GB799290A - Improvements relating to aircraft tail assemblies - Google Patents

Improvements relating to aircraft tail assemblies

Info

Publication number
GB799290A
GB799290A GB2722254A GB2722254A GB799290A GB 799290 A GB799290 A GB 799290A GB 2722254 A GB2722254 A GB 2722254A GB 2722254 A GB2722254 A GB 2722254A GB 799290 A GB799290 A GB 799290A
Authority
GB
United Kingdom
Prior art keywords
improvements relating
aircraft tail
tail assemblies
helicopter
sept
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
GB2722254A
Inventor
George Steedman Hislop
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB2722254A priority Critical patent/GB799290A/en
Publication of GB799290A publication Critical patent/GB799290A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft

Abstract

799,290. Helicopters. FAIREY AVIATION CO., Ltd. Sept. 14, 1955 [Sept. 20, 1954], No. 27222/54. Class 4. A helicopter has a tail assembly including at least one fin 3 and a tailplane 1, two aerofoils 4 symmetrically located on opposite sides of the fore-and-aft axis of the helicopter and pivoted,
GB2722254A 1954-09-20 1954-09-20 Improvements relating to aircraft tail assemblies Expired GB799290A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2722254A GB799290A (en) 1954-09-20 1954-09-20 Improvements relating to aircraft tail assemblies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2722254A GB799290A (en) 1954-09-20 1954-09-20 Improvements relating to aircraft tail assemblies

Publications (1)

Publication Number Publication Date
GB799290A true GB799290A (en) 1958-08-06

Family

ID=10256125

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2722254A Expired GB799290A (en) 1954-09-20 1954-09-20 Improvements relating to aircraft tail assemblies

Country Status (1)

Country Link
GB (1) GB799290A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5096143A (en) * 1989-09-04 1992-03-17 William Nash Tail unit with rotatable tailplane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5096143A (en) * 1989-09-04 1992-03-17 William Nash Tail unit with rotatable tailplane

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