PL425188A1 - Thin-walled construction, preferably for the aircraft skins - Google Patents

Thin-walled construction, preferably for the aircraft skins

Info

Publication number
PL425188A1
PL425188A1 PL425188A PL42518818A PL425188A1 PL 425188 A1 PL425188 A1 PL 425188A1 PL 425188 A PL425188 A PL 425188A PL 42518818 A PL42518818 A PL 42518818A PL 425188 A1 PL425188 A1 PL 425188A1
Authority
PL
Poland
Prior art keywords
thin
walled construction
layer
aircraft skins
outer layer
Prior art date
Application number
PL425188A
Other languages
Polish (pl)
Inventor
Andrzej Kubit
Dawid Wydrzyński
Tomasz Trzepieciński
Original Assignee
Politechnika Rzeszowska im. Ignacego Łukasiewicza
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 Politechnika Rzeszowska im. Ignacego Łukasiewicza filed Critical Politechnika Rzeszowska im. Ignacego Łukasiewicza
Priority to PL425188A priority Critical patent/PL425188A1/en
Publication of PL425188A1 publication Critical patent/PL425188A1/en

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Abstract

Konstrukcja cienkościenna złożona jest z połączonych ze sobą warstwy wewnętrznej (1) i warstwy zewnętrznej (2). Warstwa wewnętrzna (1) ma ukształtowane przetłoczenia usztywniające (4). Przetłoczenia usztywniające (4) tworzą strukturę typu isogrid. Warstwa zewnętrzna (2) zawiera warstwę kompozytową (3), która jest ukształtowana z kompozytu polimerowo-włóknistego. Warstwa wewnętrzna (1) i warstwa zewnętrzna (2) są połączone adhezyjnie.The thin-walled structure is composed of interconnected inner layer (1) and outer layer (2). The inner layer (1) has shaped stiffening ribs (4). The stiffening ribs (4) form an isogrid structure. The outer layer (2) comprises a composite layer (3) which is formed of a polymer-fiber composite. The inner layer (1) and the outer layer (2) are adhesively bonded.

PL425188A 2018-04-11 2018-04-11 Thin-walled construction, preferably for the aircraft skins PL425188A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL425188A PL425188A1 (en) 2018-04-11 2018-04-11 Thin-walled construction, preferably for the aircraft skins

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL425188A PL425188A1 (en) 2018-04-11 2018-04-11 Thin-walled construction, preferably for the aircraft skins

Publications (1)

Publication Number Publication Date
PL425188A1 true PL425188A1 (en) 2019-10-21

Family

ID=68238617

Family Applications (1)

Application Number Title Priority Date Filing Date
PL425188A PL425188A1 (en) 2018-04-11 2018-04-11 Thin-walled construction, preferably for the aircraft skins

Country Status (1)

Country Link
PL (1) PL425188A1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140044914A1 (en) * 2011-05-02 2014-02-13 Didier Kurtz Self-stiffened composite panel particularly for aircraft floors and method for manufacturing the same
PL224527B1 (en) * 2012-12-05 2017-01-31 Inst Pojazdów Szynowych Tabor Multi-layer plate
US20170113777A1 (en) * 2015-10-22 2017-04-27 Airbus Defence and Space GmbH Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement
US20170274577A1 (en) * 2016-03-24 2017-09-28 The Boeing Company Composite structures with stiffeners and method of making the same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140044914A1 (en) * 2011-05-02 2014-02-13 Didier Kurtz Self-stiffened composite panel particularly for aircraft floors and method for manufacturing the same
PL224527B1 (en) * 2012-12-05 2017-01-31 Inst Pojazdów Szynowych Tabor Multi-layer plate
US20170113777A1 (en) * 2015-10-22 2017-04-27 Airbus Defence and Space GmbH Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement
US20170274577A1 (en) * 2016-03-24 2017-09-28 The Boeing Company Composite structures with stiffeners and method of making the same

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