US3745699A - Device for automatically lowering and landing an electric model plane - Google Patents
Device for automatically lowering and landing an electric model plane Download PDFInfo
- Publication number
- US3745699A US3745699A US00275772A US3745699DA US3745699A US 3745699 A US3745699 A US 3745699A US 00275772 A US00275772 A US 00275772A US 3745699D A US3745699D A US 3745699DA US 3745699 A US3745699 A US 3745699A
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- United States
- Prior art keywords
- electromagnet
- plane
- battery
- horizontal tail
- horizontal
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- Expired - Lifetime
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
Definitions
- ABSTRACT A de ice for automatically lowering and landing an electric modelplane of the free flight type comprising an electromagnet securely mounted on a plane body and energized by a battery for supplying a motor for a propeller with an electric power; and a system connecting said electromagnet to horizontal planes hingedly mounted on the plane body and which includes a magnetic member rotatably held by said electromagnet and a tensile means fixed to the plane body.
- Said magnetic member is adapted to be attracted by said electromagnet against an action of the tensile means while the magnet is sufficiently energized by the battery thereby to maintain said horizontal tail planes in a horizontal flight position and said tensile means acts on the tail planes to shift the same into a slantingly raised position when the attracting force of said electromagnet is overcome by the action of said tensile means by exhaustion of the 'power thereby lowering and landing the plane automatically.
- This invention relates generally to an electric model plane of so-called free flight type, and more particuvarious kinds of devices including those devices of socalled pop up type, spoiler type and parachute type.
- the plane body is caused to loose the dynamic lift, the air resistance of the plane body is suddenly increased to correspondingly increase its lowering speed and/or the plane body is lowered by means ofa parachute'after a lapse of predetermined time with use of a time adjusting device such as a self-timer and a matchcord or fuse.
- time adjusting devices however, more or less have defects, that is to say, the self-timer involves high production costs and frequency troubles while the matchcord or fuse is susceptible to the danger of burning accidents.
- the primary object of the present invention is to provide a device for automatically lowering and landing an electric model plane which will eliminate the above noted difficulties.
- Another object of the present invention is to provide a'device for automatically lowering and landing an electric model plane of the type mentioned above which is low in manufacturing cost, easy to handle and reliable in operation.
- a further object of the present invention is to provide a device for automatically lowering and landing an electric model plane of the type mentioned above which is simple in construction and free from troubles.
- One of the features of the present invention resides a device for automatically loweing and landing an electric model plane including horizontal tail planes hingedly mounted on a plane body at a tail portion thereof, an electric motor for rotating a propeller and a battery acting as a power source forsaid electric motor; which comprises an electromagnet securely mounted on theplane body and energized by said battery; and a system for connecting said electromagnet to the horizontal tail planes which includes a magnetic member attracted by the electromagnet to maintain said horizontal tail planes in a horizontal flight position while the electromagnet'is sufficiently energized by the battery, and a tensile means acting on the tail planes for shifting the same into a slantingly raised position when the battery is almost exhausted thereby to lower the plane before complete exhaustion of the power.
- FIG. I is a side elevation of the device embodying the FIG. 3 is a side elevation showing the manner in which the plane is lowered;
- FIGS. 4 and 5 are perspective views each showing the relationship between the electromagnet and the iron plate member.
- FIG. 6 is a perspective view showing the relationship between the horizontal tail and the push rod member.
- a plane body of the model plane which has an electric motor 2, a propeller 3, battery 4, a switch 5, an electromagnet 6 and a lead line 6a from the electromagnet 6. All these component parts are mounted suitably on the plane body 1 as shown in FIG. 1.
- Designated at 7 is a plate member, preferably of iron material, securely supported on a rotary plate member 8.
- the rotary plate member 8 is mounted on a shaft 10 extending between and supported by a pair of support arms 9.
- the reference numeral 11 shows horizontal tail planes which is pivotally mounted at the tail of the plane body 1 by means of hinges 13.
- One end of a push rod member 12 is connected to the lower portion of the afore-mentioned rotary plate member 8 while the other end is connected to a horn 11a secured to the horizontal tail planes 11.
- a tension'spring 14 having one end thereof secured to the push rod member 12 and the other end to the plane body 1, It is to be noted that any tensile means such as a rubber string may be alternatively'employed.
- the electromagnet 6 is energized by the battery 4 to attract the iron plate member 8 by rotating the same around the shaft 10 from the position shown in FIG. 5 to the position shown in FIG. 4. As the iron plate member 8 is rotated, the
- push rod member 12 is brought into the position shown in FIG. 1 against the action of the tension spring 14 to maintain the horizontal tail planes in the normal flight position or horizontal position shown in FIG. 1. If, then, the battery 4 becomes almost exhausted, the attracting force of the electromagnet 6 is overcome by the action of the tension spring 14, allowing the push rod member. 12 to be shifted from the forward position shown in FIG. 1 to the retracted position shown in FIG. 2. This causes the horizontal tail planes 1 l to rotate around the hinge 13 into the slantingly raised position as shown in FIG. 2 by way of the horn 11a. With the horizontal tail plane heldin the slantingly raised position or the lower ing position, the plane body is safely lowered and landed since the rotational speed of the motor 2 is rapidly reduced due to reduced power supply from the battery 4 which is almost exhausted.
- a device for automatically lowering and landing an electric model plane including horizontal tail planes hingedly mounted on a plane body at a tail portion thereof, an electric motor for rotating a propeller and a battery acting as a power source for said electric motor; which comprises an electromagnet securely mounted on the plane body and energized by said bat tery; and a system for connecting said electromagnet to the horizontal tail planes which includes a magnetic member attracted by the electromagnet to maintain said horizontal tail planes in a horizontal flight position while the electromagnet is sufficiently energized by the battery, and a tensile means action on the tail planes for shifting the same into a slantingly raised position when the battery is almost exhausted thereby to lower the plane before complete exhaustion of the power.
- a device for automatically lowering and landing an electric model plane as claimed in claim 1, wherein said system comprises a rotary member pivotally mounted on a shaft and securely fitted to said magnetic member; a rod member connected at one end to the lower portion of said rotary member and at the other end to said horizontal tail planes, said magnetic member being attracted by said electromagnet to pull said rod member forward thereby maintaining the horizontal tail planes in the horizontal flight position while the electromagnet is sufficiently energized by said batteryrand a tension both sides of said electromagnet.
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Abstract
A device for automatically lowering and landing an electric model plane of the free flight type comprising an electromagnet securely mounted on a plane body and energized by a battery for supplying a motor for a propeller with an electric power; and a system connecting said electromagnet to horizontal planes hingedly mounted on the plane body and which includes a magnetic member rotatably held by said electromagnet and a tensile means fixed to the plane body. Said magnetic member is adapted to be attracted by said electromagnet against an action of the tensile means while the magnet is sufficiently energized by the battery thereby to maintain said horizontal tail planes in a horizontal flight position and said tensile means acts on the tail planes to shift the same into a slantingly raised position when the attracting force of said electromagnet is overcome by the action of said tensile means by exhaustion of the power thereby lowering and landing the plane automatically.
Description
United States Patent [1 1 Mabuc'hi i July 17,1973
[ DEVICE FOR AUTOMATICALLY LOWERING AND LANDING AN ELECTRIC MODEL PLANE [75] Inventor: Kenichi Mabuchi, Katsushika-ku,
Tokyo, Japan 73 Assignee: Mabuchi Motor Co., Ltd., Tokyo,
Japan 221 Filed: July 27,1972 211 Appl. No.: 275,772
[30] Foreign Application Priority Data Oct. 25, 1971 Japan 46/9794l [52] US. Cl 46/243 AV, 46/76 R [51] Int. Cl .1 A63h 27/00 [58] Field of Search 46/76 R, 243'AV [56] References Cited UNITED STATES PATENTS 2,386,288 l0/l945 Blaylock 46/76 R UX 2,599,484 6/1952 Rhodes 46/76 R 3,699,708 10/1972 Mabuchi 46/243 AV Primary Examiner-Louis G. Mancene Assistant Examiner-Robert F. Cutting Attorney-James E. Armstrong et al.
[57] ABSTRACT A de ice for automatically lowering and landing an electric modelplane of the free flight type comprising an electromagnet securely mounted on a plane body and energized by a battery for supplying a motor for a propeller with an electric power; and a system connecting said electromagnet to horizontal planes hingedly mounted on the plane body and which includes a magnetic member rotatably held by said electromagnet and a tensile means fixed to the plane body. Said magnetic member is adapted to be attracted by said electromagnet against an action of the tensile means while the magnet is sufficiently energized by the battery thereby to maintain said horizontal tail planes in a horizontal flight position and said tensile means acts on the tail planes to shift the same into a slantingly raised position when the attracting force of said electromagnet is overcome by the action of said tensile means by exhaustion of the 'power thereby lowering and landing the plane automatically.
4 Claims, 6 Drawing Figures PAIENTE JUL 1 1191s saw 2 or 2 DEVICE FOR AUTOMATICALLY LOWERING AND LANDING AN ELECTRIC MODEL PLANE This invention relates generally to an electric model plane of so-called free flight type, and more particuvarious kinds of devices including those devices of socalled pop up type, spoiler type and parachute type. With these devices, the plane body is caused to loose the dynamic lift, the air resistance of the plane body is suddenly increased to correspondingly increase its lowering speed and/or the plane body is lowered by means ofa parachute'after a lapse of predetermined time with use of a time adjusting device such as a self-timer and a matchcord or fuse. These time adjusting devices, however, more or less have defects, that is to say, the self-timer involves high production costs and frequency troubles while the matchcord or fuse is susceptible to the danger of burning accidents.-
The primary object of the present invention is to provide a device for automatically lowering and landing an electric model plane which will eliminate the above noted difficulties. 1
Another object of the present invention is to provide a'device for automatically lowering and landing an electric model plane of the type mentioned above which is low in manufacturing cost, easy to handle and reliable in operation.
A further object of the present invention is to provide a device for automatically lowering and landing an electric model plane of the type mentioned above which is simple in construction and free from troubles.
One of the features of the present invention resides a device for automatically loweing and landing an electric model plane including horizontal tail planes hingedly mounted on a plane body at a tail portion thereof, an electric motor for rotating a propeller and a battery acting as a power source forsaid electric motor; which comprises an electromagnet securely mounted on theplane body and energized by said battery; and a system for connecting said electromagnet to the horizontal tail planes which includes a magnetic member attracted by the electromagnet to maintain said horizontal tail planes in a horizontal flight position while the electromagnet'is sufficiently energized by the battery, and a tensile means acting on the tail planes for shifting the same into a slantingly raised position when the battery is almost exhausted thereby to lower the plane before complete exhaustion of the power.
These together with other objects and advantages which will become subsequently apparent reside in the details of construction and operation as more fully hereinafter described and claimed, reference being had to the accompanying drawings forming a part hereof, wherein like numerals refer to like parts throughout, and in which:
FIG. I is a side elevation of the device embodying the FIG. 3 is a side elevation showing the manner in which the plane is lowered;
FIGS. 4 and 5 are perspective views each showing the relationship between the electromagnet and the iron plate member; and
FIG. 6 is a perspective view showing the relationship between the horizontal tail and the push rod member.
Referring in detail to the accompanying drawings showing a preferred embodiment of the present invention, there is shown at l a plane body of the model plane which has an electric motor 2, a propeller 3, battery 4, a switch 5, an electromagnet 6 and a lead line 6a from the electromagnet 6. All these component parts are mounted suitably on the plane body 1 as shown in FIG. 1.
Designated at 7 is a plate member, preferably of iron material, securely supported on a rotary plate member 8. The rotary plate member 8 is mounted on a shaft 10 extending between and supported by a pair of support arms 9. The reference numeral 11 shows horizontal tail planes which is pivotally mounted at the tail of the plane body 1 by means of hinges 13. One end of a push rod member 12 is connected to the lower portion of the afore-mentioned rotary plate member 8 while the other end is connected to a horn 11a secured to the horizontal tail planes 11. There is provided a tension'spring 14 having one end thereof secured to the push rod member 12 and the other end to the plane body 1, It is to be noted that any tensile means such as a rubber string may be alternatively'employed.
With the above construction, the electromagnet 6 is energized by the battery 4 to attract the iron plate member 8 by rotating the same around the shaft 10 from the position shown in FIG. 5 to the position shown in FIG. 4. As the iron plate member 8 is rotated, the
What is claimed is:
l. A device for automatically lowering and landing an electric model plane including horizontal tail planes hingedly mounted on a plane body at a tail portion thereof, an electric motor for rotating a propeller and a battery acting as a power source for said electric motor; which comprises an electromagnet securely mounted on the plane body and energized by said bat tery; and a system for connecting said electromagnet to the horizontal tail planes which includes a magnetic member attracted by the electromagnet to maintain said horizontal tail planes in a horizontal flight position while the electromagnet is sufficiently energized by the battery, and a tensile means action on the tail planes for shifting the same into a slantingly raised position when the battery is almost exhausted thereby to lower the plane before complete exhaustion of the power.
2. A device for automatically lowering and landing an electric model plane as claimed in claim 1, wherein said system comprises a rotary member pivotally mounted on a shaft and securely fitted to said magnetic member; a rod member connected at one end to the lower portion of said rotary member and at the other end to said horizontal tail planes, said magnetic member being attracted by said electromagnet to pull said rod member forward thereby maintaining the horizontal tail planes in the horizontal flight position while the electromagnet is sufficiently energized by said batteryrand a tension both sides of said electromagnet.
* is a: 1: 1i
Claims (4)
1. A device for automatically lowering and landing an electric model plane including horizontal tail planes hingedly mounted on a plane body at a tail portion thereof, an electric motor for rotating a propeller and a battery acting as a power source for said electric motor; which comprises an electromagnet securely mounted on the plane body and energized by said battery; and a system for connecting said electromagnet to the horizontal tail planes which includes a magnetic member attracted By the electromagnet to maintain said horizontal tail planes in a horizontal flight position while the electromagnet is sufficiently energized by the battery, and a tensile means action on the tail planes for shifting the same into a slantingly raised position when the battery is almost exhausted thereby to lower the plane before complete exhaustion of the power.
2. A device for automatically lowering and landing an electric model plane as claimed in claim 1, wherein said system comprises a rotary member pivotally mounted on a shaft and securely fitted to said magnetic member; a rod member connected at one end to the lower portion of said rotary member and at the other end to said horizontal tail planes, said magnetic member being attracted by said electromagnet to pull said rod member forward thereby maintaining the horizontal tail planes in the horizontal flight position while the electromagnet is sufficiently energized by said battery; and a tension spring having one end thereof connected to said rod member and the other end secured to said plane body and pulling backward the rod member to shift the horizontal tail plane into a slantingly raised position when the battery is almost exhausted.
3. A device as defined in claim 2, wherein said rod member is connected to the horizontal tail plane by way of a horn member secured to the lower face of said horizontal tail plane.
4. A device as defined in claim 2, wherein said shaft is supported on a pair of arm members extended on both sides of said electromagnet.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1971097941U JPS5037912Y2 (en) | 1971-10-25 | 1971-10-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3745699A true US3745699A (en) | 1973-07-17 |
Family
ID=14205679
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00275772A Expired - Lifetime US3745699A (en) | 1971-10-25 | 1972-07-27 | Device for automatically lowering and landing an electric model plane |
Country Status (8)
Country | Link |
---|---|
US (1) | US3745699A (en) |
JP (1) | JPS5037912Y2 (en) |
AU (1) | AU466498B2 (en) |
CA (1) | CA942501A (en) |
DE (1) | DE2246207C3 (en) |
FR (1) | FR2152199A5 (en) |
GB (1) | GB1353874A (en) |
IT (1) | IT963459B (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3796005A (en) * | 1973-02-23 | 1974-03-12 | Mattel Inc | Simulated jet airplane toy |
US3807087A (en) * | 1972-10-10 | 1974-04-30 | Mattel Inc | Automatic battery cut-off system for electric motor-driven toy vehicles using rechargeable batteries |
US3827181A (en) * | 1972-03-23 | 1974-08-06 | Mabuchi Motor Co | Electrically driven model airplane |
US4181830A (en) * | 1976-04-29 | 1980-01-01 | Hermann Neuhierl | Flight control system for free flight model aeroplanes |
US20050178898A1 (en) * | 2004-01-28 | 2005-08-18 | Yuen Shun M. | Method and apparatus for controlling an airplane |
CN102188823A (en) * | 2011-03-09 | 2011-09-21 | 北京联合大学 | Multi-rudder cluster type electric steering gear system and control method thereof |
CN106394873A (en) * | 2016-09-26 | 2017-02-15 | 西安交通大学 | Buckling beam-based bi-stable state electromagnetic steering engine and control method |
CN106606874A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Novel aircraft power system |
CN109741673A (en) * | 2019-01-31 | 2019-05-10 | 佛山市神风航空科技有限公司 | A kind of model suspending aircraft |
US11378982B2 (en) * | 2015-04-30 | 2022-07-05 | SZ DJI Technology Co., Ltd. | System and method for landing a mobile platform via a magnetic field |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2386288A (en) * | 1941-05-02 | 1945-10-09 | Curtiss Wright Corp | Landing gear and wing slot control |
US2599484A (en) * | 1947-08-01 | 1952-06-03 | William A Rhodes | Steering control for model aircraft |
US3699708A (en) * | 1970-12-02 | 1972-10-24 | Mabuchi Motor Co | Electric-powered model airplane |
-
1971
- 1971-10-25 JP JP1971097941U patent/JPS5037912Y2/ja not_active Expired
-
1972
- 1972-07-19 GB GB3376472A patent/GB1353874A/en not_active Expired
- 1972-07-20 AU AU44812/72A patent/AU466498B2/en not_active Expired
- 1972-07-21 CA CA147,719A patent/CA942501A/en not_active Expired
- 1972-07-27 US US00275772A patent/US3745699A/en not_active Expired - Lifetime
- 1972-07-27 IT IT2753572A patent/IT963459B/en active
- 1972-09-07 FR FR7231806A patent/FR2152199A5/fr not_active Expired
- 1972-09-21 DE DE2246207A patent/DE2246207C3/en not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2386288A (en) * | 1941-05-02 | 1945-10-09 | Curtiss Wright Corp | Landing gear and wing slot control |
US2599484A (en) * | 1947-08-01 | 1952-06-03 | William A Rhodes | Steering control for model aircraft |
US3699708A (en) * | 1970-12-02 | 1972-10-24 | Mabuchi Motor Co | Electric-powered model airplane |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3827181A (en) * | 1972-03-23 | 1974-08-06 | Mabuchi Motor Co | Electrically driven model airplane |
US3807087A (en) * | 1972-10-10 | 1974-04-30 | Mattel Inc | Automatic battery cut-off system for electric motor-driven toy vehicles using rechargeable batteries |
US3796005A (en) * | 1973-02-23 | 1974-03-12 | Mattel Inc | Simulated jet airplane toy |
US4181830A (en) * | 1976-04-29 | 1980-01-01 | Hermann Neuhierl | Flight control system for free flight model aeroplanes |
US20050178898A1 (en) * | 2004-01-28 | 2005-08-18 | Yuen Shun M. | Method and apparatus for controlling an airplane |
CN102188823A (en) * | 2011-03-09 | 2011-09-21 | 北京联合大学 | Multi-rudder cluster type electric steering gear system and control method thereof |
US11378982B2 (en) * | 2015-04-30 | 2022-07-05 | SZ DJI Technology Co., Ltd. | System and method for landing a mobile platform via a magnetic field |
US20220348316A1 (en) * | 2015-04-30 | 2022-11-03 | SZ DJI Technology Co., Ltd. | System and method for landing a mobile platform via a magnetic field |
CN106606874A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Novel aircraft power system |
CN106394873A (en) * | 2016-09-26 | 2017-02-15 | 西安交通大学 | Buckling beam-based bi-stable state electromagnetic steering engine and control method |
WO2018054105A1 (en) * | 2016-09-26 | 2018-03-29 | 西安交通大学 | Buckled beam-based bi-stable state electromagnetic steering engine and control method |
CN109741673A (en) * | 2019-01-31 | 2019-05-10 | 佛山市神风航空科技有限公司 | A kind of model suspending aircraft |
Also Published As
Publication number | Publication date |
---|---|
AU4481272A (en) | 1974-02-07 |
GB1353874A (en) | 1974-05-22 |
JPS4851495U (en) | 1973-07-04 |
FR2152199A5 (en) | 1973-04-20 |
CA942501A (en) | 1974-02-26 |
AU466498B2 (en) | 1975-10-30 |
DE2246207C3 (en) | 1979-07-12 |
IT963459B (en) | 1974-01-10 |
DE2246207B2 (en) | 1978-11-02 |
DE2246207A1 (en) | 1973-05-03 |
JPS5037912Y2 (en) | 1975-11-04 |
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