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SU1637169A1 - Створка капота летательного аппарата - Google Patents

Створка капота летательного аппарата

Info

Publication number
SU1637169A1
SU1637169A1 SU4765057/23A SU4765057A SU1637169A1 SU 1637169 A1 SU1637169 A1 SU 1637169A1 SU 4765057/23 A SU4765057/23 A SU 4765057/23A SU 4765057 A SU4765057 A SU 4765057A SU 1637169 A1 SU1637169 A1 SU 1637169A1
Authority
SU
USSR - Soviet Union
Prior art keywords
cowling
section
aircraft
flap
bushings
Prior art date
Application number
SU4765057/23A
Other languages
English (en)
Inventor
А.Л. Доброскоков
Г.В. Степанов
И.В. Козлов
Original Assignee
А.Л. Доброскоков
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.Л. Доброскоков filed Critical А.Л. Доброскоков
Priority to SU4765057/23A priority Critical patent/SU1637169A1/ru
Application granted granted Critical
Publication of SU1637169A1 publication Critical patent/SU1637169A1/ru

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Insulators (AREA)

Abstract

Изобретение относится к авиастроению, в частности к конструкции капотных створок, снабженных устройствами для их заземления (металлизации). Цель изобретения - упрощение изготовления панели, повышение ее прочности и снижение веса. Обшивки створки капота соединены между собой окантовывающим профилем 8 и втулками 9. Головки втулок 9 размещены в зенковках 13, выполненных в полках профиля 8 и в обшивках и контактируют с торцами угольных волокон 10, обеспечивая передачу заряда на профиль и с нее через перемычку на пилон. 5 ил.
SU4765057/23A 1989-12-05 1989-12-05 Створка капота летательного аппарата SU1637169A1 (ru)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4765057/23A SU1637169A1 (ru) 1989-12-05 1989-12-05 Створка капота летательного аппарата

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4765057/23A SU1637169A1 (ru) 1989-12-05 1989-12-05 Створка капота летательного аппарата

Publications (1)

Publication Number Publication Date
SU1637169A1 true SU1637169A1 (ru) 1994-12-15

Family

ID=60531738

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4765057/23A SU1637169A1 (ru) 1989-12-05 1989-12-05 Створка капота летательного аппарата

Country Status (1)

Country Link
SU (1) SU1637169A1 (ru)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2469922C2 (ru) * 2007-08-20 2012-12-20 Эрсель Гондола турбореактивного двигателя, содержащая демпферы для боковых крышек
RU2471678C2 (ru) * 2007-08-20 2013-01-10 Эрсель Соединительное устройство для соединения подвижных относительно друг друга первого и второго элементов

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2469922C2 (ru) * 2007-08-20 2012-12-20 Эрсель Гондола турбореактивного двигателя, содержащая демпферы для боковых крышек
RU2471678C2 (ru) * 2007-08-20 2013-01-10 Эрсель Соединительное устройство для соединения подвижных относительно друг друга первого и второго элементов

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