GB213705A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB213705A
GB213705A GB154323A GB154323A GB213705A GB 213705 A GB213705 A GB 213705A GB 154323 A GB154323 A GB 154323A GB 154323 A GB154323 A GB 154323A GB 213705 A GB213705 A GB 213705A
Authority
GB
United Kingdom
Prior art keywords
planes
struts
stepped
series
girders
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
GB154323A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB154323A priority Critical patent/GB213705A/en
Publication of GB213705A publication Critical patent/GB213705A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/006—Paddle wheels

Abstract

213,705. McKelvey, A. L. Jan. 17, 1923. Planes, arrangement and disposition of; planes, connecting to machine; framework. -A rigid framework for supporting a stepped series of sustaining planes B, consists of a lattice girder A projecting from which are struts 5 supporting tension wires or bars 6. A complete sustaining unit comprises a number of these stepped series of planes arranged side by side, each series being supported between two lattice girders A. The girders A consist of upper and lower booms 2, formed of angle strips placed back-to-back, and rigidly connected at their ends to vertically-disposed laced struts 1. The stepped planes B are fixed, by means of angle plates 7, to diagonally-arranged bracing strips 4 which are riveted at their ends to the booms 2. Steering, balancing, and regulating altitude. - Elevating planes C are rotatably mounted in bracket-bearings 8 mounted upon the vertical struts 1.
GB154323A 1923-01-17 1923-01-17 Improvements in and relating to aircraft Expired GB213705A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB154323A GB213705A (en) 1923-01-17 1923-01-17 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB154323A GB213705A (en) 1923-01-17 1923-01-17 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB213705A true GB213705A (en) 1924-04-10

Family

ID=9723787

Family Applications (1)

Application Number Title Priority Date Filing Date
GB154323A Expired GB213705A (en) 1923-01-17 1923-01-17 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB213705A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5661741A (en) * 1994-06-07 1997-08-26 Mitsubishi Denki Kabushiki Kaisha Semiconductor light emitting device, laser amplifier, and integrated light amplifier and wavelength variable filter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5661741A (en) * 1994-06-07 1997-08-26 Mitsubishi Denki Kabushiki Kaisha Semiconductor light emitting device, laser amplifier, and integrated light amplifier and wavelength variable filter

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