[go: up one dir, main page]

RU2000105579A - METHOD FOR PLACING ON THE FLIGHT PROTECTOR OF THE PROTECTIVE ONBOARD STORAGE - Google Patents

METHOD FOR PLACING ON THE FLIGHT PROTECTOR OF THE PROTECTIVE ONBOARD STORAGE

Info

Publication number
RU2000105579A
RU2000105579A RU2000105579/28A RU2000105579A RU2000105579A RU 2000105579 A RU2000105579 A RU 2000105579A RU 2000105579/28 A RU2000105579/28 A RU 2000105579/28A RU 2000105579 A RU2000105579 A RU 2000105579A RU 2000105579 A RU2000105579 A RU 2000105579A
Authority
RU
Russia
Prior art keywords
flight
placing
protective
aircraft
protector
Prior art date
Application number
RU2000105579/28A
Other languages
Russian (ru)
Other versions
RU2206477C2 (en
Inventor
Юрий Васильевич Попов
Original Assignee
в/ч 75360
Filing date
Publication date
Application filed by в/ч 75360 filed Critical в/ч 75360
Priority to RU2000105579/28A priority Critical patent/RU2206477C2/en
Priority claimed from RU2000105579/28A external-priority patent/RU2206477C2/en
Publication of RU2000105579A publication Critical patent/RU2000105579A/en
Application granted granted Critical
Publication of RU2206477C2 publication Critical patent/RU2206477C2/en

Links

Claims (1)

Способ размещения на летательном аппарате защитного бортового накопителя, у которого приемная и подающаяся катушки располагаются одна возле другой по полету, в хвостовой части фюзеляжа отличается тем, что, с целью повышения сохранности зарегистрированной информации при авиационном происшествии защитный бортовой накопитель устанавливается так, чтобы транспортирование магнитного носителя осуществлялось перпендикулярно строительной оси летательного аппарата и на безопасное расстояние от центра масс летательного аппарата, выбранном в соответствии с отношением
Figure 00000001
,
где Sкp = 0,7l(12 + d) при l≤20 м;
Sкp = 0,7l(30 + d) при l>20 м;
l - длина летательного аппарата;
d - диаметра меделевого сечения фюзеляжа.
The method of placing a protective drive on board the aircraft, in which the receiving and feeding coils are located next to each other in flight, in the rear part of the fuselage is characterized in that, in order to increase the safety of the recorded information during an accident, the protective drive is installed so that the magnetic carrier is transported was carried out perpendicular to the aircraft building axis and to a safe distance from the center of mass of the aircraft selected according to attitude
Figure 00000001
,
where S kp = 0.7l (12 + d) at l≤20 m;
S cr = 0.7l (30 + d) for l> 20 m;
l is the length of the aircraft;
d is the diameter of the copper section of the fuselage.
RU2000105579/28A 2000-03-10 2000-03-10 Method of mounting protective on-board storage on flying vehicle RU2206477C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000105579/28A RU2206477C2 (en) 2000-03-10 2000-03-10 Method of mounting protective on-board storage on flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000105579/28A RU2206477C2 (en) 2000-03-10 2000-03-10 Method of mounting protective on-board storage on flying vehicle

Publications (2)

Publication Number Publication Date
RU2000105579A true RU2000105579A (en) 2002-01-27
RU2206477C2 RU2206477C2 (en) 2003-06-20

Family

ID=29208961

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000105579/28A RU2206477C2 (en) 2000-03-10 2000-03-10 Method of mounting protective on-board storage on flying vehicle

Country Status (1)

Country Link
RU (1) RU2206477C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2308929C2 (en) * 2005-09-07 2007-10-27 Федеральное государственное унитарное предприятие "Государственный ракетный центр "КБ им. акад. В.П. Макеева" Method for a patient's body extension

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2170383A (en) * 1937-03-23 1939-08-22 Charles R Kines Aircraft recording means
RU1764447C (en) * 1989-12-22 1994-08-15 Санкт-Петербургский опытный завод "Прибор" Tape drive
JPH07115677B2 (en) * 1990-10-30 1995-12-13 嘉三 藤本 Flight information recording method and apparatus for aircraft
RU2125238C1 (en) * 1997-03-19 1999-01-20 Открытое конструкторское бюро "Авиаавтоматика" Акционерного общества "Прибор" Data registration system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2308929C2 (en) * 2005-09-07 2007-10-27 Федеральное государственное унитарное предприятие "Государственный ракетный центр "КБ им. акад. В.П. Макеева" Method for a patient's body extension

Similar Documents

Publication Publication Date Title
GB2255758B (en) Flight information recording method and device for aircraft.
IL102653A0 (en) Shroud geometry of unmanned aerial vehicles
EP0907087A3 (en) Underwater cable arrangement
IT8424116A0 (en) COOLING SYSTEM FOR GAS TURBO ENGINE COMPONENTS.
DE69100695D1 (en) Hold-down system for expandable elements on a spacecraft.
RU2000105579A (en) METHOD FOR PLACING ON THE FLIGHT PROTECTOR OF THE PROTECTIVE ONBOARD STORAGE
DE3688646D1 (en) MAGNETIC HEAD FROM AN AMORPHOUS MAGNETIC ALLOY AND METHOD FOR PRODUCING THE SAME.
DK1783A (en) KINETIC ENERGY RECOVERY APPARATUS FROM A MOTOR VEHICLE UNDER BRAKING AND RECYCLING OF THIS ENERGY DURING ACCELERATION
IT8423422A0 (en) SETTING SYSTEM FOR GUIDED AIRCRAFT, FLYING AT SUPERSONIC SPEED.
IL139496A0 (en) Method and system for feeding a cool air inlet of the cabin of an aircraft propelled by at least one jet engine
EP0124133A3 (en) Storing system for trailing antennas, especially for submarines
RU2206477C2 (en) Method of mounting protective on-board storage on flying vehicle
JPS5725030A (en) Intersubsystem communication system
IT8324209A0 (en) CONTROL SYSTEM FOR AIRCRAFT GAS TURBO ENGINES.
DE3373034D1 (en) Justifying with printer level data stream which accommodates footers and headers
Stein Human factors analyzed in 007 navigation error.
JPH07277298A (en) Spacecraft protection device
Bolhofer et al. Summer MONEX US research flight missions, May- July 1979
ES528520A0 (en) AN IMPROVED METHOD FOR RECOVERING SUCROSA FROM AQUEOUS SOLUTIONS THAT CONTAIN IT.
Hrbud Nuclear and future flight propulsion.
EP1416299A3 (en) Coil support device for an underwater cable
VERMEULEN et al. Review of AIDS development(airborne computers for reliability engineering)
ES514546A0 (en) FLYING AERODYNAMIC TRAIL TRAIN.
CREWS Low gravity flight complement data[Final Report]
Reeves CNA's(Center for Naval Analyses) conceptual design and cost models for high-speed surface craft.