GB429723A - Improvements in or relating to supports for instruments - Google Patents
Improvements in or relating to supports for instrumentsInfo
- Publication number
- GB429723A GB429723A GB26577/34A GB2657734A GB429723A GB 429723 A GB429723 A GB 429723A GB 26577/34 A GB26577/34 A GB 26577/34A GB 2657734 A GB2657734 A GB 2657734A GB 429723 A GB429723 A GB 429723A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- annular
- resilient
- inner annular
- sept
- 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
Links
- 238000013016 damping Methods 0.000 abstract 1
- 239000011521 glass Substances 0.000 abstract 1
- 230000010355 oscillation Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Springs (AREA)
Abstract
429,723. Resilient mountings. ASKANIA WERKE AKT.-GES., VORM. CENTRALWERKSTATT DESSAU UND C. BAMBERGFRIEDENAU, 87, Kaiserallee, Friedenau, Berlin. Sept. 15, 1934, No. 26577. Convention date, Sept. 18, 1933. [Class 108 (iii)] [See also Groups XIX and XX] A resilient support for instruments, such as aircraft, &c., compasses, and variometers, comprises an outer annular member adapted to be secured directly to the dashboard &c., and an inner annular member adapted directly to receive the instrument, the annular members being connected, in order to damp oscillations, by resilient members or sets of members extending substantially tangentially to the inner annular member. As shown a compass housing 1 having a glass dome 2 has a cylindrical extension 3 supported by a clamping- ring 4, to which the inner annular conical member 10 is screwed. The outer annular conical member 7 carries a supporting bracket 6 and is secured to the member 10 by rubber cords 11, 12 passing alternately through two apertures in each member. Gaps 8 in the annular members provide accessibility to a graduated ring 9 for adjusting the compass. A greater degree of damping may be obtained by the provision of a layer 15 of sponge rubber between the annular members.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE429723X | 1933-09-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB429723A true GB429723A (en) | 1935-06-05 |
Family
ID=6477648
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26577/34A Expired GB429723A (en) | 1933-09-18 | 1934-09-15 | Improvements in or relating to supports for instruments |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB429723A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2050235A1 (en) * | 1969-07-04 | 1971-04-02 | Sud Aviation | Expanded polystyrene shock absorbant - instrument mounting for space craft |
CN111924115A (en) * | 2020-08-19 | 2020-11-13 | 苏梦 | Emergency forced landing buffer device for unmanned aerial vehicle |
-
1934
- 1934-09-15 GB GB26577/34A patent/GB429723A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2050235A1 (en) * | 1969-07-04 | 1971-04-02 | Sud Aviation | Expanded polystyrene shock absorbant - instrument mounting for space craft |
CN111924115A (en) * | 2020-08-19 | 2020-11-13 | 苏梦 | Emergency forced landing buffer device for unmanned aerial vehicle |
CN111924115B (en) * | 2020-08-19 | 2024-01-05 | 中科华控航天科技合肥有限公司 | Unmanned aerial vehicle emergency landing buffer device |
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