SU622956A1 - Hangar - Google Patents

Hangar

Info

Publication number
SU622956A1
SU622956A1 SU772454700A SU2454700A SU622956A1 SU 622956 A1 SU622956 A1 SU 622956A1 SU 772454700 A SU772454700 A SU 772454700A SU 2454700 A SU2454700 A SU 2454700A SU 622956 A1 SU622956 A1 SU 622956A1
Authority
SU
USSR - Soviet Union
Prior art keywords
hangar
elements
base element
formula
base
Prior art date
Application number
SU772454700A
Other languages
Russian (ru)
Inventor
Геннадий Георгиевич Болдин
Олег Альбинович Виксво
Original Assignee
Ленинградский Филиал Государственного Проектно-Изыскательского Научно-Исследовательского Института Гражданской Авиации "Аэропроект"
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 Ленинградский Филиал Государственного Проектно-Изыскательского Научно-Исследовательского Института Гражданской Авиации "Аэропроект" filed Critical Ленинградский Филиал Государственного Проектно-Изыскательского Научно-Исследовательского Института Гражданской Авиации "Аэропроект"
Priority to SU772454700A priority Critical patent/SU622956A1/en
Application granted granted Critical
Publication of SU622956A1 publication Critical patent/SU622956A1/en

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Landscapes

  • Hinges (AREA)
  • Hinge Accessories (AREA)

Description

(54) АНГАР(54) HANGAR

Формула иэовретени Formula formula

Ангар у включгйющий основание и корпус , в котором один из, элементов шарнирно прикреплен к элементу основанид, а остальные - жестко, отличающийс  тем, что, с целью унификации конструкции элементы выполнены треугольными, причем элементы корпуса размещены наклонно и соединены между собой боковыми гран ми, а нижними - с гран ми элемента основани .The hangar includes a base and a body in which one of the elements is hingedly attached to the base element, and the rest are rigid, characterized in that, in order to unify the design, the elements are made triangular, with the body elements placed obliquely and interconnected by side faces and the lower ones, with the edges of the base element.

Источники информации, прин тые во внимание при экспертизе:Sources of information taken into account in the examination:

1.Патент США № 3,229,649, кл. 109-1, 1966.1. US Patent No. 3,229,649, cl. 109-1, 1966.

2.Патент Великобритании №1425758, кло Е 04 Н 6/34, 1976.2. The patent of Great Britain No. 1425758, CLO 04 H 6/34, 1976.

Рш. 1Rsh. one

SU772454700A 1977-02-18 1977-02-18 Hangar SU622956A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU772454700A SU622956A1 (en) 1977-02-18 1977-02-18 Hangar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU772454700A SU622956A1 (en) 1977-02-18 1977-02-18 Hangar

Publications (1)

Publication Number Publication Date
SU622956A1 true SU622956A1 (en) 1978-09-05

Family

ID=20696366

Family Applications (1)

Application Number Title Priority Date Filing Date
SU772454700A SU622956A1 (en) 1977-02-18 1977-02-18 Hangar

Country Status (1)

Country Link
SU (1) SU622956A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2244300A (en) * 1990-05-25 1991-11-27 Stephen Paul Taylor Aircraft hanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2244300A (en) * 1990-05-25 1991-11-27 Stephen Paul Taylor Aircraft hanger

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