US2734705A - robertson - Google Patents

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US2734705A
US2734705A US2734705DA US2734705A US 2734705 A US2734705 A US 2734705A US 2734705D A US2734705D A US 2734705DA US 2734705 A US2734705 A US 2734705A
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door
hull
bombs
tray
robertson
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/04Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs

Definitions

  • one or more large bombs, torpedoes or like missiles are carried in crutches on the inner face of a door in the side of the hull, which door is arranged to pivot about its upper edge into a spanwise, or nearly spanwise, bomb discharge position.
  • crutches is meant mountings for releasably supporting the portions of the missiles nearest the door so that, when the door is open, the missiles will be suspended from the crutches
  • the crutches are supported on a tray which is capable of projection from the door in a lengthwise direction, after the door has been opened.
  • the outboard bomb can be brought into position to be dropped by merely opening the door. Usually, however, it will be necessary also to project the tray to bring the inboard bomb into position for dropping.
  • Fig. 1 is a sectional view through the hull of the flying boat, showing how the bombs are hoisted into position
  • Fig. 2 is a plan view, on a larger scale, of the portion of the deck of the hull between the bomb doors,
  • Fig. 3 is a section on the line IIIIII in Fig. 2;
  • Fig. 4 is a section on the line IVIV in Fig. 3,
  • Fig. 5 is a detail view, looking in the direction of the arrow X in Fig. 1, and
  • Fig. 6 is a section on the line VIVI in Fig. 5.
  • the hull 10 of the flying boat is provided at each side with bomb carrying doors 11, these doors being hinged to the hull at their upper ends for movement about longitudinal axes 12.
  • Each door 11 11.
  • Each tray 13 can be slid on its associated door 11, as later described, between the retracted posi-.
  • loading may be accomplished by means of a portable winch 17.
  • Lifting straps 22 fitted to the cable 18 of the winch are attached to the bombs in the vessel 19 by another operator in that vessel.
  • longitudinal guide rails 20 are provided on the tray 13 along which the inner portion 21 of the winch 17 may slide.
  • the tray 13 is adapted to carry two bombs side by side, and the winch is nited States Paten 2,734,705 Patented feb. 14, 1956 shown in Figs. '1, 5 and 6 hoisting the inboard bomb.
  • the winch is telescopic, and can be "extended so that its pawl 23 may engage a similar notch, not shown, in one o'fthe guide rails so as'to locate the winch in theoutboard loading position.
  • the doors 11 are movable from a closed position -to an open bomb dischargepositi'on ⁇ in which t'hey'extend substantially parallel to the span of the wings 40.
  • the mechanism for opening and closing the doors '11 and for moving the tray 13 'frornretracte'dto projected position is-s'hown in Figs. '2-4.
  • a pair of struts 25 To opposite sides of the right hand door 11 are pivoted, at 24, a pair of struts 25. The other ends of the struts 25 are pivoted, at 26, to carriages 27, each attached to a cable 28, extending transversely to thedoor and running over pulleys 29, 30.
  • the pulley 29 is driven, through a gear box 31, from a longitudinal shaft 32 which, in turn, is driven by a reversible electric motor 33. Consequently the door can be opened or closed by the motor 33.
  • the tray 13 of the right hand door carries at each side a nut 34, engaging a screw 35 mounted on the door.
  • the screws 35 are geared, by bevel gears, 36, to a shaft 37 which is rotatable by a reversible electric motor 38, through a gear box 39, for the purpose of moving the tray 13 from retracted to projected position and vice versa.
  • a door in the side of the hull which is hinged to the hull at its upper edge, means for moving said door upwardly and outwardly in relation to said hull from a closed position to an open position in which it extends substantially parallel to the wings, a tray mounted to slide on the door, a power operated screw jack on said door for moving said tray in relation to said door, when said door is open, in a direction transverse to the hull and, mounted on said tray, at least one crutch for supporting an elongated missile extending in the fore and aft direction of the hull.
  • a door in the side of the hull which is hinged to the hull at its upper edge, means for moving said door upwardly and outwardly in relation to said hull from a closed position to an open position in which it extends substantially parallel to the wings, a tray mounted to slide on the door, a power operated screw jack on said door for moving said tray in relation to said door, when said door is open, in a direction transverse to the hull and, mounted side by side on the tray, a pair of crutches for supporting elongated missiles extending in the fore and aft direction of the hull.
  • a door in .the side of the hull which is hinged to the hull at its upper v 3 longitudinal guideway on the tray for guiding a missile hoisting winch, said guideway being notched to locate said winch in alternative positions appropriate for hoisting missiles into the two crutches.
  • a door in the side of the hull which is hinged to the hull at its upper edge so that it may be moved from a closed position to an open position in which it extends substantially parallel to the wings, a pair of spaced cables within the hull, one cable being adjacent to one side of the door and the other cable being adjacent to the other side of the door, means for guiding said cables for movement transversely to said hull, a pair of carriages, one attached to each cable, a pair of struts pivoted respectively to said carriages and pivoted at their other ends to opposite sides of said door, power means for imparting simultaneous movement to said cables to move said door about its hinge through the agency of said carriages and struts, and,
  • At least one crutch for supporting an elongated missile extending in the fore and aft direction of the hull.

Description

Feb. 14, 1956 F. H. ROBERTSON 2,734,705
APPARATUS FOR MOUNTING BOMBS AND THE LIKE IN AIRCRAFT Filed Oct. 11,- 1950 5 Sheets-Sheet. l
Feb. 14, 1956 F. H. ROBERTSON 2,734,705
APPARATUS FOR MOUNTING BOMBS AND THE LIKE IN AIRCRAFT Filed Oct. 11, 1950 5 Sheets-Sheet 2 APPARATUS FOR MOUNTING BOMBS AND THE LIKE IN AIRCRAFT Filed Oct. 11. 1950 w 4, 1956 F. H. ROBERTSON 5 Sheets-Sheet 3 A A A Feb. 14, 1956 F. H. ROBERTSON APPARATUS FOR MOUNTING BOMBS AND THE LIKE IN AIRCRAFT Filed Oct. 11, 1950 5 Sheets-Sheet 4 WWW MN m. k .n H n l l| I lH H" H H unf lflnl l l l l i H n l l l l hu HHH I I I I HI I I Q I N I IHH MWh l I I I I I I I I'I I I MH H M w -v m wi V I I o L I l u Feb. 14, 1956 F. H. ROBERTSON 2,734,705
APPARATUS FOR MOUNTING BOMBS AND THE LIKE IN AIRCRAFT Filed Opt. 11, 1950 5 Sheets-Sheet 5 APPARATUS 'FoR MOUNTING BOMBS AND LIKE 1 AIRCRAFT "Frank Henry Robertson, -Carisbroo'k'e, Isle-oflWightQas- 'signor -to "Saunders-Roe Limited, Osborne, England Application Gctober 11, 1950, Serial No. 189,617
4 Claims. (Cl. 244-137) The dropping of large bombs or torpedoes from a flying boat presents a difiicult problem. It is hardly practicable to drop such bombs through the keel, owing to the difliculty of designing watertight doors for closing the hole in the keel and the structural difficulties of providing a sufliciently large hole. Running the bombs out from the hull onto Outriggers beneath the wings is only practicable for small bombs.
According to the invention, one or more large bombs, torpedoes or like missiles are carried in crutches on the inner face of a door in the side of the hull, which door is arranged to pivot about its upper edge into a spanwise, or nearly spanwise, bomb discharge position. By crutches is meant mountings for releasably supporting the portions of the missiles nearest the door so that, when the door is open, the missiles will be suspended from the crutches Preferably, in order to facilitate loading of the bombs from a boat, the crutches are supported on a tray which is capable of projection from the door in a lengthwise direction, after the door has been opened.
Where two large bombs are supported side by side on the tray, the outboard bomb can be brought into position to be dropped by merely opening the door. Usually, however, it will be necessary also to project the tray to bring the inboard bomb into position for dropping.
One specific embodiment of the invention will now be described in detail, by way of example, with reference to the accompanying diagrammatic drawings, in which:
Fig. 1 is a sectional view through the hull of the flying boat, showing how the bombs are hoisted into position,
Fig. 2 is a plan view, on a larger scale, of the portion of the deck of the hull between the bomb doors,
Fig. 3 is a section on the line IIIIII in Fig. 2;
Fig. 4 is a section on the line IVIV in Fig. 3,
Fig. 5 is a detail view, looking in the direction of the arrow X in Fig. 1, and
Fig. 6 is a section on the line VIVI in Fig. 5.
Referringfirst of all to Fig. 1, the hull 10 of the flying boat is provided at each side with bomb carrying doors 11, these doors being hinged to the hull at their upper ends for movement about longitudinal axes 12. Each door 11.
carries a tray 13, fitted with crutches 14 for supporting the bombs 15. Each tray 13 can be slid on its associated door 11, as later described, between the retracted posi-.
tion shown at the right hand side of Fig. 1 and the projected position shown at the left hand side of that figure. When a bombdoor 11 is in the open position, shown at the left'hand side of Fig. 1, it is at level convenient for loading by an operator standing on the deck 16. As
shown, loading may be accomplished by means of a portable winch 17. Lifting straps 22 fitted to the cable 18 of the winch are attached to the bombs in the vessel 19 by another operator in that vessel.
As shown in Figs. 5 and 6, longitudinal guide rails 20 are provided on the tray 13 along which the inner portion 21 of the winch 17 may slide. The tray 13 is adapted to carry two bombs side by side, and the winch is nited States Paten 2,734,705 Patented feb. 14, 1956 shown in Figs. '1, 5 and 6 hoisting the inboard bomb. A pawl 23 on the which engages a notch in one of the guide rails 20 so "as to locate the Winch 'in loading position. The winch is telescopic, and can be "extended so that its pawl 23 may engage a similar notch, not shown, in one o'fthe guide rails so as'to locate the winch in theoutboard loading position.
As will be seen, the doors 11 are movable from a closed position -to an open bomb dischargepositi'on {in which t'hey'extend substantially parallel to the span of the wings 40. The mechanism for opening and closing the doors '11 and for moving the tray 13 'frornretracte'dto projected position is-s'hown in Figs. '2-4.
The mechanism associated --with the righthand door will here be described, that associated with the left hand door being precisely similar. Parts associated with the left hand door bear the same reference numerals as corresponding parts associated with the right hand door, plus the suffix a.
To opposite sides of the right hand door 11 are pivoted, at 24, a pair of struts 25. The other ends of the struts 25 are pivoted, at 26, to carriages 27, each attached to a cable 28, extending transversely to thedoor and running over pulleys 29, 30. The pulley 29 is driven, through a gear box 31, from a longitudinal shaft 32 which, in turn, is driven by a reversible electric motor 33. Consequently the door can be opened or closed by the motor 33.
The tray 13 of the right hand door carries at each side a nut 34, engaging a screw 35 mounted on the door. The screws 35, are geared, by bevel gears, 36, to a shaft 37 which is rotatable by a reversible electric motor 38, through a gear box 39, for the purpose of moving the tray 13 from retracted to projected position and vice versa.
By the method of stowage according ot the invention it is possible to accommodate in the hull and to discharge eflectively missiles of length of the order of 20 ft.
What I claim as my invention and desire to secure by Letters Patent is:
1. In a flying boat having wings and a hull, a door in the side of the hull which is hinged to the hull at its upper edge, means for moving said door upwardly and outwardly in relation to said hull from a closed position to an open position in which it extends substantially parallel to the wings, a tray mounted to slide on the door, a power operated screw jack on said door for moving said tray in relation to said door, when said door is open, in a direction transverse to the hull and, mounted on said tray, at least one crutch for supporting an elongated missile extending in the fore and aft direction of the hull.
2. In a flying boat having wings and a hull, a door in the side of the hull which is hinged to the hull at its upper edge, means for moving said door upwardly and outwardly in relation to said hull from a closed position to an open position in which it extends substantially parallel to the wings, a tray mounted to slide on the door, a power operated screw jack on said door for moving said tray in relation to said door, when said door is open, in a direction transverse to the hull and, mounted side by side on the tray, a pair of crutches for supporting elongated missiles extending in the fore and aft direction of the hull.
3. In a flying boat having wings and a hull, a door in .the side of the hull which is hinged to the hull at its upper v 3 longitudinal guideway on the tray for guiding a missile hoisting winch, said guideway being notched to locate said winch in alternative positions appropriate for hoisting missiles into the two crutches.
4. In a flying boat having wings and a hull, a door in the side of the hull which is hinged to the hull at its upper edge so that it may be moved from a closed position to an open position in which it extends substantially parallel to the wings, a pair of spaced cables within the hull, one cable being adjacent to one side of the door and the other cable being adjacent to the other side of the door, means for guiding said cables for movement transversely to said hull, a pair of carriages, one attached to each cable, a pair of struts pivoted respectively to said carriages and pivoted at their other ends to opposite sides of said door, power means for imparting simultaneous movement to said cables to move said door about its hinge through the agency of said carriages and struts, and,
mounted on the inner face of the door, at least one crutch for supporting an elongated missile extending in the fore and aft direction of the hull.
References Cited the file of this patent UNITED STATES PATENTS 2,141,181 Geddes Dec. 27, 1938 2,273,724 Nelson et al Feb. 17, 1942 2,343,638 Bock Mar. 7, 1944 2,411,647 Bonnell et al Nov. 26, 1946 2,520,317 Laddon et al Aug. 29, 1950 2,529,908 Bortner Nov. 14, 1950 FOREIGN PATENTS 428,934 Great Britain May 15, 1935 554,434 Great Britain July 5, 1943 556,933 Great Britain Oct. 28, 1943
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Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2950073A (en) * 1957-02-18 1960-08-23 Lockheed Aircraft Corp Hoist mechanism
US2967631A (en) * 1957-04-26 1961-01-10 Edward M Storma Method and apparatus for underwater loading of a water vessel
US2985412A (en) * 1957-03-25 1961-05-23 Martin Co Stores loading of water-based aircraft
US3719338A (en) * 1971-02-23 1973-03-06 Us Navy Bombload handling apparatus
US4111313A (en) * 1977-05-06 1978-09-05 J. Ray Mcdermott & Co. Diving bell handling system and method
US4168047A (en) * 1975-07-03 1979-09-18 R. Alkan & Cie Automatic load carrier and jettisoning system with built-in hoisting means
US4288193A (en) * 1979-02-20 1981-09-08 Steinbock Gmbh Arrangement for forming and handling collective loads
US5762297A (en) * 1996-09-23 1998-06-09 Skyhook Rescue Systems, Inc. Recovery device for use in an airborne vehicle
US6059266A (en) * 1996-09-23 2000-05-09 Ascherin; Terry C. Recovery device
US20040155143A1 (en) * 2001-06-04 2004-08-12 Rafi Yoeli Vehicles particularly useful as vtol vehicles
US20050178881A1 (en) * 2002-05-28 2005-08-18 Rafi Yoeli Ducted fan vehicles particularly useful as VTOL aircraft
US20060113426A1 (en) * 2002-08-05 2006-06-01 Raphael Yoeli Vtol vehicles
US7104503B1 (en) * 2004-06-16 2006-09-12 Robert Callahan Aircraft loading apparatus
US20070034734A1 (en) * 2005-04-15 2007-02-15 Urban Aeronautics Ltd. Flight control system especially suited for VTOL vehicles
US20070034739A1 (en) * 2003-10-27 2007-02-15 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
US20070095971A1 (en) * 2005-06-07 2007-05-03 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
US20080283673A1 (en) * 2005-01-10 2008-11-20 Urban Aeronautics Ltd. Ducted Fan Vtol Vehicles
US20090084907A1 (en) * 2006-03-01 2009-04-02 Urban Aeronautics Ltd. Ground Effect Vanes Arrangement
US20090159757A1 (en) * 2006-05-03 2009-06-25 Raphael Yoeli Ducted Fan Vtol Vehicles
US20100051740A1 (en) * 2008-09-02 2010-03-04 Urban Aeronautics Ltd. Vtol vehicle with coaxially tilted or tiltable rotors
US20100076625A1 (en) * 2006-11-30 2010-03-25 Raphael Yoeli Flight control cockpit modes in ducted fan vtol vehicles
US20100270419A1 (en) * 2007-12-14 2010-10-28 Raphael Yoeli Redundancies and flows in vehicles
US20110049306A1 (en) * 2007-05-02 2011-03-03 Raphael Yoeli Control flows and forces in vtol vehicles
US7918416B2 (en) 2001-05-29 2011-04-05 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US8833692B2 (en) 2006-11-27 2014-09-16 Urban Aeronautics Ltd. Wall effects on VTOL vehicles
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
US10518595B2 (en) 2013-03-15 2019-12-31 Terrafugia, Inc. Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities
US10549854B2 (en) * 2015-03-26 2020-02-04 Bell Helicopter Textron Inc. Integrated aircraft hoist
US11067164B2 (en) 2016-04-15 2021-07-20 Terrafugia, Inc. Electronic gear shifter assembly for a dual-mode flying and driving vehicle
US11370544B2 (en) * 2020-06-03 2022-06-28 Textron Innovations Inc Translating payload bay pallet for aircraft
US11401035B2 (en) 2020-04-06 2022-08-02 Textron Innovations Inc. Cargo doors for payload bay having internal payload extension and retraction mechanism

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB428934A (en) * 1933-11-15 1935-05-15 Hawker Aircraft Ltd Improvements in or relating to bomb or like carrying and releasing gear for aircraft
US2141181A (en) * 1934-12-04 1938-12-27 Geddes Norman Bel Ship
US2273724A (en) * 1939-11-08 1942-02-17 Boeing Aircraft Co Bomb-carrying airplane
GB554434A (en) * 1939-10-26 1943-07-05 Blackburn Aircraft Ltd Improvements in or relating to bomb gear for aircraft
GB556933A (en) * 1941-01-14 1943-10-28 Short Brothers Rochester & Bedford Ltd Improvements in means for loading bombs on aircraft
US2343638A (en) * 1943-02-12 1944-03-07 Whiting Corp Hoisting apparatus
US2411647A (en) * 1944-08-25 1946-11-26 Cons Vultee Aircraft Corp Bomb loading apparatus for airplanes
US2520317A (en) * 1943-04-10 1950-08-29 Isaac M Laddon Bomb handling means
US2529908A (en) * 1945-09-15 1950-11-14 Glenn L Martin Co Cargo hoist

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB428934A (en) * 1933-11-15 1935-05-15 Hawker Aircraft Ltd Improvements in or relating to bomb or like carrying and releasing gear for aircraft
US2141181A (en) * 1934-12-04 1938-12-27 Geddes Norman Bel Ship
GB554434A (en) * 1939-10-26 1943-07-05 Blackburn Aircraft Ltd Improvements in or relating to bomb gear for aircraft
US2273724A (en) * 1939-11-08 1942-02-17 Boeing Aircraft Co Bomb-carrying airplane
GB556933A (en) * 1941-01-14 1943-10-28 Short Brothers Rochester & Bedford Ltd Improvements in means for loading bombs on aircraft
US2343638A (en) * 1943-02-12 1944-03-07 Whiting Corp Hoisting apparatus
US2520317A (en) * 1943-04-10 1950-08-29 Isaac M Laddon Bomb handling means
US2411647A (en) * 1944-08-25 1946-11-26 Cons Vultee Aircraft Corp Bomb loading apparatus for airplanes
US2529908A (en) * 1945-09-15 1950-11-14 Glenn L Martin Co Cargo hoist

Cited By (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2950073A (en) * 1957-02-18 1960-08-23 Lockheed Aircraft Corp Hoist mechanism
US2985412A (en) * 1957-03-25 1961-05-23 Martin Co Stores loading of water-based aircraft
US2967631A (en) * 1957-04-26 1961-01-10 Edward M Storma Method and apparatus for underwater loading of a water vessel
US3719338A (en) * 1971-02-23 1973-03-06 Us Navy Bombload handling apparatus
US4168047A (en) * 1975-07-03 1979-09-18 R. Alkan & Cie Automatic load carrier and jettisoning system with built-in hoisting means
US4111313A (en) * 1977-05-06 1978-09-05 J. Ray Mcdermott & Co. Diving bell handling system and method
US4288193A (en) * 1979-02-20 1981-09-08 Steinbock Gmbh Arrangement for forming and handling collective loads
US5762297A (en) * 1996-09-23 1998-06-09 Skyhook Rescue Systems, Inc. Recovery device for use in an airborne vehicle
US6059266A (en) * 1996-09-23 2000-05-09 Ascherin; Terry C. Recovery device
US7918416B2 (en) 2001-05-29 2011-04-05 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US20050242231A1 (en) * 2001-06-04 2005-11-03 Rafi Yoeli Vehicles particularly useful as VTOL vehicles
US7789342B2 (en) 2001-06-04 2010-09-07 Urban Aeronautics, Ltd. Vehicles particularly useful as VTOL vehicles
US20040155143A1 (en) * 2001-06-04 2004-08-12 Rafi Yoeli Vehicles particularly useful as vtol vehicles
US6883748B2 (en) * 2001-06-04 2005-04-26 Rafi Yoeli Vehicles particularly useful as VTOL vehicles
US20080142643A1 (en) * 2001-06-04 2008-06-19 Urban Aeronautics, Ltd. Vehicles particularly useful as VTOL vehicles
US7246769B2 (en) * 2001-06-04 2007-07-24 Urban Aeronautics, Ltd. Vehicles particularly useful as VTOL vehicles
US7275712B2 (en) 2002-05-28 2007-10-02 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US20050178881A1 (en) * 2002-05-28 2005-08-18 Rafi Yoeli Ducted fan vehicles particularly useful as VTOL aircraft
US20060113426A1 (en) * 2002-08-05 2006-06-01 Raphael Yoeli Vtol vehicles
US20110168834A1 (en) * 2003-10-27 2011-07-14 Urban Aeronautics Ltd. Ducted fan vtol vehicles
US20070034739A1 (en) * 2003-10-27 2007-02-15 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
US8622335B2 (en) 2003-10-27 2014-01-07 Urban Aeronautics, Ltd. Ducted fan VTOL vehicles
US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
US7104503B1 (en) * 2004-06-16 2006-09-12 Robert Callahan Aircraft loading apparatus
US20080283673A1 (en) * 2005-01-10 2008-11-20 Urban Aeronautics Ltd. Ducted Fan Vtol Vehicles
US7806362B2 (en) 2005-01-10 2010-10-05 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
US7946528B2 (en) 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US20070034734A1 (en) * 2005-04-15 2007-02-15 Urban Aeronautics Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
US20070095971A1 (en) * 2005-06-07 2007-05-03 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
US8020804B2 (en) 2006-03-01 2011-09-20 Urban Aeronautics, Ltd. Ground effect vanes arrangement
US20090084907A1 (en) * 2006-03-01 2009-04-02 Urban Aeronautics Ltd. Ground Effect Vanes Arrangement
US20090159757A1 (en) * 2006-05-03 2009-06-25 Raphael Yoeli Ducted Fan Vtol Vehicles
US8833692B2 (en) 2006-11-27 2014-09-16 Urban Aeronautics Ltd. Wall effects on VTOL vehicles
US20100076625A1 (en) * 2006-11-30 2010-03-25 Raphael Yoeli Flight control cockpit modes in ducted fan vtol vehicles
US8496200B2 (en) 2007-05-02 2013-07-30 Urban Aeronautics Ltd. Control flows and forces in VTOL vehicles
US20110049306A1 (en) * 2007-05-02 2011-03-03 Raphael Yoeli Control flows and forces in vtol vehicles
US20100270419A1 (en) * 2007-12-14 2010-10-28 Raphael Yoeli Redundancies and flows in vehicles
US8342441B2 (en) 2008-09-02 2013-01-01 Urban Aeronautics Ltd. VTOL vehicle with coaxially tilted or tiltable rotors
US20100051740A1 (en) * 2008-09-02 2010-03-04 Urban Aeronautics Ltd. Vtol vehicle with coaxially tilted or tiltable rotors
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
US10518595B2 (en) 2013-03-15 2019-12-31 Terrafugia, Inc. Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities
US11014418B2 (en) 2013-03-15 2021-05-25 Terrafugia, Inc. Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities
US10549854B2 (en) * 2015-03-26 2020-02-04 Bell Helicopter Textron Inc. Integrated aircraft hoist
US11067164B2 (en) 2016-04-15 2021-07-20 Terrafugia, Inc. Electronic gear shifter assembly for a dual-mode flying and driving vehicle
US11401035B2 (en) 2020-04-06 2022-08-02 Textron Innovations Inc. Cargo doors for payload bay having internal payload extension and retraction mechanism
US11370544B2 (en) * 2020-06-03 2022-06-28 Textron Innovations Inc Translating payload bay pallet for aircraft

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