN 201010266419 A CN201010266419 A CN 201010266419A CN 102383969 A CN102383969 A CN 102383969A
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- air
- kinetic energy
- heating chamber
- jet engine
- turbine
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Abstract
The invention relates to a jet engine which does work by utilizing kinetic energy pressure. The jet engine is characterized in that a fan, an air compressor, a heating chamber, a turbine and a tail jetter are connected in sequence in a shell. Liquid compressed air is sprayed into the heating chamber for gasification so as to blow the turbine to drive the air compressor to suck in air, compress the air and feed the compressed air to the heating chamber which is used for heating the compressed air, so that the gasification of the compressed air is accelerated, and the gasified compressed air is jet out backwards to do work.
Description
Affiliated technical field
Technical field is the air breathing engine field under the present invention, the present invention relates to a kind of air breathing engine that utilizes the work done of kinetic energy pressure.
Background technique
At present, known air breathing engine structure is to be linked in sequence and to be formed by fan, firing chamber, turbine, tail spray.Air is sucked gas compressor and the firing chamber is delivered in compression; Spray high pressure, high-temperature fuel gas work done backward with the fuel mix burning.But, can produce harmful gases such as carbon dioxide after its fuel used burning.
Summary of the invention
In order to overcome the deficiency that existing air breathing engine can produce harmful gases such as carbon dioxide, the present invention provides a kind of kinetic energy pressure type jet motor; This motor can not only provide power, and can not produce harmful gas.
The technical problem that solves
The technical solution adopted for the present invention to solve the technical problems is: in shell, fan, gas compressor, heating chamber, turbine, tail spray connect together with the turbine shaft order.In heating chamber, spray into liquid pressurized gas gasification, blow turbine and drive gas compressor and suck air and compression to deliver to heating chamber be that the pressurized gas heating is quickened gasification and sprayed work done backward; Reach the purpose that does not produce harmful gas.
The invention has the beneficial effects as follows: can in the air breathing engine work done, can not produce harmful gas.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the present invention is further specified
Fig. 1 is cross section structure figure of the present invention
1. fans among the figure, 2. gas compressor, 3. heating chamber, 4. turbine, 5. turbine shaft, 6. tail spray, 7. shell
Embodiment
In Fig. 1,, be linked in sequence with 5. turbine shafts with 1. fans, 2. gas compressor, 3. heating chamber, 4. turbine; The gas compressor pressurized gas is the liquid pressurized gas heating that sprays into heating chamber. liquid pressurized gas is to utilize the powered compressor air to form.
Claims (2)
1. air breathing engine that utilizes the work done of kinetic energy pressure in shell, fan, gas compressor, heating chamber, turbine, tail spray, is linked in sequence.It is characterized in that: the pressurized gas that gas compressor is sent into are the liquid pressurized gas heating that sprays at heating chamber.
2. air breathing engine according to claim 1 is characterized in that: liquid pressurized gas forms with the powered compressor air.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102664193A CN102383969A (en) | 2010-08-30 | 2010-08-30 | Kinetic energy pressure type jet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102664193A CN102383969A (en) | 2010-08-30 | 2010-08-30 | Kinetic energy pressure type jet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102383969A true CN102383969A (en) | 2012-03-21 |
Family
ID=45823721
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102664193A Pending CN102383969A (en) | 2010-08-30 | 2010-08-30 | Kinetic energy pressure type jet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102383969A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103742295A (en) * | 2014-01-15 | 2014-04-23 | 苟仲武 | Turbojet engine and method for mixing liquid gas during operation of turbojet engine |
| CN103742294A (en) * | 2014-01-15 | 2014-04-23 | 苟仲武 | Liquid gas afterburner jet engine and method for realizing afterburning flying of jet plane |
| CN104179595B (en) * | 2014-08-13 | 2016-03-02 | 西北工业大学 | A kind of general purpose engine directly adding hot air generation thrust |
| CN105888882A (en) * | 2014-12-25 | 2016-08-24 | 王正铉 | Device utilizing liquid carbon dioxide gasification to improve thrust of aircraft |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2086483A (en) * | 1980-10-31 | 1982-05-12 | Kershaw H A | Plant vaporizing a secondary fluid using heat of compression of a primary fluid. |
| GB2195402A (en) * | 1986-09-10 | 1988-04-07 | Kershaw H A | A method of power generation and it's use in a propulsion device |
| US4897995A (en) * | 1988-02-26 | 1990-02-06 | Guirguis Raafat H | Liquid turbojet engine |
| JPH0494442A (en) * | 1990-08-10 | 1992-03-26 | Mitsubishi Heavy Ind Ltd | Air liquefied cycle engine concurrently using ram jet |
| US5197323A (en) * | 1990-07-13 | 1993-03-30 | Sparta, Inc. | Pebble-bed heater and shock tube assembly |
| CN1355376A (en) * | 2000-11-28 | 2002-06-26 | 中国科学院低温技术实验中心 | Micro system energy driver doing work by expansion of low-temp medium |
| US20100107600A1 (en) * | 2008-11-05 | 2010-05-06 | Rolls-Royce Plc | Gas turbine engine variable area exhaust nozzle |
-
2010
- 2010-08-30 CN CN2010102664193A patent/CN102383969A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2086483A (en) * | 1980-10-31 | 1982-05-12 | Kershaw H A | Plant vaporizing a secondary fluid using heat of compression of a primary fluid. |
| GB2195402A (en) * | 1986-09-10 | 1988-04-07 | Kershaw H A | A method of power generation and it's use in a propulsion device |
| US4897995A (en) * | 1988-02-26 | 1990-02-06 | Guirguis Raafat H | Liquid turbojet engine |
| US5197323A (en) * | 1990-07-13 | 1993-03-30 | Sparta, Inc. | Pebble-bed heater and shock tube assembly |
| JPH0494442A (en) * | 1990-08-10 | 1992-03-26 | Mitsubishi Heavy Ind Ltd | Air liquefied cycle engine concurrently using ram jet |
| CN1355376A (en) * | 2000-11-28 | 2002-06-26 | 中国科学院低温技术实验中心 | Micro system energy driver doing work by expansion of low-temp medium |
| US20100107600A1 (en) * | 2008-11-05 | 2010-05-06 | Rolls-Royce Plc | Gas turbine engine variable area exhaust nozzle |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103742295A (en) * | 2014-01-15 | 2014-04-23 | 苟仲武 | Turbojet engine and method for mixing liquid gas during operation of turbojet engine |
| CN103742294A (en) * | 2014-01-15 | 2014-04-23 | 苟仲武 | Liquid gas afterburner jet engine and method for realizing afterburning flying of jet plane |
| CN104179595B (en) * | 2014-08-13 | 2016-03-02 | 西北工业大学 | A kind of general purpose engine directly adding hot air generation thrust |
| CN105888882A (en) * | 2014-12-25 | 2016-08-24 | 王正铉 | Device utilizing liquid carbon dioxide gasification to improve thrust of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice |
Addressee: Zhang Baihai Document name: the First Notification of an Office Action |
|
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120321 |