CN105905304A

CN105905304A - Manufacturing device of nuclear power bomber

Info

Publication number: CN105905304A
Application number: CN201610024803.XA
Authority: CN
Inventors: 陈从龙
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-01-06
Filing date: 2016-01-06
Publication date: 2016-08-31

Abstract

The invention relates to a manufacturing device of a nuclear power bomber. The device comprises a machine head, a machine body, a belly launch canister, balance wings, a rear machine body, a refrigeration air compressor chamber, a three-dimensional water tank, a blocking thermal insulating space, and a bolt. The machine head is internally provided with a turbine engine. The machine body can carry a nuclear warhead. The balance wings can hang a plurality of nuclear bombs. The refrigeration air compressor chamber, the three-dimensional water tank, a peripheral air cooling channel, and the blocking thermal insulating space have the same functions of blocking, stopping, isolating, and eliminating surface heat energy of an air cooling nuclear reactor, so that a nuclear power bomber can fly normally. When the nuclear reactor is hit by a guided missile, a pilot presses a button in a moment, the bolt separates from a dowel, and is pulled out in a moment under the tension of a tightener spring. Thus, the machine body and the rear machine body are separated, the air cooling nuclear reactor is thrown away, and safety of the pilot, the bomber, and the built-in nuclear warheads is guaranteed.

Description

A kind of manufacture device of nuclear-powered bomber

Technical field:

Described bomber manufactures device, is specifically related to the manufacture device of a kind of nuclear-powered bomber.

Background technology:

A kind of manufacture device of nuclear-powered bomber, it it is the problem of countries in the world scientist research, each state all wants to take the lead in studying successfully, owing to the reactor face temperature of nuclear-powered bomber is the highest, it is difficult to eliminate, therefore the manufacture of nuclear-powered bomber fails to realize so far, not enough in order to solve China's existing bomber fuel load awing, the defect that flight time is shorter, needs according to China's era development, a a kind of novel nuclear-powered bomber must be developed, meet the needs of China's national defense, safeguard our territory of country, territorial sky and the safety in territorial waters.

Summary of the invention:

For the deficiency that the bomber overcoming China is above-mentioned, the present invention provides a kind of nuclear-powered bomber to manufacture device, and its machine need not refuel, and carries nuclear bomb and is several months flight.

Technical scheme:

It is an object of the invention to provide the manufacture device of a kind of nuclear-powered bomber, including head, fuselage, abdominal part launching tube, short limb, balance wing, back launching tube, gate, joint, latch, cooling air compressor room, three-dimensional water railway carriage or compartment, block insulated space, rear body, all around cold air road, gas-cooled nuclear reactor base, the tail wing, gas-cooled nuclear reactor, steam vent, block；Fig. 1, it is characterized in that head is connected with fuselage, head lower end sets turbogenerator, hundred pieces of nuclear warheads can be loaded in fuselage, two ends connect short limb, short limb two ends connect balance wing, its wing lower end can hang nuclear bomb, described belly connects nuclear bomb launching tube, back sets launcher, its connection back, upper end nuclear bomb launching tube, built-in nuclear bomb, its back body sets gate, back body is connected with rear body, fuselage sets latch with the joint of rear body, in latch is located at cooling air compressor room and joint outer end, its compressor room rear end connects three-dimensional water railway carriage or compartment, rear end, water railway carriage or compartment connects blocking-up insulated space, rear body end sets gas-cooled nuclear reactor, its reactor surrounding sets all around cold air road, its fuselage rearmost end connects the tail wing and steam vent, the launching tube front end of its front fuselage sets block.

Beneficial effects of the present invention:

The nuclear power of bomber promotes the turbine of electromotor, making electromotor fast turn-around, promote bomber oceangoing voyage, speed increases several times, in the case of non-refuelling, a few hours can fly to continental United States overhead, carrying out core bombing, the aircraft carrier group to the U.S. has bigger lethality, a small-sized nuclear bomb simultaneously, all of for aircraft carrier group naval vessels can be sunk by bombing, there is this bomber, my South Sea, the evil neighbour in the East Sea are played deterrent effect, then dare not be recklessly acted easily；nullThis bomber is can the flight a few days under the thrust of nuclear reactor，Described gas-cooled nuclear reactor，Its external skin temperatures is high，Cabin kernel warhead detonation can be caused，In order to safety should be located at bomber afterbody gas-cooled nuclear reactor，It is equipped with cold air compressor room in rear body front end、Three-dimensional water railway carriage or compartment、Block insulated space，It is all to intercept、Block and eliminate the appearance high temperature of the quasi-nuclear reactor of gas and the efficient apparatus that makes，The surrounding of its nuclear reactor sets all around cold air road，The cold air making cooling air compressor passes through，Its cold air road is high 2 meters，Top caping sets bilayer，Can logical cold air，Its nuclear reactor base lower end sets multiple longitudinal cold duct，Reduce the high temperature of nuclear reactor lower end，Its pipeline connects 4 girder steels of lower end，The two ends of girder steel are fixed on the steel plate at rear body two ends，Its beam is whole holds gas-cooled nuclear reactor firmly，Make reactor exposed in centre，Its reactor can fill 7.5m³Nuclear fuel, weighs about 10 tons, if the promotion bomber oceangoing voyage that gas-cooled reactor uses pneumatic type is bombed, its speed is faster.

nullDescribed latch is to be located at inside and outside cooling air compressor room，With fuselage and rear body joint，Fuselage and rear body are self-existent，When the front end of rear body being inserted in the rear end of fuselage，Multiple upper and lower cotter joint hole is respectively set at two ends, joint left and right，It is enclosed within latch with strength tensioning spring，Compressing tensioning spring，Make latch pass inside pin hole and expose hole for nailing，Then pin is injected in latch hole for nailing，Two fuselages are made to combine firmly，Become an overall bomber，Just in case the nuclear reactor on bomber is hit by guided missile，Nuclear warhead blast in entail dangers to cabin and the safety of pilot，Now pilot presses push button (because push button is energized on 4 pins) moment，Moment pulls off pin，This latch is pulled out under the tension force of tensioning spring，Its rear body departs from fuselage immediately，Got rid of with nuclear reactor together with rear body，Guarantee pilot、Bomber and the safety of nuclear warhead，This nuclear reactor plant，It is equally applicable to unmanned machine，Described block can reduce air drag.

Accompanying drawing illustrates:

Below in conjunction with accompanying drawing embodiment, the invention will be further described.

Fig. 1, present configuration schematic diagram.

In figure, 1, head；2, fuselage；3, abdominal part nuclear bomb launching tube；4, short limb；5, balance wing；6, back nuclear bomb launching tube；7, gate；8, joint；9, latch；10, cooling air compressor room；11, three-dimensional water railway carriage or compartment；12, rear body；13, insulated space is blocked；14, all around cold air road；15, base；16, the tail wing；17, gas-cooled nuclear reactor；18, exhaust valve；19, block.

Specific embodiments:

Fig. 1, head 1 (inside setting turbogenerator) is connected with fuselage 2；Fuselage abdomen back of the body two ends connect abdominal part nuclear bomb launching tube 3, fuselage two ends connect short limb 4, short limb two ends connect balance wing 5, fuselage back sets nuclear bomb launching tube 6, rear end sets gate 7, the joint 8 that back body crosses with rear body 12 front end is connected, latch 9 firmly pins the joint 8 of fuselage and rear body, its joint rear end is equipped with cold air compressor room 10, its rear end, room connects three-dimensional water tank 11, its rear end, railway carriage or compartment connects blocking-up insulated space 13, rear body 12 end sets gas-cooled nuclear reactor 17, nuclear reactor surrounding sets all around cold air road 14, nuclear reactor lower end connects base 15, rear body end connects the tail wing 16, tail sets twice steam vent 17, block 18 is located at nuclear bomb launching tube front end, reduce the resistance of air.

Claims

1. a manufacture device for nuclear-powered bomber, including head, fuselage, abdominal part launching tube, Balance wing, rear body, cooling air compressor room, three-dimensional water railway carriage or compartment, all around cold air road, block every Heat space, gas-cooled nuclear reactor, air cooling pipeline, latch, is characterized in that head installs propeller for turboprop Machine, fuselage and balance wing can fill extension nuclear warhead, described rear body, install cooling air compressor Room, three-dimensional water railway carriage or compartment, all around cold air road, latch, it is characterized in that to block and eliminating its reactor Appearance heat energy；Described latch, it is characterised in that nuclear reactor is dangerous to be existed, and pilot presses Galvanic electricity button, latch is departing from pin, under the tension force of tensioning spring, makes fuselage separate with rear body, Ensure that fuselage nuclear warhead is perfectly safe.

The most according to claim 1, a kind of nuclear-powered bomber manufactures device, it is characterized in that system The cold air of cold air compressor room, can block and eliminate the outer exterior heat of gas-cooled nuclear reactor brave.

The most according to claim 1, a kind of nuclear-powered bomber manufactures device, it is characterized in that inserting Pin is when nuclear reactor is by projectile impacts, and pilot presses push button moment, makes fuselage fast with rear body Speed separates, and gets rid of nuclear reactor, it is ensured that nuclear warhead and driver, the safety of bomber in fuselage.

The most according to claim 1, a kind of nuclear-powered bomber manufactures device, it is characterized in that setting There is powerful core motive force at rear body afterbody gas-cooled nuclear reactor, make the flight oceangoing voyage of bomber a few days Bomb.

The most according to claim 1, a kind of nuclear-powered bomber malting apparatus, it is characterized in that four Enclose cold air road and air cooling pipeline, major part gas-cooled nuclear reactor appearance heat energy can be eliminated, it is ensured that rear machine Body safety.