GB578862A - Improvements relating to connection between a tug-plane and a trailer - Google Patents

Improvements relating to connection between a tug-plane and a trailer

Info

Publication number
GB578862A
GB578862A GB708544A GB708544A GB578862A GB 578862 A GB578862 A GB 578862A GB 708544 A GB708544 A GB 708544A GB 708544 A GB708544 A GB 708544A GB 578862 A GB578862 A GB 578862A
Authority
GB
United Kingdom
Prior art keywords
trailer
tug
plane
control surfaces
vertical
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
GB708544A
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.)
STEFAN WACLAW MALINOWSKI
Original Assignee
STEFAN WACLAW MALINOWSKI
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 STEFAN WACLAW MALINOWSKI filed Critical STEFAN WACLAW MALINOWSKI
Priority to GB708544A priority Critical patent/GB578862A/en
Publication of GB578862A publication Critical patent/GB578862A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D5/00Aircraft transported by aircraft, e.g. for release or reberthing during flight

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manipulator (AREA)

Abstract

578,862. Aircraft. MALINOWSKI, S. W. April 17, 1944, No. 7085. [Class 4] A rigid connection between a tug plane and trailer comprises one or more universal joints or hinges which either of themselves control the control surfaces of the trailer, or are so arranged with intercoupling of the control surfaces of the tug plane and trailer, that the trailer automatically adopts the angle of flight corresponding to the speed of the tug plane, whilst being free to move in either a vertical or a vertical and a horizontal plane with respect to the tug. Due to such connection, when the trailer moves out of alignment with the tug plane the control surfaces of the trailer may be operated automatically by rods, wires, gear wheels, or other mechanism to return the tug plane to its correct attitude, or the pilot may operate the control surfaces of both machines simultaneously. In the arrangement shown in Fig. 1, a trailer comprising two booms 1, 2, and a rear wing 5 is articulated at points A to a tug plane 7, lateral movement of the trailer being prevented by tie members 6. The rudders 3, 4, of the trailer are moved by the pilot simultaneously with the rudder 10 of the tug plane. In the form according to Fig. 2 the trailer is allowed free vertical and horizontal movement with respect to the tug plane by means of two beams 1, 2, universally attached at A to the tug plane and through vertical hinges B to the trailer wing 5, the control surfaces of the trailer being operated automatically upon displacement of the trailer relatively to the tug. In further constructions the tug and trailer planes are directly connected together by universal joints or through a rigid boom.
GB708544A 1944-04-17 1944-04-17 Improvements relating to connection between a tug-plane and a trailer Expired GB578862A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB708544A GB578862A (en) 1944-04-17 1944-04-17 Improvements relating to connection between a tug-plane and a trailer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB708544A GB578862A (en) 1944-04-17 1944-04-17 Improvements relating to connection between a tug-plane and a trailer

Publications (1)

Publication Number Publication Date
GB578862A true GB578862A (en) 1946-07-15

Family

ID=9826319

Family Applications (1)

Application Number Title Priority Date Filing Date
GB708544A Expired GB578862A (en) 1944-04-17 1944-04-17 Improvements relating to connection between a tug-plane and a trailer

Country Status (1)

Country Link
GB (1) GB578862A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5188313A (en) * 1992-01-03 1993-02-23 Piasecki Aircraft Corporation Glider aircraft tow control system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5188313A (en) * 1992-01-03 1993-02-23 Piasecki Aircraft Corporation Glider aircraft tow control system

Similar Documents

Publication Publication Date Title
US2863618A (en) Airplane coupling means
GB1500453A (en) Articulated main landing gear
US2385392A (en) Crewless glider
GB1157822A (en) VTOL Aircraft
GB578862A (en) Improvements relating to connection between a tug-plane and a trailer
US2524605A (en) Arrangement for securing and controlling a movable flap at the trailing edge of an airplane wing
US2303695A (en) Differential rudder for airplanes
GB1195387A (en) Improvements relating to VTOL Aircraft
US2659999A (en) Control for model airplanes
GB1187857A (en) Motion Simulator.
GB1323997A (en) Aircraft
GB1100376A (en) Improvements in aircraft
US2383845A (en) Device for operation of the controls of airplanes
GB922233A (en) Improvements in or relating to ornithopters
US2445550A (en) Control system for adjusting the incidence of the blades of the rotor of a rotary-wing aircraft
US1366917A (en) Controlling device for airships
GB526775A (en) Improvements in or relating to aircraft-stabilizing devices
GB584700A (en) Improvements in or relating to control flaps or tabs for aircraft
GB854459A (en) Improvements in aeroplanes
GB628684A (en) Improvements in aircraft control surfaces
GB825332A (en) Improvements in or relating to landing gear of aircraft
GB819665A (en) Improvements in or relating to high speed aircraft
US2437250A (en) Means for selective disconnection of aileron controls
GB1230381A (en)
GB585891A (en) Improvements in full span flap and aileron control