CN104018953A - Nuclear engine - Google Patents

Nuclear engine Download PDF

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Publication number
CN104018953A
CN104018953A CN201310065975.8A CN201310065975A CN104018953A CN 104018953 A CN104018953 A CN 104018953A CN 201310065975 A CN201310065975 A CN 201310065975A CN 104018953 A CN104018953 A CN 104018953A
Authority
CN
China
Prior art keywords
uranium
neutral particle
engine
generating device
particle generating
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.)
Pending
Application number
CN201310065975.8A
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Chinese (zh)
Inventor
孙国莉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201310065975.8A priority Critical patent/CN104018953A/en
Publication of CN104018953A publication Critical patent/CN104018953A/en
Pending legal-status Critical Current

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Abstract

In the technical field, a nuclear engine can be used for various aircrafts. Based on the background technology, the nuclear engine is a novel engine and can meet the requirements of various aircrafts. An air injection device assembly is composed of a fixing piece/cylinder, a uranium spraying device and a neutral particle generating device. On the aspects of shape and structure and on the aspects of effect, the air injection device assembly is characterized in that the fixing piece/cylinder is of a semi-closed structure and can be of various shapes, and the other parts, namely, the uranium spraying device and the neutral particle generating device (please see the parts in the attached drawings), are not limited in number. According to the main principle, namely, the principle of the engine, particle flow is emitted to sprayed-out uranium atomic nucleuses through the neutral particle generating device, so that impact force is generated due to thermal energy caused when chain fission happens to uranium nucleuses.

Description

Nucleon motor
Technical field
This motor can be used on various aircraft and use.
Background technique
This is a kind of novel motor, can meet various aircraft requirements.
1, air jet system totally forms
A, forms: uranium device, neutral particle generator are stopped, sprayed to fixed block/cylinder.
B, each several part physique structure feature and effect feature:
A, fixed block/cylinder body is semi-closed structure:
Can be various shape and structures.
B, other parts:
(as accompanying drawing) has spray uranium device, neutral particle device, and usage quantity is not limit.
2, cardinal principle effect
Prestige engine principles: the uranium nuclei emitted particle by neutral particle generator to ejection flows, makes the fission of uranium core generation chain type produce heat energy and impact force.
Accompanying drawing explanation:
Accompanying drawing is < < nucleon motor schematic diagram > >.

Claims (4)

1. nucleon engine principles: produce chain reaction of nuclear fission and produce impact force by neutral particle (neutron) bombardment uranium nuclei.
2. form: fixed block/cylinder body, spray uranium device, neutral particle generator.
3. by " spray uranium device " and " neutral particle generator ", become a set ofly, each usage quantity requirement is more than 1, and position is not limit.
4. fixed block/cylinder body is various physique structures.
CN201310065975.8A 2013-03-01 2013-03-01 Nuclear engine Pending CN104018953A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310065975.8A CN104018953A (en) 2013-03-01 2013-03-01 Nuclear engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310065975.8A CN104018953A (en) 2013-03-01 2013-03-01 Nuclear engine

Publications (1)

Publication Number Publication Date
CN104018953A true CN104018953A (en) 2014-09-03

Family

ID=51435890

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310065975.8A Pending CN104018953A (en) 2013-03-01 2013-03-01 Nuclear engine

Country Status (1)

Country Link
CN (1) CN104018953A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101054932A (en) * 2007-04-18 2007-10-17 陈久斌 Nuclear power engine and aerocraft produced thereby and spacecraft
CN101117927A (en) * 2007-08-23 2008-02-06 陈久斌 Nuclear reactor and flying saucer made by it
US20110051876A1 (en) * 2009-08-28 2011-03-03 Searete Llc, A Limited Liability Corporation Nuclear fission reactor, a vented nuclear fission fuel module, methods therefor and a vented nuclear fission fuel module system
CN102209990A (en) * 2008-09-18 2011-10-05 希尔莱特有限责任公司 System and method for annealing nuclear fission reactor materials
CN102217000A (en) * 2008-09-11 2011-10-12 得克萨斯大学体系董事会 Fusion neutron source for fission applications

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101054932A (en) * 2007-04-18 2007-10-17 陈久斌 Nuclear power engine and aerocraft produced thereby and spacecraft
CN101117927A (en) * 2007-08-23 2008-02-06 陈久斌 Nuclear reactor and flying saucer made by it
CN102217000A (en) * 2008-09-11 2011-10-12 得克萨斯大学体系董事会 Fusion neutron source for fission applications
CN102209990A (en) * 2008-09-18 2011-10-05 希尔莱特有限责任公司 System and method for annealing nuclear fission reactor materials
US20110051876A1 (en) * 2009-08-28 2011-03-03 Searete Llc, A Limited Liability Corporation Nuclear fission reactor, a vented nuclear fission fuel module, methods therefor and a vented nuclear fission fuel module system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
史朝龙等: "国外核动力发动机的关键技术及应用前景", 《飞航导弹》 *

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Addressee: Sun Guoli

Document name: Written decision of reexamination

RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20140903