GB294668A - Improvements relating to aeroplanes - Google Patents

Improvements relating to aeroplanes

Info

Publication number
GB294668A
GB294668A GB21963/28A GB2196328A GB294668A GB 294668 A GB294668 A GB 294668A GB 21963/28 A GB21963/28 A GB 21963/28A GB 2196328 A GB2196328 A GB 2196328A GB 294668 A GB294668 A GB 294668A
Authority
GB
United Kingdom
Prior art keywords
members
passages
longitudinal
wings
turbines
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
GB21963/28A
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.)
ADOLPH BERNARD ANDERSON
Original Assignee
ADOLPH BERNARD ANDERSON
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 ADOLPH BERNARD ANDERSON filed Critical ADOLPH BERNARD ANDERSON
Publication of GB294668A publication Critical patent/GB294668A/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
    • B64C11/001—Shrouded propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)

Abstract

294,668. Gallet, M., and Anderson, A. B. July 28, 1927, fConven.tion date]. Propelling by means other than adhesion driving-wheels and racks.-The body of an aeroplane comprises a pair of longitudinal tubular members 7 in the front ends of which are mounted motors 11 and propellers 12. The rear ends of the members are formed with depressions 14 in which are mounted turbines 16 actuated by the air currents to generate power for the motors. A central portion 5 between the members 7 is formed with vertical passages 6, lifting propellers 20 being mounted in the passages. The wings 9 have longitudinal passages 10. The longitudinal passages in the wings and body may be of rectangular, circular or oval cross-section. The members 7 may have flared front ends, as shown in Fig. 6, which also shows a modified arrangement of turbines 18. In a modification. the central portion 5 is tubular, and has a generator driven by an air-screw at its front end. According to the Specification as open to inspection under Sect. 91 (3) (a) the method of propulsion may be applied to land vehicles. This subject-matter does not appear in the Specification as accepted.
GB21963/28A 1927-07-28 1928-07-28 Improvements relating to aeroplanes Expired GB294668A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US294668XA 1927-07-28 1927-07-28

Publications (1)

Publication Number Publication Date
GB294668A true GB294668A (en) 1929-06-13

Family

ID=21849161

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21963/28A Expired GB294668A (en) 1927-07-28 1928-07-28 Improvements relating to aeroplanes

Country Status (1)

Country Link
GB (1) GB294668A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2288157A (en) * 1994-04-07 1995-10-11 Joseph Kenneth Rowe Air turbine electricity generating apparatus eg for vehicles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2288157A (en) * 1994-04-07 1995-10-11 Joseph Kenneth Rowe Air turbine electricity generating apparatus eg for vehicles

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