GB481406A - Improvements in fuel tanks for airplanes - Google Patents

Improvements in fuel tanks for airplanes

Info

Publication number
GB481406A
GB481406A GB21141/37A GB2114137A GB481406A GB 481406 A GB481406 A GB 481406A GB 21141/37 A GB21141/37 A GB 21141/37A GB 2114137 A GB2114137 A GB 2114137A GB 481406 A GB481406 A GB 481406A
Authority
GB
United Kingdom
Prior art keywords
partition
wall
airplanes
fuel tanks
secured
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB21141/37A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Breeze Corp Inc
Original Assignee
Breeze Corp Inc
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 Breeze Corp Inc filed Critical Breeze Corp Inc
Publication of GB481406A publication Critical patent/GB481406A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/06Constructional adaptations thereof
    • B64D37/08Internal partitioning

Abstract

481,406. Tanks. BREEZE CORPORATION, Inc. July 30, 1937, No. 21141. Convention date, Feb. 8. [Class 69 (i)] A fuel tank, particularly for aeroplanes, having a partition C secured at its edges to the wall A, is provided with a passage for the liquid past the partition, formed by a plate 5 secured to the outside of the wall and covering apertures 4 in the wall on each side of the partition. The partition and wall are shown connected by an interengaging bent rib and flange as described in Specification 481,329.
GB21141/37A 1937-02-08 1937-07-30 Improvements in fuel tanks for airplanes Expired GB481406A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US481406XA 1937-02-08 1937-02-08

Publications (1)

Publication Number Publication Date
GB481406A true GB481406A (en) 1938-03-10

Family

ID=21952944

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21141/37A Expired GB481406A (en) 1937-02-08 1937-07-30 Improvements in fuel tanks for airplanes

Country Status (1)

Country Link
GB (1) GB481406A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111976999A (en) * 2020-07-06 2020-11-24 西安飞机工业(集团)有限责任公司 Vibration reduction method for airplane soft oil tank
CN115636094A (en) * 2022-12-23 2023-01-24 西安远飞航空技术发展有限公司 Connecting structure of skin and partition plate, manufacturing method of connecting structure and aircraft oil tank

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111976999A (en) * 2020-07-06 2020-11-24 西安飞机工业(集团)有限责任公司 Vibration reduction method for airplane soft oil tank
CN111976999B (en) * 2020-07-06 2022-08-09 西安飞机工业(集团)有限责任公司 Vibration reduction method for airplane soft oil tank
CN115636094A (en) * 2022-12-23 2023-01-24 西安远飞航空技术发展有限公司 Connecting structure of skin and partition plate, manufacturing method of connecting structure and aircraft oil tank

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