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RU2077152C1 - AIRCRAFT - Google Patents

AIRCRAFT Download PDF

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Publication number
RU2077152C1
RU2077152C1 RU94015239/11A RU94015239A RU2077152C1 RU 2077152 C1 RU2077152 C1 RU 2077152C1 RU 94015239/11 A RU94015239/11 A RU 94015239/11A RU 94015239 A RU94015239 A RU 94015239A RU 2077152 C1 RU2077152 C1 RU 2077152C1
Authority
RU
Russia
Prior art keywords
engine
nacelle
fuselage
air intake
main wing
Prior art date
Application number
RU94015239/11A
Other languages
Russian (ru)
Other versions
RU94015239A (en
Inventor
А.В. Антонов
С.А. Богатиков
С.В. Костиков
О.А. Щелкунов
Original Assignee
Авиационный научно-технический комплекс им.А.Н.Туполева
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 Авиационный научно-технический комплекс им.А.Н.Туполева filed Critical Авиационный научно-технический комплекс им.А.Н.Туполева
Priority to RU94015239/11A priority Critical patent/RU2077152C1/en
Publication of RU94015239A publication Critical patent/RU94015239A/en
Application granted granted Critical
Publication of RU2077152C1 publication Critical patent/RU2077152C1/en

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Abstract

Самолет, содержащий фюзеляж, убираемое шасси, хвостовое оперение, основное и переднее крылья, соединенные между собой гондолами, расположенными по бокам от фюзеляжа, в каждой из которых размещен двигатель с воздушным винтом и воздухозаборником, отличающийся тем, что основное крыло расположено снизу фюзеляжа, двигатель содержит воздушный винт толкающего типа и размещен в задней части гондолы, при этом перед двигателем упомянутая гондола имеет криогенный топливный бак, причем гондола соединена с основным крылом вертикальным пилоном, внутри которого размещены ниша шасси и воздухозаборник двигателя.Aircraft containing the fuselage, retractable landing gear, tail, main and front wings, interconnected by nacelles located on the sides of the fuselage, in each of which there is an engine with a propeller and an air intake, characterized in that the main wing is located below the fuselage, engine contains a pusher type propeller and is located in the rear of the nacelle, while the nacelle in front of the engine has a cryogenic fuel tank, the nacelle being connected to the main wing by a vertical pylon, inside In which are located the chassis niche and the engine air intake.

RU94015239/11A 1994-04-26 1994-04-26 AIRCRAFT RU2077152C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94015239/11A RU2077152C1 (en) 1994-04-26 1994-04-26 AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94015239/11A RU2077152C1 (en) 1994-04-26 1994-04-26 AIRCRAFT

Publications (2)

Publication Number Publication Date
RU94015239A RU94015239A (en) 1996-05-10
RU2077152C1 true RU2077152C1 (en) 1997-04-10

Family

ID=48434718

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94015239/11A RU2077152C1 (en) 1994-04-26 1994-04-26 AIRCRAFT

Country Status (1)

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RU (1) RU2077152C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2563096C1 (en) * 2014-08-25 2015-09-20 Юлия Алексеевна Щепочкина Amphibious craft

Also Published As

Publication number Publication date
RU94015239A (en) 1996-05-10

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