GB268903A - Improvements in heavier-than-air aircraft - Google Patents

Improvements in heavier-than-air aircraft

Info

Publication number
GB268903A
GB268903A GB2034/26A GB203426A GB268903A GB 268903 A GB268903 A GB 268903A GB 2034/26 A GB2034/26 A GB 2034/26A GB 203426 A GB203426 A GB 203426A GB 268903 A GB268903 A GB 268903A
Authority
GB
United Kingdom
Prior art keywords
cylinder
air
shaft
vanes
opening
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
GB2034/26A
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.)
JAMES JOSEPH FITZGERALD
Original Assignee
JAMES JOSEPH FITZGERALD
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 JAMES JOSEPH FITZGERALD filed Critical JAMES JOSEPH FITZGERALD
Priority to GB2034/26A priority Critical patent/GB268903A/en
Publication of GB268903A publication Critical patent/GB268903A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/006—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a vertical axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

268,903. Fitzgerald, J. J. Jan. 23, 1926. Machines supported by direct fluid pressure apparatus; propelling.-An aircraft 10 is lifted straight up into the air by means of a pair of " air turbines " comprising a fixed casing 11 and sets of vanes 15, 16 carried respectively by a cylinder 12 and a shaft 17. The cylinder and shaft are driven in opposite senses by a motor and cause air to be drawn in through an opening 24 and compressed in the cylinder. When the pressure within the cylinder reaches a predetermined value the vanes 16 move the shaft 17 upwards against a spring 23 allowing air to escape through an opening 25. The Specification includes a statement of the theory of operation.
GB2034/26A 1926-01-23 1926-01-23 Improvements in heavier-than-air aircraft Expired GB268903A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2034/26A GB268903A (en) 1926-01-23 1926-01-23 Improvements in heavier-than-air aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2034/26A GB268903A (en) 1926-01-23 1926-01-23 Improvements in heavier-than-air aircraft

Publications (1)

Publication Number Publication Date
GB268903A true GB268903A (en) 1927-04-14

Family

ID=9732435

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2034/26A Expired GB268903A (en) 1926-01-23 1926-01-23 Improvements in heavier-than-air aircraft

Country Status (1)

Country Link
GB (1) GB268903A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3379366A (en) * 1965-11-18 1968-04-23 Snecma Contra-rotating compressors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3379366A (en) * 1965-11-18 1968-04-23 Snecma Contra-rotating compressors

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