GB730069A - Improvements in flying machines capable of taking off and landing vertically - Google Patents

Improvements in flying machines capable of taking off and landing vertically

Info

Publication number
GB730069A
GB730069A GB4498/53A GB449853A GB730069A GB 730069 A GB730069 A GB 730069A GB 4498/53 A GB4498/53 A GB 4498/53A GB 449853 A GB449853 A GB 449853A GB 730069 A GB730069 A GB 730069A
Authority
GB
United Kingdom
Prior art keywords
wing
turbine
taking
propeller
feb
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
GB4498/53A
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.)
HELMIT PHILIPP GEORG ALEXANDER
Original Assignee
HELMIT PHILIPP GEORG ALEXANDER
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 HELMIT PHILIPP GEORG ALEXANDER filed Critical HELMIT PHILIPP GEORG ALEXANDER
Publication of GB730069A publication Critical patent/GB730069A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091—Accessories not provided for elsewhere

Abstract

730,069. Gas turbine plant. ZBOROWSKI, H.P.G.A.R. VON. Feb. 18, 1953 [Feb. 19, 1952], No. 4498/53. Class 110 (3). [Also in Group XXXIII] A gas turbine plant includes a compressor 12 and turbine 11 the shaft of which drives contrarotating propellers 10, 10a enclosed within an annular wing 1. The turbine may be cooled as described in Specification 711,985. The turbine exhaust issues from slots 21 in propeller 10, and fuel is injected from orifices 22 in propeller 10a, being ignited by pilot devices 23, to form an afterburner within the casing of wing 1, as described in Specification 713,863. Flaps 29 may open passages 28 in the wing and surfaces 24 may be operated to deflect the jet stream.
GB4498/53A 1952-02-19 1953-02-18 Improvements in flying machines capable of taking off and landing vertically Expired GB730069A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR730069X 1952-02-19

Publications (1)

Publication Number Publication Date
GB730069A true GB730069A (en) 1955-05-18

Family

ID=9113081

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4498/53A Expired GB730069A (en) 1952-02-19 1953-02-18 Improvements in flying machines capable of taking off and landing vertically

Country Status (1)

Country Link
GB (1) GB730069A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1041367B (en) * 1955-11-22 1958-10-16 Snecma Formation of the wing flaps for vertically ascending and landing aircraft, especially tubular wing missiles, as landing feet
GB2188987A (en) * 1986-04-09 1987-10-14 Rolls Royce A turbofan gas turbine engine and mountings therefore
GB2260369A (en) * 1991-08-30 1993-04-14 United Technologies Corp Jet propulsion system having ejector shroud

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1041367B (en) * 1955-11-22 1958-10-16 Snecma Formation of the wing flaps for vertically ascending and landing aircraft, especially tubular wing missiles, as landing feet
GB2188987A (en) * 1986-04-09 1987-10-14 Rolls Royce A turbofan gas turbine engine and mountings therefore
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
GB2260369A (en) * 1991-08-30 1993-04-14 United Technologies Corp Jet propulsion system having ejector shroud
GB2260369B (en) * 1991-08-30 1994-07-06 United Technologies Corp Propulsion system assembly

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