RU2015124779A - CARGO COMPARTMENT OF THE AIRCRAFT - Google Patents

CARGO COMPARTMENT OF THE AIRCRAFT Download PDF

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Publication number
RU2015124779A
RU2015124779A RU2015124779A RU2015124779A RU2015124779A RU 2015124779 A RU2015124779 A RU 2015124779A RU 2015124779 A RU2015124779 A RU 2015124779A RU 2015124779 A RU2015124779 A RU 2015124779A RU 2015124779 A RU2015124779 A RU 2015124779A
Authority
RU
Russia
Prior art keywords
cargo
aircraft
cargo compartment
fuselage
niche
Prior art date
Application number
RU2015124779A
Other languages
Russian (ru)
Other versions
RU2614871C2 (en
Inventor
Александр Николаевич Давиденко
Михаил Юрьевич Стрелец
Юрий Георгиевич Поляков
Владимир Александрович Рунишев
Сергей Юрьевич Бибиков
Кирилл Евгеньевич Алферов
Валерий Черменович Каиров
Original Assignee
Публичное акционерное общество "Авиационная холдинговая компания "Сухой"
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 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" filed Critical Публичное акционерное общество "Авиационная холдинговая компания "Сухой"
Priority to RU2015124779A priority Critical patent/RU2614871C2/en
Publication of RU2015124779A publication Critical patent/RU2015124779A/en
Application granted granted Critical
Publication of RU2614871C2 publication Critical patent/RU2614871C2/en

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Claims (1)

Грузовой отсек самолета, представляющий собой нишу, содержащую выводное пусковое устройство, отличающийся тем, что ниша грузового отсека выполнена в зоне стыка наплыва фюзеляжа с консолью крыла, при этом ниша грузового отсека снабжена в нижней части обтекателем, содержащим, по меньшей мере, одну створку, а выводное пусковое устройство представляет собой рычажный механизм, обеспечивающий уборку и выпуск груза в плоскости, лежащей под острым углом в пределах от 20 до 70° к плоскости симметрии самолета, таким образом, что в выпущенном положении головная часть груза расположена перед передней кромкой крыла для уменьшения зоны «затенения» груза от носовой части фюзеляжа и передней кромки наплыва фюзеляжа, а продольная ось груза удалена от входа в воздухозаборник.The cargo compartment of the aircraft, which is a niche containing an output launching device, characterized in that the niche of the cargo compartment is made in the area of the junction of the influx of the fuselage with the wing console, while the niche of the cargo compartment is provided in the lower part with a fairing containing at least one wing, and the output launching device is a lever mechanism for cleaning and releasing the cargo in a plane lying at an acute angle in the range from 20 to 70 ° to the plane of symmetry of the aircraft, so that in the released position and the head part of the cargo is located in front of the front edge of the wing to reduce the zone of "shadowing" of the cargo from the nose of the fuselage and the front edge of the influx of the fuselage, and the longitudinal axis of the cargo is removed from the entrance to the air intake.
RU2015124779A 2015-06-24 2015-06-24 Aircraft cargo compartment RU2614871C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015124779A RU2614871C2 (en) 2015-06-24 2015-06-24 Aircraft cargo compartment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015124779A RU2614871C2 (en) 2015-06-24 2015-06-24 Aircraft cargo compartment

Publications (2)

Publication Number Publication Date
RU2015124779A true RU2015124779A (en) 2017-01-10
RU2614871C2 RU2614871C2 (en) 2017-03-30

Family

ID=57955540

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015124779A RU2614871C2 (en) 2015-06-24 2015-06-24 Aircraft cargo compartment

Country Status (1)

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RU (1) RU2614871C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2672706C1 (en) * 2017-10-06 2018-11-19 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Device for separating unmanned aerial vehicles from carrier aircraft
RU182345U1 (en) * 2017-10-06 2018-08-15 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" A device for separating a group of unmanned aerial vehicles from a carrier aircraft
RU2664812C1 (en) * 2017-10-06 2018-08-22 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Method of separation of the group of unmanned aerial vehicles from the aircraft planer

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2099240C1 (en) * 1995-02-16 1997-12-20 Авиационный комплекс им.С.В.Ильюшина Cargo compartment of flying vehicle
US6394392B1 (en) * 1999-10-19 2002-05-28 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
ES2282624T3 (en) * 2002-03-11 2007-10-16 Telair International Ab SYSTEM FOR THE LOADING AND UNLOADING OF GOODS IN A CARGO WAREHOUSE SPECIALLY OF AN AIRPLANE, AS WELL AS A DEVICE FOR INTERMEDIATE TRANSPORTATION OR TRANSPORT UNIT FOR THE SAME.
DE10343627B4 (en) * 2003-09-20 2014-03-06 Eads Deutschland Gmbh Closure element for an area of the outer skin of an aircraft
RU2263611C2 (en) * 2003-10-02 2005-11-10 Научно-исследовательский институт специального машиностроения Московского технического университета им. Н.Э. Баумана Aircraft complex

Also Published As

Publication number Publication date
RU2614871C2 (en) 2017-03-30

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20180625

NF4A Reinstatement of patent

Effective date: 20190827