[go: up one dir, main page]

SU482976A1 - ENTRANCE DOOR OF AIRPLANE - Google Patents

ENTRANCE DOOR OF AIRPLANE

Info

Publication number
SU482976A1
SU482976A1 SU1896105/23A SU1896105A SU482976A1 SU 482976 A1 SU482976 A1 SU 482976A1 SU 1896105/23 A SU1896105/23 A SU 1896105/23A SU 1896105 A SU1896105 A SU 1896105A SU 482976 A1 SU482976 A1 SU 482976A1
Authority
SU
USSR - Soviet Union
Prior art keywords
airplane
entrance door
parallelogram
flap
fuselage
Prior art date
Application number
SU1896105/23A
Other languages
Russian (ru)
Inventor
А.С. Артамонов
В.Ф. Сергеев
Original Assignee
А.С. Артамонов
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 А.С. Артамонов filed Critical А.С. Артамонов
Priority to SU1896105/23A priority Critical patent/SU482976A1/en
Application granted granted Critical
Publication of SU482976A1 publication Critical patent/SU482976A1/en

Links

Landscapes

  • Body Structure For Vehicles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Vehicle Step Arrangements And Article Storage (AREA)

Abstract

Входная дверь самолета, содержащая створку, соединенную параллелограммным механизмом с кареткой, установленной на направляющих, прикрепленных к борту фюзеляжа, отличающаяся тем, что, с целью обеспечения открытия двери при действии усилия, направленного изнутри фюзеляжа, на каретке перед створкой на расстоянии ее входа на параллелограммном механизме жестко закреплен щиток, например панель с сотовым наполнителем.The front door of the aircraft, containing a flap connected by a parallelogram mechanism with a carriage mounted on guides attached to the fuselage side, characterized in that, in order to ensure the opening of the door under the action of the force directed from inside the fuselage, on the carriage in front of the flap at its entrance to the parallelogram the mechanism is rigidly fixed shield, for example, a panel with a honeycomb filler.

SU1896105/23A 1973-03-23 1973-03-23 ENTRANCE DOOR OF AIRPLANE SU482976A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1896105/23A SU482976A1 (en) 1973-03-23 1973-03-23 ENTRANCE DOOR OF AIRPLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1896105/23A SU482976A1 (en) 1973-03-23 1973-03-23 ENTRANCE DOOR OF AIRPLANE

Publications (1)

Publication Number Publication Date
SU482976A1 true SU482976A1 (en) 2004-11-20

Family

ID=60517074

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1896105/23A SU482976A1 (en) 1973-03-23 1973-03-23 ENTRANCE DOOR OF AIRPLANE

Country Status (1)

Country Link
SU (1) SU482976A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2532010C2 (en) * 2009-06-29 2014-10-27 Эрбюс Операсьон Сас Frame of opening made in aircraft fuselage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2532010C2 (en) * 2009-06-29 2014-10-27 Эрбюс Операсьон Сас Frame of opening made in aircraft fuselage

Similar Documents

Publication Publication Date Title
US4245804B1 (en) Minimum drag wing configuration for aircraft operating at transonic speeds
GB1070723A (en) Improvements in or relating to aircraft
SU482976A1 (en) ENTRANCE DOOR OF AIRPLANE
GB1547903A (en) Mounting mechanism for an airplane wing trailing-edge flaps
GB785633A (en) Improvements in aircraft having a variable wing area
SU516230A1 (en) Transport aeroplane hatch cover
SU369053A1 (en) MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT
GB767043A (en) Improvements relating to bomb doors for aircraft
SU325201A1 (en) MECHANISM OF DEFLECTOR CONTROL OF AN AIRCRAFT LOCK
CA638844A (en) Spoiler for aircraft wings
SU774092A1 (en) SCANOLET-ARTEMOVA
SU516229A1 (en) Device for control of flying vehicle hatch cover
CA840848A (en) Cross ducting system for augmentor wing aircraft
CA642844A (en) Apparatus for computing aircraft position with respect to flight tracks
SU578711A1 (en) HATCH FRONT RACK CHASSIS OF AIRCRAFT
CA813726A (en) Curved wing structure for aircraft
GB1369609A (en) Aircraft wing with one or more one part or multi part flaps
SU624418A1 (en) MECHANISM OF MANAGEMENT OF DOUBLE-CHARGERS OF THE AIRCRAFT
ES347453A1 (en) An elevator device. (Machine-translation by Google Translate, not legally binding)
SU296387A1 (en) DEVICE FRONT FACILITY OF AIRCRAFT
FR87692E (en) Improvements to liftable landing gear, particularly in an aircraft fuselage
CA690680A (en) Wing fan doors for aircraft
CA769578A (en) Aircraft high-lift wing
CA694794A (en) Inlet for vertical take-off aircraft
AU272613B2 (en) Rotary wing aircraft pylon mounting