RU2015117336A - Airship early warning radar - Google Patents

Airship early warning radar Download PDF

Info

Publication number
RU2015117336A
RU2015117336A RU2015117336A RU2015117336A RU2015117336A RU 2015117336 A RU2015117336 A RU 2015117336A RU 2015117336 A RU2015117336 A RU 2015117336A RU 2015117336 A RU2015117336 A RU 2015117336A RU 2015117336 A RU2015117336 A RU 2015117336A
Authority
RU
Russia
Prior art keywords
shell
nacelle
airborne
early warning
airship
Prior art date
Application number
RU2015117336A
Other languages
Russian (ru)
Other versions
RU2604914C2 (en
Inventor
Александр Александрович Неудакин
Андрей Сергеевич Артюх
Константин Анатольевич Малугин
Original Assignee
Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации
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 Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации filed Critical Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации
Priority to RU2015117336/11A priority Critical patent/RU2604914C2/en
Publication of RU2015117336A publication Critical patent/RU2015117336A/en
Application granted granted Critical
Publication of RU2604914C2 publication Critical patent/RU2604914C2/en

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/22—Arrangement of cabins or gondolas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/10—Stowage arrangements for the devices in aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Aerials (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

Дирижабль дальнего радиолокационного обнаружения, состоящий из оболочки, гондолы, двигателя, винта и бортовой РЛС, установленной в гондоле, отличающийся тем, что антенная система бортовой РЛС выполнена в виде активной фазированной антенной решетки, приемопередающие модули и распределительная система питания которой вмонтированы в материал оболочки дирижабля на одной из его боковых сторон, а на противоположной стороне оболочки нанесена контрольная разметка, в упомянутой гондоле размещены стартовая площадка для беспилотного летательного аппарата, система слежения и канал управления упомянутым летательным аппаратом, который оснащен двумя слабонаправленными излучателями.An airborne early warning radar, consisting of a shell, a nacelle, an engine, a propeller and an airborne radar installed in a nacelle, characterized in that the airborne radar antenna system is made in the form of an active phased antenna array, the transmit-receive modules and the power distribution system of which are mounted in the airship shell material on one of its sides, and on the opposite side of the shell, control markings are applied, the launch pad for an unmanned aerial vehicle is placed in the said gondola of the apparatus, the tracking system and the control channel of said aircraft, which is equipped with two weakly directed emitters.

Claims (1)

Дирижабль дальнего радиолокационного обнаружения, состоящий из оболочки, гондолы, двигателя, винта и бортовой РЛС, установленной в гондоле, отличающийся тем, что антенная система бортовой РЛС выполнена в виде активной фазированной антенной решетки, приемопередающие модули и распределительная система питания которой вмонтированы в материал оболочки дирижабля на одной из его боковых сторон, а на противоположной стороне оболочки нанесена контрольная разметка, в упомянутой гондоле размещены стартовая площадка для беспилотного летательного аппарата, система слежения и канал управления упомянутым летательным аппаратом, который оснащен двумя слабонаправленными излучателями. An airborne early warning radar, consisting of a shell, a nacelle, an engine, a propeller and an airborne radar installed in a nacelle, characterized in that the airborne radar antenna system is made in the form of an active phased antenna array, the transmit-receive modules and the power distribution system of which are mounted in the airship shell material on one of its sides, and on the opposite side of the shell, control markings are applied, the launch pad for an unmanned aerial vehicle is placed in the said gondola of the apparatus, the tracking system and the control channel of said aircraft, which is equipped with two weakly directed emitters.
RU2015117336/11A 2015-05-06 2015-05-06 Airborne early warning airship RU2604914C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015117336/11A RU2604914C2 (en) 2015-05-06 2015-05-06 Airborne early warning airship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015117336/11A RU2604914C2 (en) 2015-05-06 2015-05-06 Airborne early warning airship

Publications (2)

Publication Number Publication Date
RU2015117336A true RU2015117336A (en) 2016-11-27
RU2604914C2 RU2604914C2 (en) 2016-12-20

Family

ID=57758912

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015117336/11A RU2604914C2 (en) 2015-05-06 2015-05-06 Airborne early warning airship

Country Status (1)

Country Link
RU (1) RU2604914C2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107031808A (en) * 2017-04-19 2017-08-11 中国科学院光电研究院 System and method based near space stratospheric airship electromagnetic launch unmanned plane
PL422647A1 (en) * 2017-08-25 2019-03-11 Advanced Protection Systems Spółka Z Ograniczoną Odpowiedzialnością Miniaturized radar sensor to be mounted on drones, intended for the assistance in landing and detecting other drones in the airspace

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2652512C1 (en) * 2017-02-21 2018-04-26 Акционерное общество "ЗАСЛОН" Method of tethering balloon circular view radar constructing
CN106976544A (en) * 2017-03-03 2017-07-25 南京航空航天大学 A kind of airship gondola structure
CN108539849A (en) * 2018-05-16 2018-09-14 中国科学院光电研究院 A kind of intelligent power distribution management module and stratospheric airship distributor
RU2721642C1 (en) * 2019-10-24 2020-05-21 Владимир Иванович Михайленко Method for long-range detection of aircrafts
US11073362B1 (en) 2020-08-24 2021-07-27 King Abdulaziz University Distributed airborne acoustic anti drone system (DAAADS)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0715220A (en) * 1993-06-23 1995-01-17 Mitsubishi Heavy Ind Ltd Airship for air patrol
RU2182544C2 (en) * 2000-04-18 2002-05-20 Государственное предприятие Научно-исследовательский институт радиоприборостроения Radar scanning aerostat
JP2011171803A (en) * 2010-02-16 2011-09-01 Mitsubishi Electric Corp Antenna device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107031808A (en) * 2017-04-19 2017-08-11 中国科学院光电研究院 System and method based near space stratospheric airship electromagnetic launch unmanned plane
PL422647A1 (en) * 2017-08-25 2019-03-11 Advanced Protection Systems Spółka Z Ograniczoną Odpowiedzialnością Miniaturized radar sensor to be mounted on drones, intended for the assistance in landing and detecting other drones in the airspace

Also Published As

Publication number Publication date
RU2604914C2 (en) 2016-12-20

Similar Documents

Publication Publication Date Title
RU2015117336A (en) Airship early warning radar
MX2018014569A (en) Radar system to track low flying unmanned aerial vehicles and objects.
EP4279395A3 (en) System and method for damping oscillations of a payload
WO2017200896A3 (en) A dynamically steered lidar adapted to vehicle shape
WO2015193433A3 (en) Micro assembled high frequency devices and arrays and method of making the same
RU2016148222A (en) DEVICE AND METHOD FOR COMMUNICATION AIR-EARTH AIRCRAFT
BR112015000756A2 (en) method of orienting a satellite antenna; and satellite antenna pointing system
CN106537823A8 (en) Offer using fixed satellite service to the broadband access of airborne platform and ground based terminal
MX2016014041A (en) Vehicle phased array antenna pattern generation.
EP2854305A3 (en) Interference suppression in a satellite communication system using onboard beamforming and ground-based processing
WO2019147196A3 (en) Autonomous unmanned aerial vehicle
GB201711537D0 (en) Systems and devices to control antenna azimuth orientation in an omni-directional unmanned aerial vehicle
JP2017028605A5 (en)
BR112019005263A2 (en) radar system, vessel and land vehicle
EP4071049A4 (en) Flight control system for unmanned aerial vehicle and geographical-feature measurement system
IL241025B (en) Patch antennas configuration for an unmanned aerial vehicle
WO2015040500A3 (en) Feed system for beam steerable circular antenna arrays
EA201600115A1 (en) LANDING RADAR
ES2547585B1 (en) AIR TRANSPORT SYSTEM FOR THE MEASUREMENT OF THE HUMIDITY OF THE LAND AND THE WATER CONTENT OF THE VEGETATION AND IMPLEMENTATION METHOD
RU2014107049A (en) SMALL-SIZED UNMANNED AIRCRAFT SUPPRESSION DEVICE
SA519402068B1 (en) Device for measuring the electromagnetic performance of a ground radar
KR20160149954A (en) the idea of the partial stealth facility of the airplane by plasma
RU2018146153A (en) The way to combat unmanned aerial vehicles using electromagnetic radiation
RU2013141499A (en) MILITARY ARMS DEVICE
UA104677U (en) The method of jamming radar and radar homing head missiles

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20170507