US1306348A - Separable aeroplane and gas-bag - Google Patents

Separable aeroplane and gas-bag Download PDF

Info

Publication number
US1306348A
US1306348A US1306348DA US1306348A US 1306348 A US1306348 A US 1306348A US 1306348D A US1306348D A US 1306348DA US 1306348 A US1306348 A US 1306348A
Authority
US
United States
Prior art keywords
aeroplane
gas bag
members
gas
truss
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 - Lifetime
Application number
Publication date
Application granted granted Critical
Publication of US1306348A publication Critical patent/US1306348A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C37/00Convertible aircraft

Definitions

  • This invention relates to means for providing a heavier than air apparatus which is provided with lifting planes, with elevating means additional to the planes thereof, said lifting means comprising a lighter than air construction.
  • It also relates to means for maintaining heavier than air apparatus elevated from the ground by'levitation; and to means for separating said apparatus from the levitation means employed.
  • Additional objects are to obtain means for joining an aeroplane to a gas bag in such manner that they will not be liable to bel come accidentally separated; that the joining means will not be liable to become broken or out of order; and that said joining means will be readily understood and easily operated to effectually join said aeroplane and gas bag.
  • Fig. 2 is an end elevation, on an enlarged scale, of the joining mechanism which is illustrated in Fig. 1.
  • Fig. 3 is a side elevation, also on an enlarged scale, of the joining mechanism illustrated in Figs. 1 and 2.
  • Fig. 4 is a side elevation of an element of the joining mechanism, and of a mutilated screw which forms a member of said element.
  • Fig. 5 is an end elevation on line 5--5 of Fig. 41, viewed in the direction indicated by the arrows.
  • F'g. 6 is a front, (plan view) of a nut which is adapted to be used in assembling the aeroplane and gas bag.
  • Fig. 7 is a side elevation of a longitudinally extending member which forms an joining mechanism, and is permanently attached to the gas bag.
  • Fig. 8 is an end elevation of a guide shaf and a mutilated internally screw threaded member which forms an element in the j oining mechanism, and is permanently attached to the aeroplane. 1
  • Fig. 9 is an end view of the member whlch is illustrated in Fig. 8.
  • Fig. 10 is a side elevation of a modification of the element which is illustrated in Figs. 8 and 9.
  • A (Fig. 1) are lines diagrammatically 1ndicating the upper and lower planes of a biplane.
  • B, B are standards which are firmly attached to the aeroplane, and b, b, are the tie rod-s or wires to said standards.
  • 0, O are members Which join the upper ends of thestandards B.
  • Dis a shaft which is secured atits ends to the members C.
  • the shaft D forms a base on which is secured, as by pins or bolts 6, the member E; and F is a member which is movably mounted on said base.
  • Members E and F are grasping members, operable in the same manner as are vise jaws, when closed upon a co-acting member, (lettered K and hereinafter described) as by nut f.
  • G is an internal screw thread, in member F, and is mutilated to correspond with the mutilated external screw is rigidly secured in place as by key I in keyway I to provide means for a measured turning of said member; and said arms I are connected 'by links or bars J J, together and to operating lever 9', so that operation of said lever operates all said members H.
  • members D, E, F and H are, as hereinbefore stated, permanently attached to the aeropgane which is to be joined to the gas bag.
  • K represent lateral grooves in member- K, throu h which grooves the members H, H, extend.
  • connection M is rigidly secured to the under side of truss L, as by bolts 70 fitting in screw threaded holes is, and said truss is attached to the gas bag 0, as by flexible connections M, m.
  • the connections M are illustrated as rods or cylinders, respectively provided with eye bolts N, engaging with eye bolts n on truss L, and n on base a.
  • Base n" is secured to the plate 0 on the under side of gas bag 0, as by rivets 0r bolts n
  • the connections m are illustrated as wire ropes and they are, also, secured to the truss L and plate 0 of the gas bag, as by eye bolts. Flexibility is attained between the truss and the gas ba 0, by the connections M, m, and eye bolts scribed; while at the same time the direction of movement of an aeroplane joined to said gas bag controls the direction of movement of said gas bag.
  • P is a rack over which the lever 9' moves, when operated, and 10 represents a sprmg actuated locking member which is adapted to engage with the teeth of the rack, to maintain said lever in its predetermined position.
  • Q (Fig. 2) is a spring between member and F.
  • the aeroplane and gas ba When the aeroplane and gas ba are joined by the grasping members E, F eing forced onto the longitudinally extending member K, and held in grasping position by the mutilated screws described, the aeroplane may be operated in the usual manner to make a flight; the levitation of the gas bagassisting materially in rising. At any time, when above the ground, the engine and propeller of the aeroplane may be stopped, and the gas bag be relied upon for levitation.
  • the aeroplane and gas bag are attached together a novice may safely attempt to operate the same, and when sufi'icient practice has been attained the aeroplane may e separated from the gas bag, by movement of lever and the flight continued in the aeroplane, after said separation;
  • the engine and propeller of the aeroplane may be rotated at reduced speed, or entirely stopped, as best suits the demands of the conditions under which said observation 'is being made.
  • a truss member means to attach said "member to said gas ba and means to separably attach said mem r to said aeroplane
  • said attaching means comprising a plurality of members attached to said aeroplane and arranged to register and co-act with said truss member, latch members respectively adapted to co-act with said truss member and said plurality of members, and movable into and out of engaging position, means to hold said latch members in engaging position, and operative means to release said latch meinbers from said holding position, said operative means comprising a lever and connections joining said lever to said holding means.
  • a truss member means to attach said truss member to said gas bag, a latch member, means to attach said latch member'to said truss member, in combination with a latch member attached to said aeroplane and arranged to register with said, truss member, a latch mem er adapted to co-act with the first named latch member, means to attach said co actuable latch member to said aerolane member, means to join said latch members and means to separate said latch memers.
  • a truss member In a combined gas bag and aeroplane, a truss member, means to attach said truss membeil sto said gas bag, a plurality of coactinglatch members, means to connect said latch members to said truss member, said latch members attached to said aeroplane and arranged to register with said truss member and said connecting means comprislurality of members adapted to 00- act with said latch members, in combination with operable means comprising a lever adapted to actuate said plurality of members to separate said co-acting latch members from said truss member.
  • an apparatus consisting of a lighter than air and a heavier than air device, separable means for joining said lighter and heavier devices, comprising a longitudinally extending bar attached to said lighter than air device in combination with members, one whereof is movable, attached to said heavier than air device and adapted to 'engage with said longitudinally extending member, means to force said movable member into engagement with said longitudinally extending member, means to hold said engageable members in engaging position and means to simultaneously release said engaging members.

Description

J. LEWIS. SEPARABLE AEROPLANE AND GAS BAG. APPLICATION FILED AUG.I8, I917.
Patented June 10, 1919.
3 SHEETSSHEET l- Inventor: J/IMES N. LEW/.5
J. N. LEWIS. SEPARABLE AEROPLANE AND GAS BAG. APPLICATION FILED AUG.I8.19II.
Iafonrod June 10, 1919-.
3 SHEETSSHEET 2- \x/ 4 I M 177% z/emvrs JAME N.LEWI5 J. N. LEWIS. SEPARA'BLE AEROPLANE AND GAS BAG. APPLICATION FILED AUG.18.1917.
Patented June 10, 1919.
3 SHEETS-SHEET 3.
JAMES N. LEWIS, OF DETROIT, MICHIGAN.
SEPARABLE AEROPLANE AND GAS-BAG.
' Specification of Letters Patent.
Patented June 10,1919.
Application filed August 18, 1917. Serial N 0. 186,900.
To all whom it may concern Be it known that I, JAMES N. LEWIS, a citizen-of the United States, and a resident of Detroit, in the county of Wayne and State of Michigan, have invented certain new and useful Improvements in Separable Aeroplanes and Gas-Bags, of which the following, when taken in connection with the drawings accompanying and forming a part hereof, is a specification. v
This invention relates to means for providing a heavier than air apparatus which is provided with lifting planes, with elevating means additional to the planes thereof, said lifting means comprising a lighter than air construction.
It also relates to means for maintaining heavier than air apparatus elevated from the ground by'levitation; and to means for separating said apparatus from the levitation means employed.
And the particular objects of the invention are to provide means for joining any type of aeroplane to any type of gas bag which means shall be so constructed that when the joined aeroplane and gas bag are being used it may be either as a flying device or as an observation station.
Further objects are to obtain means for joining the aeroplane used to the gas bag used, in suchmanner that they can be separated efiectually and quickly, to permit said aeroplaneto be operated in the usual manner.
Additional objects are to obtain means for joining an aeroplane to a gas bag in such manner that they will not be liable to bel come accidentally separated; that the joining means will not be liable to become broken or out of order; and that said joining means will be readily understood and easily operated to effectually join said aeroplane and gas bag.
And I also have for an object to so join an aeroplane to a gas bag that the united elements may be used for substantially all the purposes for which the aeroplane may be used when separated from the gas bag. Looping the loop, as it is termed, may not done when the aeroplane and gas bag are 'oined.
I ave illustrated a construction embodying this invention in the drawings accompanymg and forming a part of this specification, in which F gure 1 is a side elevation of a gas bag.
. element of the means attached to the gas bag and means attachable to an aeroplane which are adapted to join the gas bag and aeroplane, and a diagram indicating an aeroplane.
Fig. 2 is an end elevation, on an enlarged scale, of the joining mechanism which is illustrated in Fig. 1.
Fig. 3 is a side elevation, also on an enlarged scale, of the joining mechanism illustrated in Figs. 1 and 2.
Fig. 4 is a side elevation of an element of the joining mechanism, and of a mutilated screw which forms a member of said element.
Fig. 5 is an end elevation on line 5--5 of Fig. 41, viewed in the direction indicated by the arrows.
F'g. 6 is a front, (plan view) of a nut which is adapted to be used in assembling the aeroplane and gas bag.
Fig. 7 is a side elevation of a longitudinally extending member which forms an joining mechanism, and is permanently attached to the gas bag.
Fig. 8 is an end elevation of a guide shaf and a mutilated internally screw threaded member which forms an element in the j oining mechanism, and is permanently attached to the aeroplane. 1
Fig. 9 is an end view of the member whlch is illustrated in Fig. 8.
And Fig. 10 is a side elevation of a modification of the element which is illustrated in Figs. 8 and 9.
A reference character applied to a given part is used to indicate said part throughout the several figures of the drawings wherever the same appears.
A, (Fig. 1) are lines diagrammatically 1ndicating the upper and lower planes of a biplane. B, B, are standards which are firmly attached to the aeroplane, and b, b, are the tie rod-s or wires to said standards. 0, O, are members Which join the upper ends of thestandards B. Dis a shaft which is secured atits ends to the members C. The shaft D forms a base on which is secured, as by pins or bolts 6, the member E; and F is a member which is movably mounted on said base. Members E and F are grasping members, operable in the same manner as are vise jaws, when closed upon a co-acting member, (lettered K and hereinafter described) as by nut f. G is an internal screw thread, in member F, and is mutilated to correspond with the mutilated external screw is rigidly secured in place as by key I in keyway I to provide means for a measured turning of said member; and said arms I are connected 'by links or bars J J, together and to operating lever 9', so that operation of said lever operates all said members H. The
members D, E, F and H are, as hereinbefore stated, permanently attached to the aeropgane which is to be joined to the gas bag.
K represent lateral grooves in member- K, throu h which grooves the members H, H, extend.
Member K is rigidly secured to the under side of truss L, as by bolts 70 fitting in screw threaded holes is, and said truss is attached to the gas bag 0, as by flexible connections M, m. The connections M are illustrated as rods or cylinders, respectively provided with eye bolts N, engaging with eye bolts n on truss L, and n on base a. Base n" is secured to the plate 0 on the under side of gas bag 0, as by rivets 0r bolts n The connections m are illustrated as wire ropes and they are, also, secured to the truss L and plate 0 of the gas bag, as by eye bolts. Flexibility is attained between the truss and the gas ba 0, by the connections M, m, and eye bolts scribed; while at the same time the direction of movement of an aeroplane joined to said gas bag controls the direction of movement of said gas bag.
P is a rack over which the lever 9' moves, when operated, and 10 represents a sprmg actuated locking member which is adapted to engage with the teeth of the rack, to maintain said lever in its predetermined position. Q (Fig. 2) is a spring between member and F.
To close members E and F on member K, thereby joining the aeroplane and gas bag, the nut f is turned on mutilated screw H into substantially the position in which it is illustrated in Fig. 2, and the lever y is put in the position releasing jaw F from said screw. Jaw F is then moved to, say, the position which is indicated by broken lines in said figure, Member K is then placed between jaws E and F and said jaw F-is forced on to member K, (Iorcing said member K against gay; E), by turnin nut f on said screw I-I.
en jaws E an F are in close contact with bar K the screw H is turned by lever j to lock aw F in place, and nut f is returned 'n, constructed as above deto its initial position (as indicated by the broken lines in Fig. 23.
When the aeroplane and gas ba are joined by the grasping members E, F eing forced onto the longitudinally extending member K, and held in grasping position by the mutilated screws described, the aeroplane may be operated in the usual manner to make a flight; the levitation of the gas bagassisting materially in rising. At any time, when above the ground, the engine and propeller of the aeroplane may be stopped, and the gas bag be relied upon for levitation.
When the aeroplane and gas bag are attached together a novice may safely attempt to operate the same, and when sufi'icient practice has been attained the aeroplane may e separated from the gas bag, by movement of lever and the flight continued in the aeroplane, after said separation; For observation purposes the engine and propeller of the aeroplane may be rotated at reduced speed, or entirely stopped, as best suits the demands of the conditions under which said observation 'is being made.
I do not claim any particular make of gas bag, or of aeroplane; nor do I claim that the gas bag must or need be sufficiently large to levitate the aeroplane and load thereof independently of the propeller and planes of the aeroplane, as the construction of the aer plane and gas bag forms no part of my invention.
The spring Q tends to force member F away from members E and K when the mutilated screw bolt H is turned to release said member F. I claim: 1. In a. combined gas bag and aeroplane the combination of a truss member, flexible connections arranged to attach said member to said gas bag, a longitudinally extending member attached to said truss member, members attached to said aeroplane and arranged to register with said longitudinally extending member latch members adapted to 00- act with said longitudinally extending member and with said registering members, and movable into and out of engaging position therewith, and means to hold said movable latch members in engagingposition, and operative means comprising a lever and connections joining said lever to said holding means.
2. In a combined gas bag and aeroplane, the combination of a truss member, means to attach said "member to said gas ba and means to separably attach said mem r to said aeroplane, said attaching means comprising a plurality of members attached to said aeroplane and arranged to register and co-act with said truss member, latch members respectively adapted to co-act with said truss member and said plurality of members, and movable into and out of engaging position, means to hold said latch members in engaging position, and operative means to release said latch meinbers from said holding position, said operative means comprising a lever and connections joining said lever to said holding means.
3. In a combined gas bag and aeroplane, a truss member, means to attach said truss member to said gas bag, a latch member, means to attach said latch member'to said truss member, in combination with a latch member attached to said aeroplane and arranged to register with said, truss member, a latch mem er adapted to co-act with the first named latch member, means to attach said co actuable latch member to said aerolane member, means to join said latch members and means to separate said latch memers.
' 4. In a combined gas bag and aeroplane, a truss member, means to attach said truss membeil sto said gas bag, a plurality of coactinglatch members, means to connect said latch members to said truss member, said latch members attached to said aeroplane and arranged to register with said truss member and said connecting means comprislurality of members adapted to 00- act with said latch members, in combination with operable means comprising a lever adapted to actuate said plurality of members to separate said co-acting latch members from said truss member.
5. In an apparatus consisting of a lighter than air and a heavier than air device, separable means for joining said lighter and heavier devices, comprising a longitudinally extending bar attached to said lighter than air device in combination with members, one whereof is movable, attached to said heavier than air device and adapted to 'engage with said longitudinally extending member, means to force said movable member into engagement with said longitudinally extending member, means to hold said engageable members in engaging position and means to simultaneously release said engaging members.
6. The combination of a gas bag and an aeroplane, comprising a longitudinally extending member below said gas bag and connections attaching said longitudinally ex- JAMES N. LEWIS.-
In the presence of CHARLES TURNER BROWN.
US1306348D Separable aeroplane and gas-bag Expired - Lifetime US1306348A (en)

Publications (1)

Publication Number Publication Date
US1306348A true US1306348A (en) 1919-06-10

Family

ID=3373874

Family Applications (1)

Application Number Title Priority Date Filing Date
US1306348D Expired - Lifetime US1306348A (en) Separable aeroplane and gas-bag

Country Status (1)

Country Link
US (1) US1306348A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2468009A (en) * 1944-08-30 1949-04-19 Bigley Jr Releasable suspension apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2468009A (en) * 1944-08-30 1949-04-19 Bigley Jr Releasable suspension apparatus

Similar Documents

Publication Publication Date Title
US1306348A (en) Separable aeroplane and gas-bag
US3396924A (en) Load transfer device
US2024222A (en) Toggle release hook
US1879632A (en) Engine release mechanism
US1855320A (en) Parachute
US3047261A (en) Parachute disreefing device
US1893232A (en) Bomb rack and control
US1337336A (en) Life-saving device for aeroplanes
US1812759A (en) Device for releasing shells in aircraft
US2404381A (en) Arresting hook
DE666885C (en) Rescue device for aviators with a seat lifting device that can be operated by an energy store
US1704968A (en) Airplane take-off
US1509032A (en) Parachute attachment for airships
US1715742A (en) Safety device for aeroplanes
US1106626A (en) Flying-machine.
US1025629A (en) Safety device for aeroplanes.
US1861977A (en) Aeroplane
US1428013A (en) Parachute for aeroplanes
US2234489A (en) Square bowl tubing spider
US536425A (en) Attorniy
US1504715A (en) Bomb-releasing shackle
US1842583A (en) Device for landing aircraft
US1713473A (en) Safety device for aeroplanes
DE380690C (en) Drive mechanism for driving two unloading flaps which are used to form one and the same unloading opening
US1845953A (en) Dual control for aeroplanes