GB823592A - Aircraft powered by turbo-prop engines - Google Patents

Aircraft powered by turbo-prop engines

Info

Publication number
GB823592A
GB823592A GB27599/55A GB2759955A GB823592A GB 823592 A GB823592 A GB 823592A GB 27599/55 A GB27599/55 A GB 27599/55A GB 2759955 A GB2759955 A GB 2759955A GB 823592 A GB823592 A GB 823592A
Authority
GB
United Kingdom
Prior art keywords
nozzle
group xxxiii
turbo
propeller
sept
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
GB27599/55A
Inventor
Ivor Macaulay Davidson
Brian Stapleton Stratford
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB27599/55A priority Critical patent/GB823592A/en
Publication of GB823592A publication Critical patent/GB823592A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Details Of Gearings (AREA)

Abstract

823,592. Jet propulsion plant. POWER JETS (RESEARCH & DEVELOPMENT) Ltd. Sept. 14, 1956 [Sept. 28, 1955], No. 27599/55. Class 110 (3). [Also in Group XXXIII] The nozzle 17a of a turbo-prop engine is shown in vertical section, and is of fish-tail shape in plan. An adjustable flap 7 is disposed so that the exhaust gas stream always follows the upper surface of the flap. A part 20 of the nozzle is pivoted at 21 and is operable by an hydraulic jack 22, so that the area of the nozzle may be varied. The propeller may be of variable pitch, and the flaps 7 and 20 may be deflected downwardly while the pitch of the propeller is reversed to obtain a high lift and a braking effect. This may be done automatically by a device responsive to drop in airspeed. Specifications 595,357, 787,011, [Group XXXIII], 787,012, 790,193, [Group XXXIII], 790,298, [823,591 and 823,593, [both in Group XXXIII]], are referred to.
GB27599/55A 1955-09-28 1955-09-28 Aircraft powered by turbo-prop engines Expired GB823592A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27599/55A GB823592A (en) 1955-09-28 1955-09-28 Aircraft powered by turbo-prop engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27599/55A GB823592A (en) 1955-09-28 1955-09-28 Aircraft powered by turbo-prop engines

Publications (1)

Publication Number Publication Date
GB823592A true GB823592A (en) 1959-11-11

Family

ID=10262256

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27599/55A Expired GB823592A (en) 1955-09-28 1955-09-28 Aircraft powered by turbo-prop engines

Country Status (1)

Country Link
GB (1) GB823592A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1156316B (en) * 1960-06-16 1963-10-24 Power Jets Res & Dev Ltd Aircraft with control elements that can be adjusted in the opposite or in the same direction
FR2893909A1 (en) * 2005-11-29 2007-06-01 Airbus France Sas Horizontally flying aircraft e.g. transport plane, safety ensuring method, involves partially retracting wing flaps when traction force of motors carried by fixed wing is equal to predetermined high value

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1156316B (en) * 1960-06-16 1963-10-24 Power Jets Res & Dev Ltd Aircraft with control elements that can be adjusted in the opposite or in the same direction
FR2893909A1 (en) * 2005-11-29 2007-06-01 Airbus France Sas Horizontally flying aircraft e.g. transport plane, safety ensuring method, involves partially retracting wing flaps when traction force of motors carried by fixed wing is equal to predetermined high value
US8561948B2 (en) 2005-11-29 2013-10-22 Airbus Operations Sas Method for ensuring the safety of an aircraft flying horizontally at low speed

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