US1045030A - Elevator for aerial vessels. - Google Patents
Elevator for aerial vessels. Download PDFInfo
- Publication number
- US1045030A US1045030A US65977111A US1911659771A US1045030A US 1045030 A US1045030 A US 1045030A US 65977111 A US65977111 A US 65977111A US 1911659771 A US1911659771 A US 1911659771A US 1045030 A US1045030 A US 1045030A
- Authority
- US
- United States
- Prior art keywords
- elevator
- plane
- elevator plane
- stays
- supporting
- 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
Links
- KHOITXIGCFIULA-UHFFFAOYSA-N Alophen Chemical compound C1=CC(OC(=O)C)=CC=C1C(C=1N=CC=CC=1)C1=CC=C(OC(C)=O)C=C1 KHOITXIGCFIULA-UHFFFAOYSA-N 0.000 description 1
- 241001394244 Planea Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Definitions
- This invention relates to elevators for aerial and other'vessels and refers to an-improvpd means-of actuating suchelevators by ⁇ vhic i the elevator plane orplanes are well under control and in which they are'held perfectly rigid in all positions.
- Figure 1 is 'a part sectional elevation of an elevator constructed according to my in vention.
- Fig. 2 is a front elevation of a portion of Fig. 1.
- Fig. 3 is a plan of Fig. 1.
- the same letters of reference are employed to denote the same parts in all the views z' a is an elevator.plane suitably pivoted to the supporting plane 6, said plane 6 being suitably cut away at the front thereof to p.er--
- the curvature -of the guide 6 is such that it. forms an arc of a circle struck from f,-.which is the center of rotat iori eif the elevator plane a.
- the piece d is set in various positions on s atues-Foe iAERIA'L te ms;
- the cables passing over suitable guide pulleys-f m is a handle for operating the drums 71:.
- $tates of America is 1.
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Escalators And Moving Walkways (AREA)
Description
I A. HORTON. ELEVATOR FOR AERIAL VESSELS. APPLIOATIZON FILED NOV. 11, 1911.
, 1,045,030. BatehtedNov. 1 ,1912.
a a g a 4 d 5 o L? "intense? 1 a To' all whom it may concern: Be it known that I, ALEXANDER a subject of the King of England, at 38 Marmion road, Portsmouth,
HORTON, residing England,
have-invented certain new and useful Improvements Relating. to Elevators for Aerial Vessels; of which the following is a specification.
- This invention relates to elevators for aerial and other'vessels and refers to an-improvpd means-of actuating suchelevators by \vhic i the elevator plane orplanes are well under control and in which they are'held perfectly rigid in all positions. I
" In carrying outlmy invention I attach to the corners of the elevator plane suitable stays which pass to a sliding piece adapted to slide-alonghn arc-shaped guide. The curvature of the arc is such that it is struck from the center, of rotation of theelevator plane. Suitable means are provided for enabling the pilot to alter the position of the sl'idingpart and thus control the position of the plane. And in order that my said invention maybe better understood I will now. proceed to describe the same with reference to the drawing accompanying this specification which shows "by way of example one method of carrying my aforesaid invention into practice.
Figure 1 is 'a part sectional elevation of an elevator constructed according to my in vention. Fig. 2 is a front elevation of a portion of Fig. 1. Fig. 3 is a plan of Fig. 1. The same letters of reference are employed to denote the same parts in all the views z' a is an elevator.plane suitably pivoted to the supporting plane 6, said plane 6 being suitably cut away at the front thereof to p.er--
mit of movement of the elevator plane a (see Fig. 3).
c are stays attached to the corners of the elevator plane a. These stays are united to a sliding piece at, which is adapted to slide.
along an arc-shaped guide'e. The curvature -of the guide 6 is such that it. forms an arc of a circle struck from f,-.which is the center of rotat iori eif the elevator plane a.
The piece d is set in various positions on s atues-Foe iAERIA'L te ms;
I p Specification ofLettersPateiit. Pa ented Nov. 19,1912. Application filed November 11, 1911:. Serial no. 659,771;
a v i the guide 6 in order to actuate the elevator plane a by meansof the cables g h, the cables passing over suitable guide pulleys-f m is a handle for operating the drums 71:.
When it is required to alter the angle of inclination of the elevator plane a it is simply necessary to turn the handle m in the required direction which causes the sliding piece (Z to be drawn-into the retpaired position on the" guide 6, carrying with it the stays 0 which set the elevator plane a in the required position. Owing to the construction of stays extending to the corners of this planea it is held perfectly rigidly in all positions.
$tates of America is 1. The combination with a supporting plane. of an aeroplane, ofan' elevator plane horizontally pivoted on said supporting'plan'e; an. arcuate guiding member rigidly mounted on the aeroplane and having its center coaxial with the pivotal axis of the elevator plane; a member-slidably mounted on'said 'arcua'te member; stays connecting said slidable. member with said elevator plane; and means connected with the slidable member for moving the same to actuate the elevator plane, substantially as described.
2. The combination "with a supporting 230' plane' of an aeroplane, of an elevator plane horizontally pivoted on said supporting plane, said supporting plane being cut away at the front portion thereof to' allow of V movement of the elevator plane; an arcuate'.85 guiding member rigidly mounted on the aeroplane" and having its center co-axial with the pivotal axis of the elevator plane;
' a member slida-bly mounted 'on said arcuate member; stays connecting said slidab-le mem her with said elevator plane; and .means connected with" the slidaible member for moving the same toactuate the elevator plane, substantially as described.
3. The combination with a supporting plane of an aeroplane, of an elevator plane horizontally pivoted on" said supporting plane; an arcuate guiding member rigidly at ent of the United What I'claimas invention and desire o5? said slidable member with said elevator plane; cords attached to said slidable memher; and a pair of drums journaled 0n the aeroplane having said cords oppositely wound thereon whereby to actuate the elevator plane, substantially as described. 10 In testimony whereof I have hereunto set my hand in the presence of two witnesses. ALEXANDER HORTON.
\Vitnesses:
L. SIMMONDS, T. O. RowLEY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US65977111A US1045030A (en) | 1911-11-11 | 1911-11-11 | Elevator for aerial vessels. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US65977111A US1045030A (en) | 1911-11-11 | 1911-11-11 | Elevator for aerial vessels. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1045030A true US1045030A (en) | 1912-11-19 |
Family
ID=3113304
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US65977111A Expired - Lifetime US1045030A (en) | 1911-11-11 | 1911-11-11 | Elevator for aerial vessels. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1045030A (en) |
-
1911
- 1911-11-11 US US65977111A patent/US1045030A/en not_active Expired - Lifetime
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2665084A (en) | Flap actuator and control system | |
| US5131603A (en) | Rotary wing aircraft split segmented duct shrouded propeller tail assembly | |
| US4040579A (en) | Variable camber leading edge airfoil system | |
| US3515361A (en) | Control of aircraft by deflection of propulsion gases | |
| US2609165A (en) | Flap positioning control system | |
| US2272725A (en) | Control of aircraft surfaces | |
| US1415176A (en) | Aeroplane control | |
| US1557214A (en) | Airplane-control mechanism | |
| US1536515A (en) | Control post | |
| US2445940A (en) | Aileron-rudder tab linkage | |
| US2788182A (en) | Aircraft wing and aileron controls | |
| US1309961A (en) | Aeroplane | |
| US1066860A (en) | Automatic stabilizer for aerial vehicles or other moving bodies. | |
| US2204404A (en) | Aircraft construction | |
| US1809936A (en) | Airplane control | |
| US1368548A (en) | Aileron braking system | |
| US1174679A (en) | Aerial vehicle. | |
| US1720960A (en) | Aeroplane control | |
| US1565097A (en) | Differential aileron control | |
| US3295797A (en) | Aircraft control systems | |
| US1165731A (en) | Rudder mechanism for airships. | |
| US2684216A (en) | Control mechanism | |
| US2186991A (en) | Draft check and control | |
| US1769161A (en) | Airplane | |
| US1233616A (en) | Aeroplane. |