RU2007116751A - Aerial bomb - Google Patents

Aerial bomb Download PDF

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Publication number
RU2007116751A
RU2007116751A RU2007116751/02A RU2007116751A RU2007116751A RU 2007116751 A RU2007116751 A RU 2007116751A RU 2007116751/02 A RU2007116751/02 A RU 2007116751/02A RU 2007116751 A RU2007116751 A RU 2007116751A RU 2007116751 A RU2007116751 A RU 2007116751A
Authority
RU
Russia
Prior art keywords
board computer
control
aircraft bomb
casing
bomb
Prior art date
Application number
RU2007116751/02A
Other languages
Russian (ru)
Other versions
RU2347178C1 (en
Inventor
Николай Борисович Болотин (RU)
Николай Борисович Болотин
Original Assignee
Николай Борисович Болотин (RU)
Николай Борисович Болотин
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 Николай Борисович Болотин (RU), Николай Борисович Болотин filed Critical Николай Борисович Болотин (RU)
Priority to RU2007116751/02A priority Critical patent/RU2347178C1/en
Publication of RU2007116751A publication Critical patent/RU2007116751A/en
Application granted granted Critical
Publication of RU2347178C1 publication Critical patent/RU2347178C1/en

Links

Claims (6)

1. Aircraft bomb containing an axisymmetric casing with four stabilizers, inside which an explosive device is installed, and a control system, characterized in that a fuel tank is installed inside the casing, four solid-propellant rocket engines in the rear of the casing along the periphery, and installed along the casing axis a liquid fuel gas turbine engine comprising an air intake, a compressor, a combustion chamber and a turbine, a fuel tank connected to a fuel pipe in which a fuel pump is installed with a pump drive, with a combustion chamber, and the control system contains a stabilizer drive and an on-board computer.
2. Aircraft bomb according to claim 1, characterized in that the control system has a control controller connected to the control drive on the one hand and to the on-board computer on the other.
3. Aircraft bomb according to claim 1 or 2, characterized in that the pump drive is connected to the engine controller, which, in turn, is connected to the on-board computer.
4. Aircraft bomb according to claim 1 or 2, characterized in that a transmitting and receiving device with an antenna is connected to the on-board computer.
5. Aircraft bomb according to claim 1 or 2, characterized in that it contains a global positioning system receiver connected to the antenna and to the on-board computer.
6. Aircraft bomb according to claim 1 or 2, characterized in that the on-board computer is connected to the fuse controller, connected, in turn, to the explosive device.
RU2007116751/02A 2007-05-03 2007-05-03 Air bomb RU2347178C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2007116751/02A RU2347178C1 (en) 2007-05-03 2007-05-03 Air bomb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2007116751/02A RU2347178C1 (en) 2007-05-03 2007-05-03 Air bomb

Publications (2)

Publication Number Publication Date
RU2007116751A true RU2007116751A (en) 2008-11-27
RU2347178C1 RU2347178C1 (en) 2009-02-20

Family

ID=40531862

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007116751/02A RU2347178C1 (en) 2007-05-03 2007-05-03 Air bomb

Country Status (1)

Country Link
RU (1) RU2347178C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2477449C1 (en) * 2011-07-15 2013-03-10 Николай Борисович Болотин Hydrogen bomb
RU2480706C2 (en) * 2011-07-15 2013-04-27 Николай Борисович Болотин Nuclear bomb
RU170644U1 (en) * 2016-06-09 2017-05-03 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" WING Rocket SATELLITE NAVIGATION SYSTEM

Also Published As

Publication number Publication date
RU2347178C1 (en) 2009-02-20

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