GB794768A - Jet propelling unit - Google Patents

Jet propelling unit

Info

Publication number
GB794768A
GB794768A GB1811/56A GB181156A GB794768A GB 794768 A GB794768 A GB 794768A GB 1811/56 A GB1811/56 A GB 1811/56A GB 181156 A GB181156 A GB 181156A GB 794768 A GB794768 A GB 794768A
Authority
GB
United Kingdom
Prior art keywords
engines
jet
jan
aircraft
adjusted
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
GB1811/56A
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
Publication of GB794768A publication Critical patent/GB794768A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets

Abstract

794,768. Jet propulsion plant. CAILLETTE, G. Jan. 19, 1956 [Jan. 25, 1955], No. 1811/56. Class 110 (3). [Also in Group XXXIII] A jet-propulsion plant comprises two jetpropulsion engines 2, 3 arranged coaxially with their air inlets facing each other. The rear engine 2 has a single propulsion nozzle 8, the direction of which may be adjusted for control purposes and the front engine 3 is provided with a bifurcated jet pipe 9, each branch of which terminates in a rearwardly directed nozzle 11. These also may be adjusted for control purposes and the flow of gas to the respective nozzles may be controlled by valve mechanism 16. When installed in an aircraft, air. intakes located on each side of the aircraft each connect with a duct 5, each divided into branches 6, 7 taken respectively to the engines 2 and 3. The airflow to respective engines may be controlled by valve mechanism 15 at the junction of each set of ducts 5, 6 and 7. Specification 740,796, [Group XX], and French Specification 947,552 are referred to.
GB1811/56A 1955-01-25 1956-01-19 Jet propelling unit Expired GB794768A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR794768X 1955-01-25

Publications (1)

Publication Number Publication Date
GB794768A true GB794768A (en) 1958-05-07

Family

ID=9234234

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1811/56A Expired GB794768A (en) 1955-01-25 1956-01-19 Jet propelling unit

Country Status (1)

Country Link
GB (1) GB794768A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2264907A (en) * 1992-02-10 1993-09-15 Peter Antony Hulmes Multi-engined aircraft.
GB2313580A (en) * 1996-05-31 1997-12-03 Astovl Limited Power plant for producing variable direction efflux

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2264907A (en) * 1992-02-10 1993-09-15 Peter Antony Hulmes Multi-engined aircraft.
GB2313580A (en) * 1996-05-31 1997-12-03 Astovl Limited Power plant for producing variable direction efflux
GB2313580B (en) * 1996-05-31 2000-02-23 Astovl Limited An aircraft power plant
US6260800B1 (en) 1996-05-31 2001-07-17 Astovl Limited Aircraft power plant with two air intake fans

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