GB413948A - Improvements in auxiliary lifting means for aeroplanes - Google Patents

Improvements in auxiliary lifting means for aeroplanes

Info

Publication number
GB413948A
GB413948A GB34266/33A GB3426633A GB413948A GB 413948 A GB413948 A GB 413948A GB 34266/33 A GB34266/33 A GB 34266/33A GB 3426633 A GB3426633 A GB 3426633A GB 413948 A GB413948 A GB 413948A
Authority
GB
United Kingdom
Prior art keywords
aircraft
stabilizers
aeroplanes
lifting means
fuselage
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
GB34266/33A
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 GB34266/33A priority Critical patent/GB413948A/en
Publication of GB413948A publication Critical patent/GB413948A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

413,948. Aircraft. WOOD, W. H., 248, Winona Drive, Toronto, Canada. Dec. 6, 1933, No. 34266. [Class 4.] Slots 6 in the top wall of an aircraft fuselage are connected by a divided channel having suction outlets 11 leading into two longitudinal tubes 12 through which air is forced by forward travel of the machine and which are provided with nozzles 13 and suction fans 16 driven, e.g. from the aircraft engine. The front ends of the tubes may be closed by shutters operated by the pilot. Stabilizers comprising two discs with radial vanes are mounted one on each side of the fuselage, the upper half of the stabilizers being covered in so that they are revolved by air flow.
GB34266/33A 1933-12-06 1933-12-06 Improvements in auxiliary lifting means for aeroplanes Expired GB413948A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB34266/33A GB413948A (en) 1933-12-06 1933-12-06 Improvements in auxiliary lifting means for aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB34266/33A GB413948A (en) 1933-12-06 1933-12-06 Improvements in auxiliary lifting means for aeroplanes

Publications (1)

Publication Number Publication Date
GB413948A true GB413948A (en) 1934-07-26

Family

ID=10363500

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34266/33A Expired GB413948A (en) 1933-12-06 1933-12-06 Improvements in auxiliary lifting means for aeroplanes

Country Status (1)

Country Link
GB (1) GB413948A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490644A (en) * 1993-12-20 1996-02-13 The Boeing Company Ducted boundary layer diverter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490644A (en) * 1993-12-20 1996-02-13 The Boeing Company Ducted boundary layer diverter

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